Garmin Software Version 0734 7A Pilots Guide
2015-05-27
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Embraer Prodigy® Flight Deck 100 Pilot’s Guide Embraer Phenom 100 Copyright © 2008-2010, 2012-2014 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0734.7A or later for the Embraer Phenom 100. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Garmin International, Inc., 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. Tel: 913/397.8200 Fax: 913/397.8282 Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A. Tel: 503/391.3411 Fax 503/364.2138 Garmin (Europe) Ltd, Liberty House, Hounsdown Business Park, Southampton, SO40 9LR, U.K. Tel: 44 (0) 23 8052 4000 Fax: 44 (0) 23 8052 4004 Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan Tel: 886/02.2642.9199 Fax: 886/02.2642.9099 For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount and integrated avionics systems, please contact Garmin’s AOG Hotline at 913.397.0836. Web Site Address: www.garmin.com Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited. Prodigy® is a registered trademark of Embraer-Empresa Brasileira de Aeronautica S.A. Garmin® is a registered trademark of Garmin Ltd. or its subsidiaries. WATCH®, FliteCharts®, and SafeTaxi® are trademarks of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin. Bendix/King® and Honeywell® are registered trademarks of Honeywell International, Inc.; Becker® is a registered trademark of Becker Flugfunkwerk GmbH; NavData® is a registered trademark of Jeppesen, Inc.; XM® is a registered trademark of XM Satellite Radio, Inc. SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio, Inc. AC-U-KWIK® is a registered trademark of Penton Business Media Inc. AOPA Membership Publications, Inc. and its related organizations (hereinafter collectively “AOPA”) expressly disclaim all warranties, with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties of merchantability and fitness for a particular purpose. The information is provided “as is” and AOPA does not warrant or make any representations regarding its accuracy, reliability, or otherwise. Under no circumstances including negligence, shall AOPA be liable for any incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even if AOPA or an AOPA authorized representative has been advised of the possibility of such damages. User agrees not to sue AOPA and, to the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action, claims or losses related to any actual or alleged inaccuracies in the information. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations or exclusions may not apply to you. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”) expressly disclaim all warranties with respect to the AC-U-KWIK information included in this data, express or implied, including, but not limited to, the implied warranties of merchantability and fitness for a particular purpose. The information is provided “as is” and AC-U-KWIK Organizations do not warrant or make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses related to any actual or alleged inaccuracies in the information arising out of Garmin’s use of the information in the datasets. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations or exclusions may not apply to licensee. October, 2014 Embraer Prodigy® Flight Deck 100 Pilot’s Guide Printed in the U.S.A. 190-00728-06 Rev. A WARNINGS, CAUTIONS, AND NOTES WARNING: Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature. The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The terrain avoidance feature is only to be used as an aid for terrain avoidance. Terrain data is obtained from third party sources. Garmin is not able to independently verify the accuracy of the terrain data. WARNING: The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical charts for appropriate minimum clearance altitudes. WARNING: The altitude calculated by the GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters, such as the GDC 74B Air Data Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always use pressure altitude displayed by the PFD or other pressure altimeters in aircraft. WARNING: Do not use outdated database information. Databases used in the system must be updated regularly in order to ensure that the information remains current. Pilots using any outdated database do so entirely at their own risk. WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness. WARNING: Traffic information shown on system displays is provided as an aid in visually acquiring traffic. Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic. WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous weather. Information contained within data link weather products may not accurately depict current weather conditions. WARNING: Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather product. Due to time delays inherent in gathering and processing weather data for data link transmission, the weather information shown by the data link weather product may be significantly older than the indicated weather product age. WARNING: The Prodigy® Integrated Flight Deck, as installed in the Embraer Phenom 100 aircraft, has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/or self-test capability for all conceivable system failures is not practical. Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the system. It is thus the responsibility of the pilot to detect such an occurrence by means of cross-checking with all redundant or correlated information available in the cockpit. WARNING: For safety reasons, system operational procedures must be learned on the ground. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide iii WARNINGS, CAUTIONS, AND NOTES WARNING: The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the system utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system can be misused or misinterpreted and, therefore, become unsafe. WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the Prodigy® Pilot’s Guide documentation and the Embraer Phenom 100 Airplane Flight Manual. Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications from the system to all available navigation sources, including the information from other NAVAIDs, visual sightings, charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation. WARNING: The illustrations in this guide are only examples. Never use the system to attempt to penetrate a thunderstorm. Both the FAA Advisory Circular, Subject: Thunderstorms, and the Aeronautical Information Manual (AIM) recommend avoiding “by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo.” WARNING: Lamp(s) inside this product may contain mercury (HG) and must be recycled or disposed of according to local, state, or federal laws. For more information, refer to our website at www.garmin.com/ aboutGarmin/environment/disposal.jsp. WARNING: Because of variation in the earth’s magnetic field, operating the system within the following areas could result in loss of reliable attitude and heading indications. North of 72° North latitude at all longitudes. South of 70° South latitude at all longitudes. North of 65° North latitude between longitude 75° W and 120° W. (Northern Canada). North of 70° North latitude between longitude 70° W and 128° W. (Northern Canada). North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia). South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and New Zealand). WARNING: Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned in error as displayed. CAUTION: The PFD and MFD displays use a lens coated with a special anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an eyeglass lens cleaner that is specified as safe for anti-reflective coatings. CAUTION: The system does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and the pilot’s authority to operate this device under FAA/FCC regulations. iv Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A WARNINGS, CAUTIONS, AND NOTES NOTE: All visual depictions contained within this document, including screen images of the panel and displays, are subject to change and may not reflect the most current system and databases. Depictions of equipment may differ slightly from the actual equipment. NOTE: This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions: (1) this device may not cause harmful interference, and (2) this device must accept any interference received, including interference that may cause undesired operation. NOTE: This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with California’s Proposition 65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/prop65. NOTE: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition. NOTE: Use of polarized eyewear may cause the flight displays to appear dim or blank. NOTE: Do not rely solely upon data link services to provide Temporary Flight Restriction (TFR) information. Always confirm TFR information through official sources such as Flight Service Stations or Air Traffic Control. NOTE: The FAA has asked Garmin to remind pilots who fly with Garmin database-dependent avionics of the following: • It is the pilot’s responsibility to remain familiar with all FAA regulatory and advisory guidance and information related to the use of databases in the National Airspace System. • Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen. Databases obtained from Garmin or Jeppesen are assured compliance with all data quality requirements (DQRs) by virtue of a Type 2 Letter of Authorization (LOA) from the FAA. A copy of the Type 2 LOA is available for each database and can be viewed at http://fly.garmin.com by selecting ‘Type 2 LOA Status.’ • Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with established FAA regulatory guidance, but does not constitute authorization to fly any and all terminal procedures that may be presented by the system. It is the pilot’s responsibility to operate in accordance with established AFM(S) and regulatory guidance or limitations as applicable to the pilot, the aircraft, and installed equipment. NOTE: The pilot/operator must review and be familiar with Garmin’s database exclusion list as discussed in SAIB CE-14-04 to determine what data may be incomplete. The database exclusion list can be viewed at www.flygarmin.com by selecting ‘Database Exclusions List.’ 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide v WARNINGS, CAUTIONS, AND NOTES NOTE: The pilot/operator must have access to Garmin and Jeppesen database alerts and consider their impact on the intended aircraft operation. The database alerts can be viewed at www.flygarmin.com by selecting ‘Aviation Database Alerts.’ NOTE: If the pilot/operator wants or needs to adjust the database, contact Garmin Product Support to coordinate the revised DQRs. NOTE: Garmin requests the flight crew report any observed discrepancies related to database information. These discrepancies could come in the form of an incorrect procedure; incorrectly identified terrain, obstacles and fixes; or any other displayed item used for navigation or communication in the air or on the ground. Go to FlyGarmin.com and select ‘Report An Aviation Data Error Report.’ vi Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A REVISION INFORMATION Record of Revisions Part Number 190-00728-00 190-00728-01 Revision Date A July, 2008 A Page Range All 190-00728-02 A September, 2009 All 190-00728-02 B September, 2009 190-00728-03 A November, 2010 Copyright Page All 190-00728-04 A March, 2012 All 190-00728-05 A May, 2013 All 190-00728-06 Rev. A Description Production release Added ADF Added ChartView and FliteCharts Added TAS Added flight plan import/export Added other GDU 9.14 parameters Added Synthetic Vision System TAWS-A TCAS I TCAS II ADF Tuning Radar Altimeter Added AOPA Airport Directory Added Iridium Satellite Telephone and Data Link Services Electronic checklists Added dual navigation database capability Added database synchronization Added other GDU 10.00 parameters Changed system software number from 0734.19 to 0734.24 Added METARs to active flight plan and maps Updated XM Weather product age and icon display Added SMS texting Updated database update procedures Added other GDU 11.12 parameters Updated CAS messages Updated SiriusXM Satellite Radio audio mute procedure Added Pilot Profiles Updated Database Update procedures Added optional Spoilers Added AC-U-KWIK Airport Directory capability Updated GFDS registration procedure Added Inset Map WX LGND Softkey Removed flightplan sorting capability Added other GDU 12.11 parameters Added CPDLC Added User Defined Holds Added temperature compensated altitude Updated CAS and voice messages Added other GDU 13.01 parameters Embraer Prodigy® Flight Deck 100 Pilot’s Guide vii REVISION INFORMATION Record of Revisions 190-00728-06 viii A October, 2014 All Added support for ADS-B out Updated MFD Data Bar Field choices Added Ice Detector Option Added Wind Speed and Heading Indicator Improvements Added support for Bottlang Charts Updated CPDLC discussion Added Profile View Added Weather Radar overlay on the Navigation Map Updated Iridium Telephone Page Displays Updated CAS messages Added other GDU 14.02 parameters Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A TABLE OF CONTENTS SECTION 1 SYSTEM OVERVIEW 1.1 System Description.................................................. 1 1.2 Line Replaceable Units (LRU).................................. 2 1.3 Prodigy® Controls..................................................... 8 MFD/PFD Controls......................................................... 8 MFD Control Unit........................................................ 10 AFCS Controls............................................................. 11 Audio Panel Controls................................................... 13 Softkey Function.......................................................... 15 1.4 Secure Digital Cards.............................................. 26 1.5 System Power-up.................................................... 27 1.6 System Operation................................................... 28 Normal Operation........................................................ 28 Reversionary Mode...................................................... 29 AHRS Operation.......................................................... 30 Prodigy® System Annunciations..................................... 31 GPS Receiver Operation............................................... 32 1.7 Accessing System Functionality........................... 37 Menus........................................................................ 37 MFD Page Groups........................................................ 37 MFD System Pages...................................................... 43 1.8 Display Backlighting.............................................. 59 Automatic Adjustment................................................. 59 Manual Adjustment..................................................... 59 SECTION 2 FLIGHT INSTRUMENTS 2.1 Flight Instruments.................................................. 64 Airspeed Indicator....................................................... 64 Attitude Indicator........................................................ 67 Altimeter.................................................................... 69 Vertical Speed Indicator (VSI)........................................ 72 Vertical Deviation........................................................ 73 Horizontal Situation Indicator (HSI)............................... 74 Course Deviation Indicator (CDI)................................... 79 2.2 Supplemental Flight Data..................................... 87 Temperature Displays................................................... 87 Wind Data.................................................................. 88 Vertical Navigation (VNV) Indications............................ 89 2.3 PFD Annunciations and Alerting Functions......... 90 System Annunciations.................................................. 90 Marker Beacon Annunciations...................................... 91 190-00728-06 Rev. A Traffic Annunciations................................................... 91 TAWS Annunciations.................................................... 92 Altitude Alerting.......................................................... 92 Low Altitude Annunciation........................................... 93 Minimum Descent Altitude/Decision Height Alerting....... 93 Radar Altimeter........................................................... 95 2.4 Abnormal Operations............................................ 97 Altitude Alerting.......................................................... 97 Abnormal GPS Conditions............................................ 97 Heading Failure Modes................................................ 98 Unusual Attitudes........................................................ 98 SECTION 3 ENGINE AND AIRFRAME SYSTEMS 3.1 Engine Indication System (EIS)........................... 104 Takeoff Data Set Window........................................... 105 Engine Indications..................................................... 106 Fuel and Electrical Indications..................................... 108 Cabin Pressurization.................................................. 109 Spoiler and Landing Gear........................................... 110 Flaps and Trim........................................................... 110 3.2 Synoptics............................................................... 111 System Status............................................................ 111 Environmental Control System (ECS)........................... 112 Electrical................................................................... 114 Fuel.......................................................................... 115 Ice Protection System................................................. 116 Engine Maintenance.................................................. 118 3.3 Abnormal Operations.......................................... 119 Engine...................................................................... 119 Cabin Pressurization.................................................. 119 Flaps........................................................................ 120 Trim.......................................................................... 120 SECTION 4 AUDIO PANEL AND CNS 4.1 Overview............................................................... 121 Audio Panel Volume Control....................................... 121 MFD/PFD Controls and Frequency Display.................... 122 Audio Panel Controls................................................. 124 4.2 COM Operation..................................................... 126 COM Transceiver Selection and Activation.................... 126 COM Transceiver Manual Tuning................................. 127 Quick-tuning and Activating 121.500 MHz................... 128 Auto-tuning the COM Frequency................................. 129 Embraer Prodigy® Flight Deck 100 Pilot’s Guide ix TABLE OF CONTENTS Frequency Spacing..................................................... 133 Automatic Squelch..................................................... 134 Volume..................................................................... 134 4.3 Controller Pilot Data Link Communications (CPDLC)............................................................................ 135 CPDLC Session Overview............................................ 135 CPDLC System Status................................................. 136 CPDLC Message Status Icons...................................... 137 Connecting to the CPDLC System................................ 138 Creating a Message................................................... 140 Responding to an ATC Message.................................. 141 Viewing an ATC Message........................................... 142 Viewing CPDLC Message Dialogs................................ 142 Deleting Message Dialogs.......................................... 143 Disconnecting from the CPDLC System........................ 144 Disabling Data Mode................................................. 144 CPDLC System Failure................................................ 144 4.4 NAV Operation...................................................... 145 NAV Radio Selection and Activation............................ 145 NAV Receiver Manual Tuning...................................... 146 Auto-tuning a NAV Frequency from the MFD................ 148 Marker Beacon Receiver............................................. 152 ADF/DME Tuning....................................................... 153 4.5 Mode S Transponder............................................ 157 GTX 33/33D Transponder Controls............................... 158 GTX 33/33D Transponder Mode Selection.................... 159 TCAS II Transponder Controls (optional)....................... 161 TCAS II Transponder Mode Selection (optional)............. 162 Entering a Transponder Code...................................... 164 IDENT Function......................................................... 165 Flight ID Reporting.................................................... 166 4.6 Additional Audio Panel Functions...................... 167 Power-Up.................................................................. 167 Mono/Stereo Headsets............................................... 167 Speaker.................................................................... 167 Intercom................................................................... 168 Passenger Address (PA) System................................... 169 Simultaneous COM Operation..................................... 169 Clearance Recorder and Player.................................... 170 Entertainment Inputs................................................. 171 4.7 Audio Panels Preflight Procedure....................... 172 4.8 Abnormal Operation............................................ 174 x Stuck Microphone...................................................... 174 COM Tuning Failure.................................................... 174 PFD Failure, Dual System............................................ 174 Audio Panel Fail-safe Operation.................................. 175 Reversionary Mode.................................................... 176 SECTION 5 FLIGHT MANAGEMENT 5.1 Introduction.......................................................... 177 Navigation Status Box................................................ 178 5.2 Using Map Displays.............................................. 180 Map Orientation........................................................ 180 Map Range............................................................... 182 Map Panning............................................................. 185 Measuring Bearing and Distance................................. 190 Topography............................................................... 191 Map Symbols............................................................ 194 Airways.................................................................... 200 Track Vector.............................................................. 202 Wind Vector.............................................................. 203 Nav Range Ring........................................................ 204 Fuel Range Ring........................................................ 205 Field of View (SVS)..................................................... 206 Selected Altitude Intercept Arc.................................... 207 5.3 Waypoints.............................................................. 208 Airports.................................................................... 209 Intersections............................................................. 216 NDBs........................................................................ 218 VORs........................................................................ 220 User Waypoints......................................................... 222 5.4 Airspaces............................................................... 228 5.5 Direct-to-Navigation ........................................... 232 5.6 Flight Planning...................................................... 238 Flight Plan Creation................................................... 239 Adding Waypoints to an Existing Flight Plan................. 244 Adding Airways to a Flight Plan.................................. 246 Adding Procedures to a Stored Flight Plan................... 249 Flight Plan Storage.................................................... 256 Flight Plan Editing..................................................... 258 Along Track Offsets.................................................... 262 Parallel Track............................................................. 263 Activating a Flight Plan Leg........................................ 266 Inverting a Flight Plan................................................ 267 Flight Plan Views....................................................... 268 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A TABLE OF CONTENTS Closest Point of FPL................................................... 270 User-Defined Holding Patterns.................................... 270 5.7 Vertical Navigation.............................................. 275 Altitude Constraints................................................... 277 5.8 Procedures............................................................ 281 Departures................................................................ 282 Arrivals .................................................................... 285 Approaches .............................................................. 288 5.9 Trip Planning......................................................... 296 Trip Planning............................................................. 296 Weight Planning........................................................ 300 Weight Caution And Warning Conditions..................... 302 5.10 RAIM Prediction................................................... 303 5.11 Navigating a Flight Plan...................................... 307 5.12 Abnormal Operation............................................ 335 SECTION 6 HAZARD AVOIDANCE 6.1 SiriusXM Weather................................................. 338 Activating Services.................................................... 338 Using SiriusXM Weather Products............................... 339 6.2 Garmin Connext Weather.................................... 373 Registering the system for Garmin Connext Weather..... 373 Accessing Garmin Connext Weather Products............... 375 Connext Weather Data Requests................................. 381 Garmin Connext Weather Products.............................. 385 Abnormal Operations................................................. 397 6.3 Airborne Color Weather Radar........................... 399 System Description.................................................... 399 Principles of Pulsed Airborne Weather Radar................ 399 NEXRAD and Airborne Weather Radar ........................ 400 Antenna Beam Illumination........................................ 400 Safe Operating Distance............................................. 403 Basic Antenna Tilt Setup............................................. 404 Weather Mapping and Interpretation.......................... 406 Ground Mapping and Interpretation............................ 418 Weather Radar Overlay on the Navigation Map Page.... 419 System Status............................................................ 420 6.4 TAWS-B.................................................................. 422 Displaying TAWS-B Data............................................. 423 TAWS-B Page............................................................ 426 TAWS-B Alerts........................................................... 428 System Status............................................................ 434 190-00728-06 Rev. A 6.5 TAWS-A.................................................................. 436 Displaying TAWS-A Data............................................ 437 TAWS-A Alerts........................................................... 442 System Status............................................................ 454 TAWS-A Abnormal operations..................................... 455 6.8 Profile View Terrain.............................................. 457 Profile View Display................................................... 457 Profile Path............................................................... 458 6.7 Traffic Information Service (TIS)......................... 461 Displaying TRAFFIC Data............................................ 462 Traffic Map Page........................................................ 464 TIS Alerts.................................................................. 465 System Status............................................................ 467 6.8 Garmin TCAS I Traffic........................................... 469 Theory of operation................................................... 469 TCAS I Alerts............................................................. 472 System Test............................................................... 473 Operation................................................................. 474 6.9 TCAS II Traffic........................................................ 483 TCAS II Symbology..................................................... 483 TCAS II Alerts............................................................ 484 System Test............................................................... 487 Operation................................................................. 488 System Status............................................................ 494 SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM 7.1 AFCS Controls....................................................... 498 7.2 Flight Director Operation.................................... 500 Activating the Flight Director...................................... 500 AFCS Status Box........................................................ 501 Flight Director Modes................................................. 502 Flight Director Selection............................................. 502 Command Bars.......................................................... 503 7.3 Vertical Modes...................................................... 504 Pitch Hold Mode (PIT)................................................ 505 Selected Altitude Capture Mode (ALTS)........................ 506 Altitude Hold Mode (ALT)........................................... 506 Vertical Speed Mode (VS)........................................... 508 Flight Level Change Mode (FLC).................................. 509 Vertical Navigation Modes (VPTH, ALTV)...................... 511 Glidepath Mode (GP) (sbas Only)................................ 516 Glideslope Mode (GS)................................................ 518 Takeoff (TO) and Go Around (GA) Modes..................... 519 Embraer Prodigy® Flight Deck 100 Pilot’s Guide xi TABLE OF CONTENTS 7.4 Lateral Modes....................................................... 520 Roll Hold Mode (ROL)................................................ 521 Low Bank Mode........................................................ 521 Heading Select Mode (HDG)....................................... 522 Navigation Modes (GPS, VOR, LOC, BC)....................... 523 Approach Modes (GPS, VAPP, LOC).............................. 525 7.5 Autopilot and Yaw Damper Operation.............. 527 Flight Control............................................................ 527 Engaging the Autopilot and Yaw Damper..................... 528 Control Wheel Steering.............................................. 528 Disengaging the Autopilot and Yaw Damper................. 529 7.6 Example Flight Plan............................................. 530 Departure................................................................. 531 Intercepting a VOR Radial........................................... 533 Flying a Flight Plan/GPS Course.................................. 534 Descent.................................................................... 535 Approach.................................................................. 539 Go Around/Missed Approach...................................... 542 7.7 AFCS Annunciations and Alerts.......................... 544 AFCS CAS Messages.................................................. 544 AFCS Voice Alerts....................................................... 545 Overspeed Protection................................................. 545 SECTION 8 ADDITIONAL FEATURES 8.1 Synthetic Vision Technology (SVT)...................... 548 SVT Operation........................................................... 549 SVT Features............................................................. 551 Field of View............................................................. 560 8.2 SafeTaxi................................................................. 562 SafeTaxi Database Cycle Number and Revision............. 565 8.3 ChartView.............................................................. 568 ChartView Softkeys.................................................... 569 Terminal Procedures Charts........................................ 570 Chart Options............................................................ 578 Day/Night View......................................................... 584 ChartView Cycle Number and Expiration Date.............. 586 8.4 FliteCharts............................................................. 589 FliteCharts Softkeys................................................... 590 Terminal Procedures Charts........................................ 591 Chart Options............................................................ 598 xii Day/Night View......................................................... 602 FliteCharts Cycle Number and Expiration Date.............. 604 8.5 Airport Directory.................................................. 607 Airport Directory Database Cycle Number and Revision.608 8.6 Satellite Telephone and SMS Messaging........... 610 Registering With Garmin Connext............................... 610 Telephone Communication......................................... 611 Text Messaging (SMS)................................................ 626 8.7 Wi-Fi Connections................................................ 638 8.8 Maintenance Logs................................................ 643 8.9 SiriusXM Satellite Radio Entertainment............ 645 Activating SiriusXM Satellite Radio Services................. 645 Using SiriusXM Satellite Radio.................................... 647 8.10 Scheduler............................................................... 650 8.11 Electronic Checklists............................................ 652 8.12 Abnormal Operation............................................ 655 SVT Troubleshooting.................................................. 655 Reversionary Mode.................................................... 655 Unusual Attitudes...................................................... 656 APPENDICES Annunciations and Alerts.............................................. 659 CAS Messages........................................................... 659 Comparator Annunciations......................................... 663 Reversionary Sensor Annunciations............................. 664 Prodigy® System Annunciations................................... 665 Prodigy® System Message Advisories........................... 669 TAWS-A Alerts........................................................... 682 TAWS-B Alerts........................................................... 684 TCAS I Alerts and Annunciations................................. 685 TCAS II Alerts and Annunciations................................ 686 CPDLC ATC Alert........................................................ 687 Other Prodigy® Aural Alerts......................................... 687 Flight Plan Import/Export Messages............................ 688 Pilot Profile Import/Export Messages........................... 688 Database Management................................................. 689 Jeppesen Databases................................................... 690 Garmin Databases..................................................... 693 Glossary........................................................................... 701 Frequently Asked Questions......................................... 707 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A TABLE OF CONTENTS General TIS Information................................................ 711 Introduction.............................................................. 711 TIS vs. TAS/TCAS........................................................ 711 TIS Limitations.......................................................... 711 Display Symbols............................................................. 713 INDEX Index .................................................................................I-1 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide xiii TABLE OF CONTENTS Blank Page xiv Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW SECTION 1 SYSTEM OVERVIEW 1.1 SYSTEM DESCRIPTION This section provides an overview of the Prodigy® Integrated Flight Deck as installed in the Embraer Phenom 100. The system is an integrated flight control system that presents flight instrumentation, position, navigation, communication, and identification information to the pilot through large-format displays. The system consists of the following Line Replaceable Units (LRUs): • GDU 1240A Primary Flight Displays and Multifunction Display • GDR 66 VHF Data Link Transceiver (optional) • GIA 63W Integrated Avionics Unit • GSR 56 Iridium Transceiver (optional) • GDC 74B Air Data Computer (ADC) • GWX 68 Weather Radar (optional) • GEA 71 Engine/Airframe Unit • GCU 475 MFD Control Unit • GRS 77 Attitude and Heading Reference System (AHRS) • GMC 715 AFCS Control Unit • GMU 44 Magnetometer • GMA 1347D Dual Audio System with Integrated Marker Beacon Receiver • GDL 59 Data Link (optional) • GSD 41 Data Concentrator • GTS 850 TCAS 1 System (optional) • GA 36 and GA 37 GPS/SBAS Antennas • GA 58 Traffic Avoidance System Antennas • GTX 33/33D Mode S Transponder (not used with TCAS II) • GSA 81 AFCS Servos • GDL 69A Satellite Data Link Receiver • GSM 86 Servo Gearboxes A top-level system block diagram is shown in Figure 1-1 (it does not include the GA 36, GA 37, GA 58, or GSM 86). NOTE: Refer to the AFCS section for details on the Garmin AFCS. In the Embraer Phenom 100, the Garmin AFCS+ Automated Flight Control System (AFCS) provides the flight director (FD), autopilot (AP), and yaw damper (YD) functions of the system. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 1 SYSTEM OVERVIEW 1.2 LINE REPLACEABLE UNITS (LRU) • GDU 1240A (3) – Each unit is configured as one of two PFDs or one MFD. The GDU 1240A features a 12-inch LCD with 1024 x 768 resolution. The unit installed on the left/pilot side is designated as PFD1, and the one installed on the right/copilot side is designated as PFD2. The unit installed in the center is designated the MFD. These units communicate with each other and with the on-side GIA 63W Integrated Avionics Unit through a High-Speed Data Bus (HSDB) connection. • GMA 1347D (2) – Integrates NAV/COM digital audio, intercom system and marker beacon controls, and is installed in dual configuration on the outboard side of PFD1 and PFD2. This unit also enables the manual control of the display reversionary mode (red DISPLAY BACKUP button) and communicates with the on-side GIA 63W, using an RS-232 digital interface. • GCU 475 (1) – Provides the Flight Management System (FMS) controls for the MFD through an RS-232 digital interface. • GMC 715 (1) – Provides the controls for the Garmin AFCS through an RS-232 digital interface allowing communication with both PFDs. 2 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW • GIA 63W (2) – Functions as the main communication hub, linking all LRUs with the on-side PFD. Each GIA 63W contains a GPS SBAS receiver, VHF COM/NAV/GS receivers, a flight director (FD) and system integration microprocessors. Each GIA 63W is paired with the on-side PFD via HSDB connection. The GIA 63Ws are not paired together and do not communicate with each other directly. • GDC 74B (2) – Processes data from the pitot/static system as well as the OAT probe. This unit provides pressure altitude, airspeed, vertical speed and OAT information to the system, and it communicates with the on-side GIA 63W, on-side GDU 1240A and on-side GRS 77, using an ARINC 429 digital interface. The GDC 74B is designed to operate in Reduced Vertical Separation Minimum (RVSM) airspace. • GEA 71 (3) – Receives and processes signals from the engine and airframe sensors. This unit communicates with both GIA 63Ws using an RS-485 digital interface. • GRS 77 (2) – Provides aircraft attitude and heading information via ARINC 429 to both the on-side GDU 1240A and the on-side GIA 63W. The GRS 77 contains advanced sensors (including accelerometers and rate sensors) and interfaces with the on-side GMU 44 to obtain magnetic field information, with the GDC 74B to obtain air data, and with both GIA 63Ws to obtain GPS information. AHRS modes of operation are discussed later in this document. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 3 SYSTEM OVERVIEW • GMU 44 (2) – Measures local magnetic field. Data is sent to the GRS 77 for processing to determine aircraft magnetic heading. This unit receives power directly from the GRS 77 and communicates with the GRS 77, using an RS-485 digital interface. • GTX 33 (1) and GTX 33D (1) – Solid-state transponders that provide Modes A/C/S capability and optional 1090 MHz Extended Squitter Automatic Dependent Serveillance (ADS-B out) transmission. The GTX 33D includes Mode S with diversity and is indicated as ‘XPDR2’. The GTX 33 is indicated as ‘XPDR1’. Both transponders can be controlled from either PFD, and only one transponder can be active at a time. Each transponder communicates with the on-side GIA 63W through an RS-232 digital interface. These transponders are not used when the TCAS II option is installed. • GDL 69A (1) – A satellite radio receiver that provides weather information to the MFD (and, indirectly, to the inset map of the PFD) as well as digital audio entertainment. The GDL 69A communicates with the MFD via HSDB connection. A subscription to the SiriusXM Satellite Radio service is required to enable the GDL 69A capability. • GDL 59 (1) – Provides system WI-FI connectivity. GDL 59 operation is performed with the MFD through the HSDB. Connectivity with the GSR 56 is through the RS-232 bus. Computers and/or EFBs (Electronic Flight Bag) may also be connected through three Ethernet ports. 4 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW • GDR 66 (1) – Provides Controller Pilot Data Link Communications (CPDLC) connectivity. The GDR66 is connected to the GSD 41 through the RS-422 bus. • GSR 56 (1) – The Iridium Transceiver operation for voice communication is by means of a telephone handset. The tranceiver can also send and receive data provided by the GDL 59 through the RS-232 bus. • GWX 68 (1) – Provides airborne weather and ground mapped radar data to the MFD, through the GSD 41, via HSDB connection. • GTS 850 (1) – The optional GTS 850 TCAS I uses active interrogations of Mode S and Mode C transponders to provide Traffic Advisories to the pilot independent of the air traffic control system. • GSD 41 (1) – This unit is a data concentrator used to expand the input and output capabilities of the system. Communication is through the High Speed Data Bus. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 5 SYSTEM OVERVIEW • GSA 81 (3) and GSM 86 (3) – The GSA 81 servos are used for the automatic control of pitch, roll, and yaw. These units interface with each GIA 63W. The GSM 86 servo gearbox is responsible for transferring the output torque of the GSA 81 servo actuator to the mechanical flight-control surface linkage. • GA 36 (1) and GA 37 (1) – The GA 36 is a through-mount GPS/SBAS antenna. The GA 37 is a through-mount GPS/SBAS antenna with SiriusXM/Data Link. GA 36 GA 37 • GA 58 – The optional GA 58 is directional antenna for the Traffic Avoidance System. One top-mounted directional antenna is required. Optional bottom mounted antenna offers better threat visibility. 6 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW GWX 68 GDR 66 GSD 41 GSR 56 GDL 69A GTS 850 (Optional) GDU 1240A (PFD #1) GDU 1240A GDL 59 (PFD #2) GCU 475 GDU 1240A (MFD) GMC 715 Normal Mode HSDB Rev Switch* MFD Failed Mode GMA 1347D #1 GMA 1347D #2 GMU 44 #1 GMU 44 #2 GRS 77 #1 GRS 77 #2 GIA 63W #1 GDC 74B #1 VHF COM VHF NAV/LOC GPS/WAAS G/S GDC 74B #2 VHF COM VHF NAV/LOC GPS/WAAS G/S GSA 81 AFCS Mode Logic Flight Director Servo Management GIA 63W #2 AFCS Mode Logic Flight Director Servo Management (Pitch) GSA 81 (Roll) GTX 33 GSA 81 GTX 33D (Yaw) GEA 71 #1 GEA 71 #2 GEA 71 #3 * External to the G1000 system High Speed Data Bus Figure 1-1 System LRU Configuration 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 7 SYSTEM OVERVIEW 1.3 PRODIGY® CONTROLS NOTE: The Audio Panel (GMA 1347D) and AFCS controls (GMC 715) are described in the CNS & Audio Panel and AFCS sections respectively. The system controls are located on the PFD and MFD bezels, MFD Control Unit, AFCS Control Unit and audio panel. Some controls found on the MFD are duplicated on the MFD Control Unit. These control functions may be operated from either the MFD or the MFD Control Unit. The controls for the PFDs and MFD are discussed within the following pages of this section. MFD/PFD CONTROLS 1 2 4 3 5 6 7 8 Figure 1-2 PFD Controls 9 13 10 14 11 15 12 8 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW The following list provides an overview of the controls located on the PFD and MFD bezels (see Figure 1-2). 1 NAV VOL/ID Knob – Controls NAV audio volume level. Press to toggle the Morse code identifier audio ON and OFF. Volume level is shown in the NAV frequency field as a percentage. 2 NAV Frequency Transfer Key – Switches the standby and active NAV frequencies. 3 Dual NAV Knob – Tunes the standby frequencies for the NAV receiver (large knob for MHz; small knob for kHz). Press to switch the tuning box (cyan box) between NAV1 and NAV2. 4 Joystick – Changes the map range when rotated. Activates the map pointer when pressed. 5 BARO Knob – Sets the altimeter barometric pressure. Press to enter standard pressure (29.92). 6 Dual COM Knob – Tunes the standby frequencies for the COM transceiver (large knob for MHz; small knob for kHz). Press to switch the tuning box (cyan box) between COM1 and COM2. 7 COM Frequency Transfer Key – Switches the standby and active COM frequencies. Press and hold this key for two seconds to tune the emergency frequency (121.5 MHz) automatically into the active frequency field. 8 COM VOL/SQ Knob – Controls COM audio volume level. Volume level is shown in the COM frequency field as a percentage. Press to turn the COM automatic squelch ON and OFF. 9 Direct-to Key – Allows the user to enter a destination waypoint and establish a direct course to the selected destination (the destination is either specified by the identifier, chosen from the active route, or taken from the map pointer position). 10 FPL Key – Displays the active Flight Plan Page for creating and editing the active flight plan. 11 CLR Key – Erases information, cancels entries, or removes page menus. 12 Dual FMS Knob – Flight Management System Knob. Press the FMS Knob to turn the selection cursor ON and OFF. When the cursor is ON, data may be entered in the applicable window by turning the small and large knobs. The large knob moves the cursor on the page, while the small knob selects individual characters for the highlighted cursor location. 13 MENU Key – Displays a context-sensitive list of options. This list allows the user to access additional features or make setting changes that relate to particular pages. 14 PROC Key – Gives access to IFR departure procedures (DPs), arrival procedures (STARs) and approach procedures (IAPs) for a flight plan. If a flight plan is used, available procedures for the departure and/or arrival airport are automatically suggested. These procedures can then be loaded into the active flight plan. If a flight plan is not used, both the desired airport and the desired procedure may be selected. 15 ENT Key – Validates or confirms a menu selection or data entry. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 9 SYSTEM OVERVIEW MFD CONTROL UNIT Many of the controls on the MFD Control Unit (GCU 475) have the same function as those located on the MFD. The following list provides an overview of the controls located on the MFD Control Unit (see Figure 1-3): 1 3 2 4 5 6 7 8 9 14 13 12 11 10 Figure 1-3 MFD Control Unit (GCU 475) 10 1 Dual FMS Knob – Flight Management System Knob. This knob selects the MFD page to be viewed; the large knob selects a page group (MAP, WPT, AUX, NRST), while the small knob selects a specific page within the page group. Pressing the FMS Knob turns the selection cursor ON and OFF. When the cursor is ON, data may be entered in the applicable window by turning the small and large knobs. In this case, the large knob moves the cursor on the page, while the small knob selects individual characters for the highlighted cursor location. 2 Direct-to Key – Allows the user to enter a destination waypoint and establish a direct course to the selected destination (the destination is either specified by the identifier, chosen from the active route, or taken from the map pointer position). 3 FPL Key – Displays the active Flight Plan Page for creating and editing the active flight plan, or for accessing stored flight plans. 4 MENU Key – Displays a context-sensitive list of options. This list allows the user to access additional features or make setting changes that relate to particular pages. 5 PROC Key – Gives access to IFR departure procedures (DPs), arrival procedures (STARs) and approach procedures (IAPs) for a flight plan. If a flight plan is used, available procedures for the departure and/or arrival airport are automatically suggested. Theses procedures can then be loaded into the active flight plan. If a flight plan is not used, both the desired airport and the desired procedure may be selected. 6 Joystick – Changes the map range when rotated. Activates the map pointer when pressed. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW 7 Alphanumeric Keys – Allow the user to enter data quickly, without having to select individual characters with the FMS Knob. 8 Plus (+) Minus (-) Key – Toggles a (+) or (-) character. 9 Decimal Key – Enters a decimal point. 10 SEL Key – The center of this key activates the selected softkey, while the right and left arrows move the softkey selection box to the right and left, respectively. 11 ENT Key – Validates or confirms a menu selection or data entry. 12 CLR Key – Erases information, cancels entries, or removes page menus. Pressing and holding this key displays the Navigation Map Page automatically. 13 SPC Key – Adds a space character. 14 BKSP Key – Moves the cursor back one character space. AFCS CONTROLS 1 20 2 3 19 18 17 4 16 5 6 15 14 7 8 9 10 13 12 11 Figure 1-4 AFCS Control Unit (GMC 715) The Garmin AFCS is mainly controlled through the GMC 715 AFCS Control Unit. The AFCS Control Unit consists of the following controls: 10 FD Key – Activates/deactivates the selected flight director (pilot- or copilot-side) in default vertical and lateral modes. Press the other FD Key to toggle the corresponding PFD’s Command Bars off/on. 2 NAV Key – Selects/deselects Navigation Mode. 3 HDG Key – Selects/deselects Heading Select Mode. 4 AP Key – Engages/disengages the autopilot. 1 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 11 SYSTEM OVERVIEW 5 YD Key – Engages/disengages the yaw damper. 6 ALT Key – Selects/deselects Altitude Hold Mode. 7 VNV Key – Selects/deselects Vertical Path Tracking Mode for Vertical Navigation flight control. 8 VS Key – Selects/deselects Vertical Speed Mode. 9 FLC Key – Selects/deselects Flight Level Change Mode. 20 CRS Knobs – Adjusts the Selected Course in 1° increments on the Horizontal Situation Indicator (HSI) of the corresponding PFD. Press to re-center the Course Deviation Indicator (CDI) and return course pointer directly TO the bearing of the active waypoint/station. 12 SPD SEL Knob – Adjusts the Airspeed Reference and bug in 1-kt (0.01 M) increments. Press to toggle the Airspeed Reference units from IAS to Mach. 13 UP/DN Wheel – Adjusts theVertical Speed Reference and bug in 100-fpm increments. 14 ALT SEL Knob – Adjusts the Selected Altitude and bug in 100-ft increments (a finer resolution of 10 feet is available under approach conditions). 15 CSC Key – Selects/deselects Current Speed Control (when Altitude Hold Mode is active)(if available). 16 CPL Key – Transfers selection between the active flight director and standby flight director. When the flight directors are switched, the modes revert to default. An arrow in the AFCS Status Box indicates the active FD (pilot- or copilot-side). 17 HDG SEL Knob – Adjusts the Selected Heading and bug in 1° increments on the HSI (both PFDs). Press to synchronize the Selected Heading to the current heading. 18 APR Key – Selects/deselects Approach Mode. 19 BANK Key – Manually selects/deselects Low Bank Mode. 11 ADDITIONAL AFCS CONTROLS The AP DISC (Autopilot Disconnect) Switch, CWS (Control Wheel Steering) Button, GO AROUND Switch, and MEPT (Manual Electric Pitch Trim) Switch are additional AFCS controls and are located in the cockpit, separately from the AFCS Control Unit. These are discussed in detail in the AFCS section. 12 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW AUDIO PANEL CONTROLS 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 Figure 1-5 Audio Panel Controls (GMA 1347D) NOTE: When a key is selected, a triangular annunciator above the key is illuminated. 1 COM1 MIC – Selects the #1 transmitter for transmitting. COM1 receive is simultaneously selected when this key is pressed allowing received audio from the the #1 Com receiver to be heard. COM2 receiver audio can be added by pressing the COM2 Key. 2 COM1 – When selected, audio from the #1 Com receiver can be heard. 3 COM2 MIC – Selects the #2 transmitter for transmitting. COM2 is simultaneously selected when this key is pressed allowing received audio from the the #2 Com receiver to be heard. COM2 can be deselected by pressing the COM2 Key, or COM1 can be added by pressing the COM1 Key. 4 COM2 – When selected, audio from the #2 Com receiver can be heard. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 13 SYSTEM OVERVIEW 14 5 COM3 MIC – Selects the #3 transmitter (HF) for transmitting. COM3 receive is simultaneously selected when this key is pressed allowing received audio from the #3 COM receiver to be heard. 6 COM3 – When selected, audio from the #3 COM receiver (HF) can be heard. 7 PA – Selects the passenger address system. The selected Com transmitter is deselected when the PA Key is pressed. 8 TEL – When selected, activates the SATCOM transceiver. 9 MUSIC – Turns the Music 1 input on or off. 10 SPKR – Pressing this key selects and deselects the corresponding cockpit speaker. Com and Nav receiver audio will be heard on the speaker. 11 MKR/MUTE – Mutes the currently received Marker Beacon Receiver audio. Unmutes when new marker beacon audio is received. 12 HI SENS – Press to increase Marker Beacon Receiver sensitivity. Press again to return to normal. 13 DME – Pressing turns DME audio on or off. 14 NAV1 – When selected, audio from the #1 Nav receiver can be heard. 15 ADF – Pressing turns on or off the audio from the ADF receiver, if installed. 16 NAV2 – When selected, audio from the #2 Nav receiver can be heard. 17 AUX – Turns optional DME 2 audio on or off. 18 MAN SQ – Pressing activates/deactivates intercom manual squelch operation. 19 PLAY – Press once to play the last recorded audio. Press during play to play the previously recorded memory block. Each subsequent press of the PLAY Key will begin playing the next previously recorded block. 20 INTR COM – Pressing selects/deselects the pilot/copilot intercom on both audio panels. 21 CABIN – Pressing activates/deactivates two-way communication between pilot/copilot and passengers. 22 ICS Knob – Turn to adjust intercom volume or squelch. Press to switch between volume and squelch control as indicated by the ‘VOL’ or ‘SQ’ being illuminated. The MAN SQ Key must be selected to allow squelch adjustment. 23 MSTR Knob – The Master Volume Control adjusts volume for the blended NAV, COM, and intercom audio. 24 Reversionary Mode Button – Pressing manually selects Reversionary Mode. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW SOFTKEY FUNCTION The softkeys are located along the bottoms of the displays. The softkeys shown depend on the softkey level or page being displayed. The bezel keys below the softkeys can be used to select the appropriate softkey. When a softkey is selected, its color changes to black text on gray background and remains this way until it is turned off, at which time it reverts to white text on black background. Softkey On Softkey Names (displayed) Bezel-Mounted Softkeys (press) Figure 1-6 Softkeys (Second-Level PFD Configuration) Another means of selecting softkeys on the MFD is by using the MFD Control Unit: Selecting a softkey using the MFD Control Unit 1) Move the softkey selection box to the desired softkey using the arrows of the SEL Key. 2) Press the center of the SEL Key to select the desired softkey. PFD SOFTKEYS The CDI, IDENT, TMR/REF, NRST, and MSG Softkeys undergo a momentary change to black text on gray background and automatically switch back to white text on black background when selected. If messages remain after acknowledgement, the MSG Softkey will be black on white. The PFD softkeys provide control over flight management functions, including GPS, NAV, terrain, traffic, and lightning (optional). Each softkey sublevel has a BACK Softkey which can be pressed to return to the previous level. The MSG Softkey is visible in all softkey levels. For the top level softkeys and the transponder (XPDR) levels, the IDENT Softkey remains visible. Level 1 CAS Level 2 CAS ↑ CAS ↓ INSET or TRFC/MAP OFF 190-00728-06 Rev. A Level 3 Level 4 Description Displays the scroll keys. Only displayed when the number of CAS messages exceeds the capacity of the display window. Scroll up CAS messages (Accessible only when the CAS Softkey is displayed) Scroll down CAS messages (Accessible only when the CAS Softkey is displayed) Displays Inset Map in PFD lower left corner. The TRFC/MAP Softkey is displayed when the TCAS II option is installed. Pressing the TRFC/MAP Softkey displays the Inset Map showing Traffic Map Page. Removes Inset Map Embraer Prodigy® Flight Deck 100 Pilot’s Guide 15 SYSTEM OVERVIEW Level 1 Level 2 DCLTR (3) Level 3 WX LGND TRAFFIC TOPO Description Selects desired amount of map detail; cycles through declutter levels: DCLTR (No Declutter): All map features visible DCLTR-1: Declutters land data DCLTR-2: Declutters land and SUA data DCLTR-3: Removes everything except for the active flight plan Displays icon and age on the Inset Map for the selected weather products (optional) Cycles through traffic display options: TRFC-1: Traffic displayed on inset map TRFC-2: Traffic Map Page is displayed in the inset map window Displays topographical data (e.g., coastlines, terrain, rivers, lakes) and elevation scale on Inset Map SYN TERR Displays terrain information on Inset Map (not available with TAWS-A) Displays NEXRAD weather and coverage information on Inset Map (optional feature) Displays SiriusXM Weather lightning information on Inset Map (optional feature) Displays METAR flags on airport symbols shown on the Inset Map Displays softkeys for selecting the #1 and #2 AHRS and Air Data Computers Selects the #1 Air Data Computer Selects the #2 Air Data Computer Selects the standby air data input Selects the #1 AHRS Selects the #2 AHRS Selects the standby attitude input. Heading input will come from the #1 AHRS. Displays second-level softkeys for additional PFD configurations Displays the softkeys for enabling or disabling Synthetic Vision features Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan Enables synthetic terrain depiction HRZN HDG Displays compass heading along the Zero-Pitch line TERRAIN NEXRAD XM LTNG METAR SENSOR ADC1 ADC2 ADCSTBY AHRS1 AHRS2 ATTSTBY PFD SYN VIS PATHWAY 16 Level 4 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW Level 1 Level 2 Level 3 APTSIGNS METERS Description Displays position markers for airports within approximately 15 nm of the current aircraft position. Airport identifiers are displayed when the airport is within approximately 9 nm. Resets PFD to default settings, including changing units to standard Displays softkeys to select wind data parameters Headwind/tailwind and crosswind arrows with numeric speed components Wind direction arrow with numeric speed Wind direction arrow with headwind/tailwind and crosswind speed components Information not displayed Displays the information window for DME number 1 Cycles the Bearing 1 Information Window through NAV1, GPS/ waypoint identifier and GPS-derived distance information. Provides access to the HSI formatting softkeys Displays the HSI in a 360 degree view Displays the HSI as an arc Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS-derived distance information. Displays the information window for DME number 2 Displays softkeys for setting the altimeter and BARO settings to metric units When enabled, displays altimeter in meters IN Press to display the BARO setting as inches of mercury HPA Press to display the BARO setting as hectopacals DFLTS WIND OPTN 1 OPTN 2 OPTN 3 OFF DME1 BRG1 HSI FRMT 360 HSI ARC HSI BRG2 DME2 ALT UNIT STD BARO OBS CDI ADF/DME Level 4 Sets barometric pressure to 29.92 in Hg (1013 hPa if metric units are selected) Selects OBS mode on the CDI when navigating by GPS (only available with active leg) Cycles through GPS, VOR1 (LOC1), and VOR2 (LOC2) navigation source on the CDI Displays the ADF/DME Tuning Window, providing ADF tuning capability and allowing selection of the NAV source for tuning each DME Transponder Softkeys without TCAS II Option 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 17 SYSTEM OVERVIEW Level 1 XPDR Level 2 Level 3 XPDR1 XPDR2 STBY ON ALT GND VFR CODE 0—7 BKSP IDENT TMR/REF NRST MSG XPDR/TFC MODE 18 Level 4 Description Displays transponder mode selection softkeys Selects the #1 transponder as active Selects the #2 transponder as active Selects standby mode (transponder does not reply to any interrogations) Selects Mode A (transponder replies to identification interrogations) Selects Mode C – altitude reporting mode (transponder replies to identification and altitude interrogations) Manually selects Ground Mode, the transponder does not allow Mode A and Mode C replies, but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations (not available with TCAS II) Automatically enters the VFR code (1200 in the U.S.A. only)(not avialable with TCAS II) Displays transponder code selection softkeys 0-7 Use numbers to enter code Removes numbers entered, one at a time Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen Displays Timer/References Window Displays Nearest Airports Window Displays Messages Window Transponder/Traffic Softkeys with TCAS II Option Displays the transponder and TCAS II system selection softkeys Displays transponder mode selection softkeys Selects transponder Standby Mode (transponder STBY does not reply to any interrogations). When the transponder is set to standby, the TCAS II system is also set to standby. Activates transponder (transponder replies to ON identification interrogations). When the transponder is set to ON, the TCAS II system is set to standby. Altitude Reporting Mode (transponder replies to ALT identification and altitude interrogations). When the transponder is set to ALT, the TCAS II system is set to standby. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW Level 1 Level 2 Level 3 TA ONLY TA/RA BACK TCAS REL ABS ALT RNG TEST BACK CODE 0—7 IDENT BKSP IDENT TMR/REF NRST MSG 190-00728-06 Rev. A Level 4 Description Activates the TCAS II system in TA Only Mode and sets the transponder to ALT Activates the TCAS II system in TA/RA Mode and sets the transponder to ALT Returns to the previous softkey level Displays the TCAS control softkeys Displays intruder altitude as altitude relative to own aircraft altitude Displays intruder MSL altitude Displays the altitude display range softkeys Displays non-threat traffic from 9900 feet above the ABOVE aircraft to 2700 feet below the aircraft. Typically used during climb phase of flight. NORMAL Displays non-threat traffic from 2700 feet above the aircraft to 2700 feet below the aircraft. Typically used during enroute phase of flight. Displays non-threat traffic from 2700 feet above the BELOW aircraft to 9900 feet below the aircraft. Typically used during descent phase of flight. UNREST All traffic is displayed Activates Test Mode and displays test intruder symbols Returns to the previous softkey level Displays transponder code selection softkeys 0-7 Use numbers to enter code Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen Removes numbers entered, one at a time Activates the Special Position Identification (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen Displays Timer/References Window Displays Nearest Airports Window Displays Messages Window Embraer Prodigy® Flight Deck 100 Pilot’s Guide 19 SYSTEM OVERVIEW (optional TCAS II) (optional TCAS II) TRFC/MAP XPDR/TFC ADF/DME CAS Figure 1-7 Top Level PFD Softkeys ADF/DME CAS Select the BACK Softkey on this level to return to the top softkey level. CAS ↑ CAS ↓ BACK Figure 1-8 CAS Softkeys ADF/DME CAS METAR WX LGND TRFC-1 Select the BACK or OFF Softkey to return to the top-level softkeys. TRFC-2 Figure 1-9 INSET Map Softkeys ADF/DME CAS Press the BACK Softkey to return to the top level softkeys. ADC1 ADC2 ADCSTBY AHRS1 AHRS2 ATTSTBY BACK MSG Figure 1-10 SENSOR Softkeys 20 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW ADF/DME CAS SYN VIS DME1 DME2 HSI FMT NAV1 NAV2 GPS GPS OFF OFF 360 HSI Select the BACK Softkey to return to the top-level softkeys BACK ARC HSI METERS PATHWAY ALT UNIT IN HPA SYN TERR HRZN HDG APTSIGNS Figure 1-11 PFD Configuration Softkeys CAS ADF/DME Press the BACK Softkey to return to the top-level softkeys. MSG Selecting BACK returns to the previous softkey level. MSG Figure 1-12 XPDR Softkeys (without TCAS II) 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 21 SYSTEM OVERVIEW CAS TRFC/MAP SENSOR PFD OBS CDI (optional) ADF/DME XPDR/TFC IDENT TMR/REF NRST MSG Press the BACK Softkey to return to the top-level softkeys. MODE TCAS CODE BACK IDENT MSG Selecting BACK returns to the previous softkey level. REL ABS ALT RNG TEST BACK MSG Selecting BACK returns to the previous softkey level. ABOVE NORMAL BELOW UNREST BACK MSG Selecting BACK returns to the previous softkey level. STBY ON ALT TA ONLY BACK TA/RA MSG Selecting BACK returns to the previous softkey level. 0 1 2 3 4 5 6 7 IDENT BKSP BACK MSG Figure 1-13 XPDR Softkeys (with TCAS II) MFD SOFTKEYS Level 1 SYSTEM Level 2 ENG SET LFE 22 Level 3 Description Accesses EIS softkeys Accesses the FADEC settings softkeys; displays the Takeoff Data Set Window when aircraft is parked or taxiing Selects the continuous thrust rating. Disabled when aircraft is on CON the ground. Selects the maximum climb thrust rating. Disabled when aircraft is CLB on the ground. Increases the takeoff outside air temperature setting in one-degree OAT ↑ Celsius increments. Disabled when aircraft is in the air. Decreases the takeoff outside air temperature setting in one-degree OAT ↓ Celsius increments. Disabled when aircraft is in the air. ATR ON Enables Automatic Thrust Reserve (ATR). Disabled when aircraft is in the air. ATR OFF Disables Automatic Thrust Reserve (ATR). Disabled when aircraft is in the air. Returns display to previous softkey level BACK ACCEPT Confirms the selected takeoff settings Accesses softkeys for manually setting the Landing Field Elevation (LFE) Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW Level 1 Level 2 STATUS ECS ELEC FUEL ICEPROT ENG MNT BACK CPDLC SYSTEM CPDLC LOGON LOGOFF NEW DELETE DEL ALL BACK MAP TRAFFIC PROFILE TOPO TERRAIN AIRWAYS (Default label is dependant on map setup option selected) 190-00728-06 Rev. A Level 3 FMS LFE +500 FT -500 FT +50 FT -50 FT ACCEPT BACK Description Sets current flight plan destination elevation as displayed LFE Increases currently displayed LFE value by 500 ft Decreases currently displayed LFE value by 500 ft Increases currently displayed LFE value by 50 ft Decreases currently displayed LFE value by 50 ft Confirms the LFE setting and returns to the previous softkey level Returns display to previous softkey level Displays the System-Status Page Displays the System-ECS (Environmental Control System) Page Displays the System-Electrical Page Displays the System-Fuel Page Displays the System-Deice Page Displays the Engine Maintenance Page. Enabled only while aircraft is on the ground and engines are off. Returns display to previous softkey level Accesses theCPDLC softkeys Accesses EIS softkeys Accesses CPDLC softkeys Displays Logon screen for the CPDLC system Logs off the CPDLC system Accesses New CPDLC message screen Delete selected CPDLC message. Delete all CPDLC messages. Returns display to previous softkey level Enables second-level Navigation Map softkeys Displays traffic information on Navigation Map Displays/removes Profile View on Navigation Map Page (optional) Displays topographical data (e.g., coastlines, terrain, rivers, lakes) and elevation scale on Navigation Map Displays terrain information on Navigation Map Displays airways on the map; cycles through the following: AIRWAYS: No airways are displayed AIRWY ON: All airways are displayed AIRWY LO: Only low altitude airways are displayed AIRWY HI: Only high altitude airways are displayed Embraer Prodigy® Flight Deck 100 Pilot’s Guide 23 SYSTEM OVERVIEW Level 1 Level 2 NEXRAD or PRECIP XM LTNG or Description Displays NEXRAD weather and coverage information on the Navigation Map (optional) Displays Connext precipitation on Navigation Map (optional) Displays SiriusXM Weather lightning information on the Navigation Map (optional) DL LTNG Displays Connext Worldwide Weather lightning information on the Navigation Map (optional) METAR LEGEND Displays METAR flags on airport symbols Displays the legend for the selected weather products. Available only when NEXRAD, XM LTNG, and/or METAR softkeys are selected. Displays Color Weather Radar images on the Navigation Map (optional) Returns to top-level softkeys Selects desired amount of map detail; cycles through declutter levels: DCLTR (No Declutter): All map features visible DCLTR-1: Declutters land data DCLTR-2: Declutters land and SUA data DCLTR-3: Removes everything except the active flight plan When available, displays optional airport and terminal procedure charts When available, displays optional checklists WX RADAR BACK DCLTR (3) SHW CHRT CHKLIST SYSTEM Level 3 (optional) CPDLC (optional) MAP DCLTR SHW CHRT (optional) CHKLST DCLTR-1 DCLTR-2 DCLTR-3 Figure 1-14 Top Level MFD Softkeys 24 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW (optional) CPDLC SYSTEM ENG SET MAP LFE STATUS FMS LFE +500 FT CON (optional) (optional) SHW CHRT CHKLST DCLTR CLB ECS -500 FT +50 FT OAT ↑ OAT ↓ ELEC FUEL ICEPROT ENG MNT -50 FT ATR ON ENGINE ATR OFF BACK ACCEPT BACK BACK ACCEPT DONE EXIT EMERGCY The DONE Softkey label changes to UNDO when the checklist item is already checked. Figure 1-15 SYSTEM and CHKLST Softkeys SYSTEM (optional) CPDLC (optional) DCLTR MAP SHW CHRT (optional) CHKLST DCLTR-1 DCLTR-2 PROFILE (optional) PRECIP DL LTNG or (optional) TRAFFIC (optional) TOPO TERRAIN AIRWAYS NEXRAD or XM LTNG DCLTR-3 (optional) METAR LEGEND WX RADAR BACK Select the BACK Softkey on this level to return to the top softkey level. AIRWY ON AIRWY LO AIRWAY HI CPDLC LOGON LOGOFF NEW DELETE DEL ALL BACK Figure 1-16 CPDLC and MAP Softkeys 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 25 SYSTEM OVERVIEW 1.4 SECURE DIGITAL CARDS NOTE: DO NOT use the database SD cards for any purpose other than database storage. NOTE: Refer to the Appendices for instructions on updating databases. NOTE: Ensure that the system is powered off before inserting the SD card. The GDU 1240A data card slots use Secure Digital (SD) cards and are located on the top right portion of the display bezels. Each display bezel is equipped with two SD card slots. SD cards are used for the various databases and system software updates as well as terrain database storage. Not all SD cards are compatible with the Prodigy® system. Use only SD cards supplied by Garmin or the aircraft manufacturer. Install an SD card Insert the SD card in the SD card slot, pushing the card in until the spring latch engages. The front of the card should remain flush with the face of the display bezel. Remove an SD card Gently press on the SD card to release the spring latch and eject the card. SD Card Slots Figure 1-17 Display Bezel SD Card Slots 26 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW 1.5 SYSTEM POWER-UP NOTE: Refer to the Appendices for AHRS initialization bank angle limitations. NOTE: See the Appendices for additional information regarding system-specific annunciations and alerts. NOTE: See the Airplane Flight Manual (AFM) for specific procedures concerning avionics power application and emergency power supply operation. The system is integrated with the aircraft electrical system and receives power directly from electrical busses. The PFDs, MFD and supporting sub-systems include both power-on and continuous built-in test features that exercise the processor, RAM, ROM, external inputs and outputs to provide safe operation. During system initialization, test annunciations are displayed, as shown in Figure 1-18. All system annunciations should disappear typically within one minute of power-up. Upon power-up, key annunciator lights also become momentarily illuminated on the audio panels, the control units and the display bezels. On the PFD, the AHRS begins to initialize and displays ‘AHRS ALIGN: Keep Wings Level’. The AHRS should display valid attitude and heading fields typically within one minute of power-up. The AHRS can align itself both while taxiing and during level flight. When the MFD powers up (Figure 1-19), the MFD Power-up Page displays the following information: • System version • Airport Terrain database name and version • Copyright • Obstacle database name and version • Land database name and version • Navigation database name, version, and effective dates • Safe Taxi database information • Airport Directory name, version and effective dates • Terrain database name and version • FliteCharts/ChartView database information Current database information includes the valid operating dates, cycle number and database type. When this information has been reviewed for currency (to ensure that no databases have expired), the pilot is prompted to continue. Pressing the ENT Key acknowledges this information and displays the System - Status Page. Figure 1-18 PFD Initialization 190-00728-06 Rev. A Figure 1-19 MFD Power-up Page Embraer Prodigy® Flight Deck 100 Pilot’s Guide 27 SYSTEM OVERVIEW 1.6 SYSTEM OPERATION The displays are connected via a single Ethernet bus, thus allowing for high-speed communication. As shown in Figure 1-1. The GIA 63W #1 is connected to PFD1 and GIA 63W #2 is connected to the HSDB switch. This section discusses the normal and reversionary modes of operation as well as the various AHRS modes of the system. In the event of display failure, the display modes are as follows: • PFD1 failure – MFD enters reversionary mode; PFD2 remains in normal mode. • MFD failure – PFD1 and PFD2 enter reversionary mode. • PFD2 failure – PFD1 and the MFD remain in normal mode. NORMAL OPERATION PFD In normal mode, the PFD presents graphical flight instrumentation (attitude, heading, airspeed, altitude and vertical speed), thereby replacing the traditional flight instrument cluster. The PFD also offers control for COM and NAV frequency selection. MFD In normal mode, the right portion of the MFD displays a full-color moving map with navigation information, while the left portion of the MFD is dedicated to engine, fuel, electrical, cabin pressurization, oxygen, landing gear, and trim/flaps indication. Figure 1-20 gives an example of the system displays in normal mode. PFD1 MFD PFD2 Figure 1-20 Normal Operation 28 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW REVERSIONARY MODE NOTE: The system alerts the pilot when backup paths are utilized by the LRUs. Refer to the Appendices for further information regarding system-specific alerts. Reversionary mode is a mode of operation in which all important flight information is presented identically on at least one of the remaining displays (see Figure 1-21). Transition to reversionary mode should be straightforward for the pilot, for flight parameters are presented in the same format as in normal mode. Figure 1-21 Reversionary Mode Reversionary mode is activated by pressing the dedicated DISPLAY BACKUP button at the bottom of the audio panel (see Figure 1-22 and refer to the Audio Panel section for further details). Pressing this button again deactivates reversionary mode. Pressing the DISPLAY BACKUP button activates/ deactivates reversionary mode for both the on-side PFD and the MFD. Figure 1-22 DISPLAY BACKUP Button Each display can be configured to operate in reversionary mode, as follows: • PFD1 – By pressing the DISPLAY BACKUP button on the left audio panel. • MFD – By pressing the DISPLAY BACKUP button on the left or the right audio panel. • PFD2 – By pressing the DISPLAY BACKUP button on the right audio panel. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 29 SYSTEM OVERVIEW AHRS OPERATION NOTE: Refer to the Appendices for specific AHRS alert information. NOTE: Aggressive maneuvering while the AHRS is not operating normally can degrade AHRS accuracy. In addition to using internal sensors, the GRS 77 AHRS uses GPS information, magnetic field data and air data to assist in attitude/heading calculations. In normal mode, the AHRS relies upon GPS and magnetic field measurements. If either of these external measurements is unavailable or invalid, the AHRS uses air data information for attitude determination. Four AHRS modes of operation are available (see Figure 1-23) and depend upon the combination of available sensor inputs. Loss of air data, GPS, or magnetometer sensor inputs is communicated to the pilot by message advisory alerts. YES NO Mag Data AND Air Data Available and Reliable? NO YES Mag Data Available and Reliable? NO YES GPS Data Available and Reliable? AHRS Normal Mode NO YES Air Data Available and Reliable? AHRS no-Mag Mode AHRS no-Mag/ no-Air Mode Heading Invalid Heading Invalid AHRS no-GPS Mode AHRS coast-on-gyros until invalid Attitude/Heading Invalid Figure 1-23 AHRS Operation The AHRS (GRS 77) corrects for shifts and variations in the Earth’s magnetic field by applying the Magnetic Field Variation Database. The Magnetic Field Variation Database is derived from the International Geomagnetic Reference Field (IGRF). The IGRF is a mathematical model that describes the Earth’s main magnetic field and its annual rate of change. The database is updated approximately every five years. See the Appendices for information on updating the Magnetic Field Variation Database. The system will prompt the pilot on startup when an update is available. Failure to update this database could lead to erroneous heading information being displayed to the pilot. 30 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW GPS INPUT FAILURE NOTE: In-flight initialization of AHRS, when operating without any valid source of GPS data and at true air speed values greater than approximately 200 knots, is not guaranteed. Under these rare conditions, it is possible for in-flight AHRS initialization to take an indefinite amount of time which would result in an extended period of time where valid AHRS outputs are unavailable. The system provides two sources of GPS information. If a single GPS receiver fails, or if the information provided from one of the GPS receivers is unreliable, the AHRS seamlessly transitions to using the other GPS receiver. An alert message informs the pilot of the use of the backup GPS path. If both GPS inputs fail, the AHRS continues to operate in reversionary No-GPS mode so long as the air data and magnetometer inputs are available and valid. AIR DATA INPUT FAILURE A failure of the air data input has no effect on AHRS output while AHRS is operating in normal mode. A failure of the air data input while the AHRS is operating in reversionary No-GPS mode results in invalid attitude and heading information on the PFD (as indicated by red “X” flags). MAGNETOMETER FAILURE If the magnetometer input fails, the AHRS transitions to one of the reversionary No-Magnetometer modes and continues to output valid attitude information. However, if the aircraft is airborne, the heading output on the PFD does become invalid (as indicated by a red “X”). PRODIGY® SYSTEM ANNUNCIATIONS NOTE: For a detailed description of all annunciations and alerts, refer to Appendix A. Refer to the Airplane Flight Manual (AFM) for additional information regarding pilot responses to these annunciations. When an LRU or an LRU function fails, a large red “X” is typically displayed on windows associated with the failed data (Figure 1-24 displays all possible flags and responsible LRUs). Upon system power-up, certain windows remain invalid as equipment begins to initialize. All windows should be operational within one minute of powerup. If any window remains flagged, the system should be serviced by a Garmin-authorized repair facility. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 31 SYSTEM OVERVIEW GIA 63W Integrated Avionics Units GIA 63W Integrated Avionics Units GDC 74B Air Data Computer FADEC GRS 77 AHRS Or GMU 44 Magnetometer GEA 71 Engine Airframe Unit KRA 405B Radar Altimeter or GIA 63W Integrated Avionics Units Pressure Controller GEA 71 Engine Airframe Unit & GSD 71 Data Concentrator GIA 63W Integrated Avionics Units & GEA 71 Engine Airframe Unit GIA 63W Integrated Avionics Units FADEC GDC 74B Air Data Computer GTX 33/D Transponder Or GIA 63W Integrated Avionics Units Figure 1-24 System Failure Annunciations GPS RECEIVER OPERATION Each GIA 63W Integrated Avionics Unit (GIA) contains a GPS receiver. Information collected by the specified receiver (GPS1 for the #1 GIA or GPS2 for the #2 GIA) may be viewed on the AUX - GPS Status Page. GPS1 provides information to the pilot-side PFD and GPS2 provides data to the copilot-side PFD. Internal system checking is performed to ensure both GPS receivers are providing accurate data to the PFDs. In some circumstances, both GPS receivers may be providing accurate data, but one receiver may be providing a better GPS solution than the other receiver. In this case the GPS receiver producing the better solution will be automatically coupled to both PFDs. “BOTH ON GPS 1” or “BOTH ON GPS 2” will then be displayed in the Reversionary Sensor Window (see Appendix A) indicating which GPS receiver is being used. Both GPS receivers are still functioning properly, but one receiver is performing better than the other at that particular time. These GPS sensor annunciations are most often seen after system power-up when one GPS receiver has acquired satellites before the other, or one of the GPS receivers has not yet acquired an SBAS (Satellite Based Augmentation System) signal. While the aircraft is on the ground, the SBAS signal may be blocked by obstructions causing one GPS receiver to have difficulty acquiring a good signal. Also, while airborne, turning the aircraft may result in one of the GPS receivers temporarily losing the SBAS signal. If the sensor annunciation persists, check for a system failure message in the Messages Window on the PFD. If no failure message exists, check the GPS Status Page and compare the information for GPS1 and GPS2. Discrepancies may indicate a problem. 32 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW Viewing GPS receiver status information: 1) Use the large FMS Knob on the MFD to select the Auxiliary Page Group (see Section 1.7 for information on navigating MFD page groups). 2) Use the small FMS Knob to select GPS Status Page. Selecting the GPS receiver for which data may be reviewed: 1) Use the FMS Knob to select the AUX - GPS Status Page. 2) To change the selected GPS receiver: a) Press the desired GPS Softkey. Or: a) Press the MENU Key. b) Use the FMS Knob to highlight the receiver which is not selected and press the ENT Key. Satellite Constellation Diagram Satellite Signal Information Status GPS Receiver Status RAIM Availability Prediction Enabled SBAS Options Satellite Signal Strength Bars GPS Selection Softkeys RAIM Softkey Selected SBAS Softkey Selected Figure 1-25 GPS Status Page (RAIM or SBAS Selected) 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 33 SYSTEM OVERVIEW The GPS Status Page provides the following information: • Satellite constellation diagram Satellites currently in view are shown at their respective positions on a sky view diagram. The sky view is always in a north-up orientation, with the outer circle representing the horizon, the inner circle representing 45° above the horizon, and the center point showing the position directly overhead. Each satellite is represented by an oval containing the Pseudo-random noise (PRN) number (i.e., satellite identification number). Satellites whose signals are currently being used are represented by solid ovals. • Satellite signal information status The accuracy of the aircraft’s GPS fix is calculated using Estimated Position Uncertainty (EPU), Dilution of Precision (DOP), and horizontal and vertical figures of merit (HFOM and VFOM). EPU is the radius of a circle centered on an estimated horizontal position in which actual position has 95% probability of laying. EPU is a statistical error indication and not an actual error measurement. DOP measures satellite geometry quality (i.e., number of satellites received and where they are relative to each other) on a range from 0.0 to 9.9, with lower numbers denoting better accuracy. HFOM and VFOM, measures of horizontal and vertical position uncertainty, are the current 95% confidence horizontal and vertical accuracy values reported by the GPS receiver. The current calculated GPS position, time, altitude, ground speed, and track for the aircraft are displayed below the satellite signal accuracy measurements. • GPS receiver status The selected GPS receiver is indicated for the pilot and copilot display. The GPS solution type (ACQUIRING, 2D NAV, 2D DIFF NAV, 3D NAV, 3D DIFF NAV) for the active GPS receiver (GPS1 or GPS2) is shown in the upper right of the GPS Status Page. When the receiver is in the process of acquiring enough satellite signals for navigation, the receiver uses satellite orbital data (collected continuously from the satellites) and last known position to determine the satellites that should be in view. ACQUIRING is indicated as the solution until a sufficient number of satellites have been acquired for computing a solution. When the receiver is in the process of acquiring a 3D navigational GPS solution, 3D NAV is indicated as the solution until the 3D differential fix has finished acquisition. SBAS (Satellite-Based Augmentation System) will indicate INACTIVE. When acquisition is complete, the solution status will indicate 3D DIFF NAV and SBAS will indicate ACTIVE. • RAIM (Receiver Autonomous Integrity Monitoring) Prediction (RAIM Softkey is selected) In most cases performing a RAIM prediction will not be necessary. However, in some cases, the selected approach may be outside the SBAS coverage area and it may be necessary to perform a RAIM prediction for the intended approach. Receiver Autonomous Integrity Monitoring (RAIM) is a GPS receiver function that performs a consistency check on all tracked satellites. RAIM ensures that the available satellite geometry allows the receiver to calculate a position within a specified RAIM protection limit (2.0 nautical miles for oceanic and enroute, 1.0 nm for terminal, and 0.3 nm for non-precision approaches). During oceanic, enroute, and terminal phases of flight, RAIM is available nearly 100% of the time. 34 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW The RAIM prediction function also indicates whether RAIM is available at a specified date and time. RAIM computations predict satellite coverage within ±15 min of the specified arrival date and time. Because of the tighter protection limit on approaches, there may be times when RAIM is not available. The system automatically monitors RAIM and warns with an alert message when it is not available. If RAIM is not predicted to be available for the final approach course, the approach does not become active, as indicated by the messages “Approach is not active” and “RAIM not available from FAF to MAP”. If RAIM is not available when crossing the FAF, the missed approach procedure must be flown. Predicting RAIM availability: 1) Select the GPS Status Page. 2) If necessary, select the RAIM Softkey. 3) Press the FMS Knob. The ‘WAYPOINT’ field is highlighted. 4) Turn the small FMS Knob to display the Waypoint Information Window. 5) Enter the desired waypoint: a) Use the FMS Knob to enter the desired waypoint by identifier, facility, or city name and press the ENT Key. Refer to Section 1.7 for instructions on entering alphanumeric data into the system. Or: a) Use the large FMS Knob to scroll to the Most Recent Waypoints List. b) Use the small FMS Knob to highlight the desired waypoint in the list and press the ENT Key. The system automatically fills in the identifier, facility, and city fields with the information for the selected waypoint. c) Press the ENT Key to accept the waypoint entry. Or: a) To use the present position, press the MENU Key. b) With ‘Set WPT to Present Position’ highlighted, press the ENT Key. c) Press the ENT Key to accept the waypoint entry. 6) Use the FMS Knob to enter an arrival time and press the ENT Key. 7) Use the FMS Knob to enter an arrival date and press the ENT Key. 8) With the cursor highlighting ‘COMPUTE RAIM?’, press the ENT Key. Once RAIM availability is computed, one of the following is displayed: • ‘COMPUTE RAIM?’—RAIM has not been computed for the current waypoint, time, and date combination • ‘COMPUTING AVAILABILITY’—RAIM calculation in progress • ‘RAIM AVAILABLE’—RAIM is predicted to be available for the specified waypoint, time, and date • ‘RAIM NOT AVAILABLE’—RAIM is predicted to be unavailable for the specified waypoint, time, and date Predicting RAIM availability at present position 1) Select the GPS Status Page. 2) If necessary, select the RAIM Softkey. 3) Press the FMS Knob. The ‘WAYPOINT’ field is highlighted. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 35 SYSTEM OVERVIEW 4) Press the MENU Key. 5) With ‘Set WPT to Present Position’ highlighted, press the ENT Key. 6) Press the ENT Key to accept the waypoint entry. 7) Use the FMS Knob to enter an arrival time and press the ENT Key. 8) Use the FMS Knob to enter an arrival date and press the ENT Key. 9) With the cursor highlighting ‘COMPUTE RAIM?’, press the ENT Key. Once RAIM availability is computed, one of the following is displayed: • ‘COMPUTE RAIM?’—RAIM has not been computed for the current waypoint, time, and date combination • ‘COMPUTING AVAILABILITY’—RAIM calculation in progress • ‘RAIM AVAILABLE’—RAIM is predicted to be available for the specified waypoint, time, and date • ‘RAIM NOT AVAILABLE’—RAIM is predicted to be unavailable for the specified waypoint, time, and date • SBAS Selection (SBAS Softkey is pressed)(WAAS, EGNOS, or MSAS capable systems only) In certain situations, such as when the aircraft is outside or on the fringe of the WAAS, EGNOS, or MSAS coverage area, it may be desirable to disable the reception of the applicable SBAS signal (although it is not recommended). When disabled, the SBAS field in the GPS Status box indicates DISABLED. There may be a small delay for the GPS Status box to be updated upon WAAS, EGNOS, and MSAS enabling/disabling. Disabling WAAS, EGNOS or MSAS 1) Select the GPS Status Page. 2) If necessary, select the SBAS Softkey. 3) Press the FMS Knob, and turn the large FMS Knob to highlight the desired SBAS system. 4) Press the ENT Key to uncheck the box. 5) Press the FMS Knob to remove the cursor. • GPS Satellite Signal Strengths The GPS Status Page can be helpful in troubleshooting weak (or missing) signal levels due to poor satellite coverage or installation problems. As the GPS receiver locks onto satellites, a signal strength bar is displayed for each satellite in view, with the appropriate satellite PRN number (01-32 or 120-138 for WAAS) below each bar. The progress of satellite acquisition is shown in three stages, as indicated by signal bar appearance: - No bar—Receiver is looking for the indicated satellite - Hollow bar—Receiver has found the satellite and is collecting data - Light blue bar—Receiver has collected the necessary data and the satellite signal can be used - Green bar—Satellite is being used for the GPS solution - Checkered bar—Receiver has excluded the satellite (Fault Detection and Exclusion) - “D” indication—Denotes the satellite is being used as part of the differential computations Each satellite has a 30-second data transmission that must be collected (signal strength bar is hollow) before the satellite may be used for navigation (signal strength bar becomes solid). 36 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW 1.7 ACCESSING SYSTEM FUNCTIONALITY MENUS The system has a MENU Key that, when pressed, displays a context-sensitive list of options. This options list allows the user to access additional features or make settings changes which specifically relate to the currently displayed window/page. There is no all-encompassing menu. Some menus provide access to additional submenus that are used to view, edit, select, and review options. Menus display ‘NO OPTIONS’ when there are no options for the window/page selected. The main controls used in association with all window/page group operations are described in section 1.3. Softkey selection does not display menus or submenus. Navigating the Page Menu Window: 1) Press the MENU Key to display the Page Menu Window. 2) Turn the FMS Knob to scroll through a list of available options (a scroll bar appears to the right of the window when the option list is longer than the window). 3) Press the ENT Key to select the desired option. 4) The CLR Key may be pressed to remove the menu and cancel the operation. Pressing the FMS Knob also removes the displayed menu. No Options with NRST Window Displayed on the PFD Options with FPL Window Displayed Figure 1-26 Page Menu Examples MFD PAGE GROUPS NOTE: Refer to other supporting sections in this Pilot’s Guide for details on specific pages. Information on the MFD is presented on pages which are grouped according to function. The page group and active page title are displayed in the upper center of the screen, below the Navigation Status Box. In the bottom right corner of the screen, a page group window is displayed by turning either FMS Knob. The page group tabs are displayed along the bottom of the window. The page titles are displayed in a list above the page group tabs. The current page group and current page within the group are shown in light blue. For some of these pages (Airport/Procedures/Weather Information, XM, Procedure Loading), the active title of the page changes while the page name in the list remains the same. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 37 SYSTEM OVERVIEW Active Page Title Page Group MFD Pages in Current Group Page Groups Figure 1-27 Page Title and Page Groups The main page groups are navigated using the FMS Knob; specific pages within each group can vary depending on the configuration of optional equipment. Selecting a page using the FMS Knob: 1) Turn the large FMS Knob to display the list of page groups; continue turning the large FMS Knob until the desired page group is selected 2) Turn the small FMS Knob to display the desired page within a specific page group. There are also several pages (Airport/Procedures/Weather Information and XM pages) which are selected first from within a main page group with the FMS Knob, then with the appropriate softkey at the bottom of the page (or from the page menu). In this case, the page remains set to the selected page until a different page softkey is selected, even if a different page group is selected. 38 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW Map Pages (MAP) Navigation Map Traffic Map Weather Radar (optional) XM Weather Data Link or Weather Data Link (CNXT) (service optional) TAWS-B/TAWS-A (TAWS-A optional) Figure 1-28 Map Pages Waypoint Pages (WPT) Airport Information pages - Airport Information (INFO-1 Softkey) - Airport Directory (INFO-2 Softkey) - Departure Information (DP Softkey) - Arrival Information (STAR Softkey) - Approach Information (APR Softkey) - Weather Information (WX Softkey) Intersection Information NDB Information Airport Information Pages VOR Information User Waypoint Information Figure 1-29 Waypoint Pages 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 39 SYSTEM OVERVIEW Auxiliary Pages (AUX) Weight Planning Trip Planning Utility GPS Status System Setup XM Radio Satellite Phone Pages - XM Information (INFO Softkey) - XM Radio (RADIO Softkey) Satellite Phone - Telephone (TEL Softkey) - SMS (SMS Softkey) XM Satellite Pages Data Link Maintenance Logs System Status Figure 1-30 Auxiliary Pages The Flight Plan Pages may also be accessed using the FPL Key on the MFD. 40 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW Flight Plan Pages (FPL) Active Flight Plan - Wide View, Narrow View (VIEW Softkey) Flight Plan Catalog or Stored Flight Plan (NEW Softkey) Figure 1-31 Flight Plan Pages System Pages (SYS) System Status Environmental Control System Electrical System Fuel System Ice Protection System Engine Maintenance Figure 1-32 System Pages The Checklist Page may be accessed from the page group tab or the CHKLIST Softkey. See the Additional Features section for a discussion on using the Checklist Page. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 41 SYSTEM OVERVIEW Nearest Pages (NRST) Nearest Airports Nearest Intersections Nearest NDB Nearest VOR Nearest User Waypoints Nearest Frequencies Nearest Airspaces Figure 1-33 Nearest Pages In addition to the page groups previously addressed, there are pages for loading procedures which are accessed by pressing the PROC Key on the MFD bezel. In some instances, softkeys may be used to access the Procedure Pages. A menu is initialized, and when a departure, approach, or arrival is selected, the appropriate Procedure Loading Page is opened. Turning the FMS Knob does not scroll through the Procedure pages. Procedure Pages (PROC) Departure Loading Arrival Loading Approach Loading Figure 1-34 Procedure Pages For some of these pages (Airport Information pages, XM Satellite pages, Procedure pages), the title of the page may change. 42 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW The CPDLC page is accessed by selecting the CPDLC Softkey on MFD. CPDLC Page (CPDLC Softkey) Figure 1-35 CPDLC Page MFD SYSTEM PAGES In the Auxiliary (AUX) Page Group, there are two system pages: System Setup and System Status. The System Setup Page allows management of various system parameters, while the System Status Page displays the status of all system LRUs. SYSTEM SETUP PAGE The System Setup Page allows management of the following system parameters: • Pilot Profiles • Page Navigation • Date/time • MFD Data Bar Fields (Navigation Status Box) (see Flight Management Section) • Display Units (see Flight Instruments Section) • Baro Transition Alert (see Flight Instruments Section) • Airspace Alerts (see Flight Management Section) • Arrival Alerts (see Flight Management Section) • Audio Alerts • Flight Director 190-00728-06 Rev. A • GPS CDI scaling for GPS navigation source (see Flight Instruments Section) • COM Configuration (see Audio Panel and CNS Section) • Nearest Airports display criteria (see Flight Management Section) • Synchronization of Baro and CDI between PFDs Embraer Prodigy® Flight Deck 100 Pilot’s Guide 43 SYSTEM OVERVIEW Figure 1-36 System Setup Page Pilot Profiles Various system settings may be saved under a pilot profile. When the system is powered on, the last selected pilot profile is shown on the MFD power-up screen (Figure 1-19). The system can store up to 25 profiles; the currently active profile, the amount of memory used, and the amount of memory available are shown at the top of the System Setup Page in the box labeled ‘PILOT PROFILE’. From here, pilot profiles may be created, selected, renamed, or deleted. Pilot profiles may also be imported from an SD card, or exported to an SD card. Pilot Profiles cannot not be imported if originally created using a previous version of system software. Figure 1-37 Pilot Profiles (System Setup Page) 44 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW System settings on the AUX-System Setup Page that are pilot adjustable are saved to the pilot profile, as well as, but not limited to, the following: • Altimeter units setting • Map settings • SBAS settings • Chart settings • HSI and wind display settings • SVS options Creating a profile: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight ‘CREATE’ in the Pilot Profile Box. 4) Press the ENT Key. A ‘Create Profile’ window is displayed. 5) Use the FMS Knob to enter a profile name up to 16 characters long and press the ENT Key. Pilot profile names cannot begin with a blank as the first letter. 6) In the next field, use the small FMS Knob to select the desired settings upon which to base the new profile. Profiles can be created based on Garmin factory defaults, default profile settings (initially based on Garmin factory defaults unless edited by the pilot), or current system settings. 7) Press the ENT Key. 8) With ‘CREATE’ highlighted, press the ENT Key to create the profile Or: Use the large FMS Knob to select ‘CREATE and ACTIVATE’ and press the ENT Key to activate the new profile. 9) To cancel the process, select ‘CANCEL’ with the large FMS Knob and press the ENT Key. 10) Press the FMS Knob to deactivate the cursor. Selecting an active profile: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the active profile field in the Pilot Profile Box. 4) Turn the small FMS Knob to display the pilot profile list and highlight the desired profile. 5) Press the ENT Key. The system loads and displays the system settings for the selected profile. 6) Press the FMS Knob to deactivate the cursor. Renaming a profile: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight ‘RENAME’ in the Pilot Profile Box. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 45 SYSTEM OVERVIEW 4) Press the ENT Key. 5) In the ‘Rename Profile’ window, turn the FMS Knob to select the profile to rename. 6) Press the ENT Key. 7) Use the FMS Knob to enter a new profile name up to 16 characters long and press the ENT Key. 8) With ‘RENAME’ highlighted, press the ENT Key. 9) To cancel the process, use the large FMS Knob to select ‘CANCEL’ and press the ENT Key. 10) Press the FMS Knob to deactivate the cursor. Deleting a profile: NOTE: The profile that is currently active cannot be deleted. If this is the desired profile to delete, select another profile, then delete the desired profile. 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight ‘DELETE’ in the Pilot Profile Box. 4) Press the ENT Key. 5) In the ‘Delete Profile’ window, turn the FMS Knob to select the profile to delete. 6) Press the ENT Key. 7) With ‘DELETE’ highlighted, press the ENT Key. 8) To cancel the process, use the large FMS Knob to select ‘CANCEL’ and press the ENT Key. 9) Press the FMS Knob to deactivate the cursor. Importing a profile from an SD card: 1) Insert an SD card containing the pilot profile(s) into the top card slot on the MFD. 2) Turn the FMS Knob to select the AUX - System Setup Page. 3) Select the IMPORT Softkey. Or: a) Press the MENU Key. b) Turn the FMS Knob to highlight ‘Import Pilot Profile’ and press the ENT Key. 4) The system displays the Pilot Profile Importing Window with ‘IMPORT’ highlighted. To change the selected profile to be imported from the SD card (shown as ‘SELECT FILE’), turn the large FMS Knob to highlight the profile file name, then turn the small FMS Knob to highlight a profile from the list, and press the ENT Key. 5) If desired, the profile name to be used after profile has been imported can be changed by turning the FMS Knob to highlight the ‘PROFILE NAME’ field, then use the large and small FMS Knobs to enter the name, and press the ENT Key. Imported profile names cannot begin with a blank space or be named ‘DEFAULT’, ‘GARMIN DEFAULTS’ or ‘DEFAULT SETTINGS’. 6) With ‘IMPORT’ highlighted, press the ENT Key. 46 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW 7) If the imported profile name is the same as an existing profile on the system, the system displays an ‘Overwrite existing file? OK or CANCEL’ prompt. Press the ENT Key to replace profile on the system with the profile imported from the SD card, or turn the FMS Knob to highlight ‘CANCEL’ and press the ENT Key to return to the Pilot Profile Importing Window. 8) If successful, the system displays ‘Pilot profile import succeeded.’ in the IMPORT RESULTS window below. With ‘OK’ highlighted, press the ENT or CLR Keys or press the FMS Knob to return to the AUX - System Setup Page. The imported profile becomes the active profile. Pilot Profile Importing and Import Results Window Pilot Profiles Available for Import from SD Card (‘STEVE’S PROFILE’ Selected) Import Successful Figure 1-38 Pilot Profile Importing Window (AUX - System Setup Page) Exporting a profile to an SD card: 1) Insert the SD card for storing the Pilot Profile into the top card slot on the MFD. 2) Turn the FMS Knob to select the AUX - System Setup Page. 3) If necessary, activate the desired pilot profile to export. Only the currently active Pilot Profile can be exported. 4) Select the EXPORT Softkey. The system displays the Pilot Profile Exporting Window. Or: a) Press the MENU Key. b) Turn the FMS Knob to highlight ‘Export Pilot Profile’ and press the ENT Key. 5) To export the pilot profile using the current supplied name, press the ENT Key with ‘EXPORT’ highlighted. To change the profile file name turn the large FMS Knob to highlight the ‘SELECT FILE’ field, then enter the new name with the large and small FMS Knobs, then press the ENT Key. Then press the ENT Key with ‘EXPORT’ highlighted. 6) If the profile name to be exported is the same as an existing profile file name on the SD card, the system displays an ‘Overwrite existing file? OK or CANCEL’ prompt. Press the ENT Key to replace the profile on the SD card with the profile to be exported, or turn the FMS Knob to highlight ‘CANCEL’ and press the ENT Key to return to the Pilot Profile Exporting Window without exporting the profile. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 47 SYSTEM OVERVIEW 7) If successful, the EXPORT RESULTS window displays ‘Pilot profile export succeeded.’ With ‘OK’ highlighted, press the ENT or CLR Keys, or press the FMS Knob to return to the AUX - System Setup Page. Pilot Profile Exporting Window, Enter a Name to Use for Exported Profile Export Successful Figure 1-39 Pilot Profile Exporting Window (AUX - System Setup Page) Date/Time The Date/Time Box on the System Setup Page displays the current date and time and allows the pilot to set the time format (local 12-hr, local 24-hr, or UTC) and offset. The time offset is used to define current local time. UTC (also called GMT or Zulu) date and time are calculated directly from the GPS satellites signals and cannot be changed. When using a local time format, designate the offset by adding or subtracting the desired number of hours. Setting the system time format: 1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor. 2) Turn the large FMS Knob to highlight the time format field in the Date/Time Box. 3) Turn the small FMS Knob to select the desired system time format (local 12hr, local 24hr, UTC) and press the ENT Key. Setting the current time offset: 1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor. 2) Turn the large FMS Knob to highlight the time offset field in the Date/Time Box. 3) Enter the time offset and press the ENT Key. Display Units The Display Units Box on the System Setup Page shows the configured units of measure used for each category. Only the NAV ANGLE, ALT,VS, and POSITION are pilot selectable. The following indicates the system parameters affected by changes within that category. • Nav angle (magnetic, true) When set to ‘MAGNETIC’, magnetic variation is figured into the displayed value. When ‘TRUE’ is selected, no magnetic variation is calculated and a ‘T’ is displayed next to the value. Affects the BRG field in the PFD Navigation Status Box. 48 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW Affects Current Heading, Selected Heading, and Selected Course boxes on the PFD. Affects the BRG, DTK, TKE, TRK, and XTK fields in the MFD Navigation Status Box. • Altitude and vertical speed (feet, meters) Affects all altitude and elevation displays on the MFD, with the exception of VNV altitudes on the Active Flight Plan Page. • Position (HDDD°MM.MM’, HDDD°MM’SS.S”) Affects all position displays. To change a Display Units setting: 1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor. 2) Turn the large FMS Knob to highlight the desired field in the Display Units Box. 3) Turn the small FMS Knob to select from a list of measurement units and press the ENT Key when the desired unit is highlighted. Press the CLR Key to cancel the action without changing the units. BARO Transition Alert See the Flight Instruments section for a discussion on setting the Baro Transition Alert. Airspace Alerts The Airspace Alerts Box allows the pilot to turn the controlled/special-use airspace message alerts on or off. This does not affect the alerts listed on the Nearest Airspaces Page or the airspace boundaries depicted on the MFD Navigation Map Page. It simply turns on/off the warning provided when the aircraft is approaching or near an airspace. Alerts for the following airspaces can be turned on/off in the Airspace Alerts Box: • Class B/TMA • Restricted • Class C/TCA • MOA (Military) • Class D • Other/ADIZ An altitude buffer is also provided which “expands” the vertical range above or below an airspace. For example, if the buffer is set at 500 feet, and the aircraft is more than 500 feet above/below an airspace, an alert message will not be generated, but if the aircraft is less than 500 feet above/below an airspace and projected to enter it, the pilot is notified with an alert message. The default setting for the altitude buffer is 200 feet. Changing the altitude buffer distance setting: 1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor. 2) Turn the large FMS Knob to highlight the altitude buffer field in the Airspace Alerts Box. 3) Turn the FMS Knobs to enter an altitude buffer value and press the ENT Key. 4) Press the FMS Knob to deactivate the cursor. Turn an airspace alert on or off 1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 49 SYSTEM OVERVIEW 2) Turn the large FMS Knob to highlight the desired field in the Airspace Alerts Box. 3) Turn the small FMS Knob clockwise to turn the airspace alert ON or counterclockwise to turn the alert OFF. 4) Press the FMS Knob to deactivate the cursor. Arrival Alerts The Arrival Alert Box on the System Setup Page allows arrival alerts to be turned on/off and the alert trigger distance set. An arrival alert can be set to notify the pilot with a message upon reaching a userspecified distance from the final destination (the direct-to waypoint or the last waypoint in a flight plan). Once the set distance (up to 99.9 units) has been reached, an “Arriving at waypoint” message is displayed in the PFD Navigation Status Box. Enabling/disabling an arrival alert: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to select the ON/OFF field in the Arrival Alert Box. 4) Turn the small FMS Knob clockwise to turn the airspace alert ON or counterclockwise to turn the alert OFF. 5) Press the FMS Knob to deactivate the cursor. Changing the arrival alert trigger distance: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the distance field in the Arrival Alert Box. 4) Use the FMS Knob to enter a trigger distance and press the ENT Key. 5) Press the FMS Knob to deactivate the cursor. Flight Director Two formats are available for the display of the flight director. Single Cue or X-Pointer may be selected. To change the flight director format: 1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor. 2) Turn the large FMS Knob to highlight the Format Active field in the Flight Director Box. 3) Turn the small FMS Knob to display and highlight the desired flight director format and press the ENT Key. 4) Press the FMS Knob to deactivate the cursor. Page Navigation The large FMS Knob displays the Page Group Tabs and navigates through the tabs. The small FMS Knob navigates through the pages listed within a specific group. The number of clicks it takes to display the Page Group Tabs and change to the next tab can be controlled from the Page Navigation box on the AUX - System Setup Page. OFF – Displays the Page Group Tabs with one click of either FMS Knob. 50 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW ON – Displays the Page Group Tabs and navigates to the next tab with one click of either FMS Knob. The pilot can select, from the AUX - System Setup Page, the amount of time the Page Group Tabs are displayed (in the lower right corner of the MFD). The timeout can range from two to ten seconds. Selecting page navigation settings: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the ‘Change On 1st Click’ field in the Page Navigation Box. 4) Turn the small FMS Knob to select ‘OFF’ or ‘ON’. 5) Turn the large FMS Knob to highlight the ‘Timeout Seconds’ field in the Page Navigation Box. 6) Turn the small FMS Knob to select the desired number of seconds 7) Press the FMS Knob momentarily to remove the flashing cursor. MFD Data Bar Fields The MFD Data Bar Fields Box on the System Setup Page displays the current configuration of the MFD Navigation Status Box. By default, the Navigation Status Bar is set to display ground speed (GS), distance to next waypoint (DIS), estimated time enroute (ETE), and enroute safe altitude (ESA). Changing the information shown in an MFD Navigation Status Bar field: 1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor. 2) Turn the large FMS Knob to highlight the desired field number in the MFD Data Bar Fields Box. 3) Turn the small FMS Knob to display and scroll through the data options list and press the ENT Key when the desired data selection is highlighted. 4) Press the FMS Knob to deactivate the cursor. The following data may be selected for display in each of the four fields of the Navigation Status Box. • Bearing (BRG) • Track (TRK) • Distance (DIS) • Vertical Speed Required (VSR) • Desired Track (DTK) • Crosstrack Error (XTK) • En Route Safe Altitude (ESA) • Fuel Over Destination (FOD) • Estimated Time of Arrival (ETA) • Fuel On Board (FOB) • Estimated Time En Route (ETE) • Endurance (END) • Ground Speed (GS) • Enroute (ENR) • Minimum Safe Altitude (MSA) • International Standard Atmosphere (ISA) • True Air Speed (TAS) • Landing Time (LDG) • Track Angle Error (TKE) 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 51 SYSTEM OVERVIEW GPS CDI The GPS CDI Box on the System Setup Page allows the pilot to define the range for the on-screen course deviation indicator (CDI). The range values represent full range deflection for the CDI to either side. The default setting is ‘AUTO’. At this setting, leaving the departure airport the CDI range is set to 1.0 nm and gradually ramps up to 2 nm beyond 30 nm from the departure airport. The CDI range is set to 2.0 nautical miles during the en route phase of flight. Within 30 nm of the destination airport, the CDI range gradually ramps down to 1.0 nm (terminal area). During approach operations, the CDI range ramps down even further to 0.3 nm. This transition normally occurs within 2.0 nm of the final approach fix (FAF). If a lower CDI range setting is selected (i.e., 1.0 or 0.3 nm), the higher range settings are not selected during any phase of flight. For example, if 1.0 nm is selected, the system uses this for en route and terminal phases and ramps down to 0.3 nm during an approach. Note that the Receiver Autonomous Integrity Monitoring (RAIM) protection limits follow the selected CDI range and corresponding flight phases. The GPS CDI Box on the System Setup Page displays the following: • Selected CDI range (auto, 2 nm, 1 nm, 0.3 nm) • Current system CDI range (2 nm, 1 nm, 0.3 nm) Changing the CDI range: 1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor. 2) Turn the large FMS Knob to highlight the selected field in the GPS CDI Box. 3) Turn the small FMS Knob to display and scroll through the range list and press the ENT Key when the desired selection is highlighted. 4) Press the FMS Knob to deactivate the cursor. COM Configuration NOTE: 8.33 kHz VHF communication frequency channel spacing is not required for use in the United States. Select the 25.0 kHz channel spacing option for use in the United States. The COM Configuration Box on the System Setup Page allows the pilot to select 8.33 kHz or 25.0 kHz COM frequency channel spacing. Changing COM channel spacing: 1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor. 2) Turn the large FMS Knob to highlight the channel spacing field in the COM Configuration Box. 3) Turn the small FMS Knob to select the desired spacing and press the ENT Key. 4) Press the FMS Knob to deactivate the cursor. Nearest Airports The Nearest Airports Box on the System Setup Page defines the minimum runway length and surface type used when determining the nine nearest airports to display on the MFD Nearest Airports Page. A minimum runway length and/or surface type can be entered to prevent airports with small runways or runways that are not of appropriate surface from being displayed. Default settings are zero feet (or meters) for runway length and “HARD/SOFT” for runway surface type. 52 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW Selecting the nearest airport surface matching criteria (any, hard only, hard/soft): 1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor. 2) Turn the large FMS Knob to highlight the runway surface field in the Nearest Airports Box. 3) Turn the small FMS Knob to display and scroll through the runway options (any, hard only, hard/soft) and press the ENT Key when the desired selection is highlighted. 4) Press the FMS Knob to deactivate the cursor. Selecting the nearest airport minimum runway length matching criteria: 1) While on the System Setup Page, press the FMS Knob momentarily to activate the flashing cursor. 2) Turn the large FMS Knob to highlight the minimum length field in the Nearest Airport Box. 3) Turn the FMS Knobs to enter the minimum runway length (zero to 25,000 feet) and press the ENT Key. 4) Press the FMS Knob to deactivate the cursor. CDI/BARO Synchronization See the Flight Instruments section for a discussion on synchronizing both PFD’s Course Deviation Indicators and the altimeter barometric settings. SYSTEM STATUS PAGE The System Status Page displays the status and software version numbers for all detected system LRUs. Pertinent information on all system databases is also displayed. Active LRUs are indicated by green check marks and failed LRUs are indicated by red “X”s. Failed LRUs should be noted and an Embraer service center or Garmin dealer informed. Figure 1-40 System Status Page 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 53 SYSTEM OVERVIEW The LRU and ARFRM, Softkeys on the System Status Page select the applicable list (LRU INFO or AIRFRAME window) through which the FMS Knob can be used to scroll information within the selected window. Selecting the MFD1 DB Softkey (label background changes to grey indicting the softkey is selected) places the cursor in the DATABASE window. Use the FMS Knob to scroll through database information for the MFD. Selecting the softkey again will change the softkey label to PFD1 DB. PFD 1 database information is now displayed in the DATABASE window. Selecting the softkey a third time will change the softkey label to PFD2 DB. PFD 2 database information is now displayed in the DATABASE window. The ANN TEST Softkey, when selected, causes an annunciation test tone to be played. Selecting the SYNC DBS Softkey (label background changes to grey indicting the softkey is selected) activates the Automatic Database Synchronization feature. When this feature is active, databases are updated automatically in the MFD and both PFDs from one SD card. For a detailed discussion on database synchronization, see the SD Card Use section in the Appendices. UTILITY PAGE For flight planning purposes, timers, trip statistics, and a scheduler feature are provided on the AUX - Utility Page. The timers available include a stopwatch-like generic timer, a total time in flight timer, and a record of the time of departure. Trip statistics—odometer, trip odometer, and average trip and maximum groundspeeds—are displayed from the time of the last reset. A scheduler feature is also provided so the pilot can enter reminder messages to be displayed at specified intervals in the Messages Window on the PFD (see Figure 1-41). Figure 1-41 Utility Page 54 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW Timers The generic timer can be set to count up or down from a specified time (HH:MM:SS). When the countdown on the timer reaches zero the digits begin to count up from zero. If the timer is reset before reaching zero on a countdown, the digits are reset to the initial value. If the timer is counting up when reset, the digits are zeroed. Setting the generic timer: 1) Use the FMS Knob to select the AUX - Utility Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the small FMS Knob to select the timer counting direction (UP/DN) and press the ENT Key. 4) If a desired starting time is desired: a) Use the large FMS Knob to highlight the HH:MM:SS field. b) Use the FMS Knob to enter the desired time and press the ENT Key. 5) Turn the large FMS Knob to highlight ‘START?’ and press the ENT Key to start the timer. The field changes to ‘STOP?’. 6) To stop the timer, press the ENT Key with ‘STOP?’ highlighted. The field changes to ‘RESET?’. 7) To reset the timer, press the ENT Key with ‘RESET?’ highlighted. The field changes back to ‘START?’ and the digits are reset. The flight timer can be set to count up from zero starting at system power-up or from the time that the aircraft lifts off; the timer can also be reset to zero at any time. Setting the flight timer starting criterion: 1) Use the FMS Knob to select the AUX - Utility Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the field next to the flight timer. 4) Turn the small FMS Knob to select the starting criterion (PWR-ON or IN-AIR) and press the ENT Key. 5) Press the FMS Knob to deactivate the cursor. Resetting the flight timer: 1) Use the FMS Knob to select the AUX - Utility Page. 2) Press the MENU Key. 3) With ‘Reset Flight Timer’ highlighted, press the ENT Key. The system records the time at which departure occurs, depending on whether the pilot prefers the time to be recorded from system power-up or from aircraft lift off. The displayed departure time can also be reset to display the current time at the point of reset. The format in which the time is displayed is controlled from the System Setup Page. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 55 SYSTEM OVERVIEW Setting the departure timer starting criterion: 1) Use the FMS Knob to select the AUX - Utility Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the field next to the departure time. 4) Turn the small FMS Knob to select the starting criterion (PWR-ON or IN-AIR) and press the ENT Key. Resetting the departure time: 1) Use the FMS Knob to select the AUX - Utility Page. 2) Press the MENU Key. 3) Use the FMS Knob to highlight ‘Reset Departure Time’ and press the ENT Key. The hour meter starts counting up when either engine is running and the aircraft is in the air. The hour meter stops counting when both engines have stopped running or the aircraft is on the ground. This is a system timer and is not pilot adjustable. Trip Statistics The odometer and trip odometer record the total mileage traveled from the last reset; these odometers can be reset independently. Resetting the trip odometer also resets the average trip groundspeed. Maximum groundspeed for the period of time since the last reset is also displayed. Resetting trip statistics readouts: 1) Use the FMS Knob to select the AUX - Utility Page. 2) Press the MENU Key. The following reset options for trip statistics are displayed: • Reset Trip ODOM/AVG GS—Resets trip average ground speed readout and odometer • Reset Odometer—Resets odometer readout only • Reset Maximum Speed—Resets maximum speed readout only • Reset All—Resets flight timer, departure timer, odometers, and groundspeed readouts 2) Use the FMS Knob to highlight the desired reset option and press the ENT Key. The selected parameters are reset to zero and begin to display data from the point of reset. Flight Data Logger This feature is not available on the Phenom 100. Scheduler The scheduler feature can be used to enter and display reminder messages. Messages can be set to display based on a specific date and time (event), once the message timer reaches zero (one-time; default setting), or recurrently whenever the message timer reaches zero (periodic). Message timers set to periodic alerting automatically reset to the original timer value once the message is displayed. When power is cycled, messages are retained until deleted, and message timer countdown is restarted. 56 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW Entering a scheduler message: 1) Use the FMS Knob to select the AUX - Utility Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the first empty scheduler message naming field. 4) Enter the message text to be displayed in the Messages Window and press the ENT Key. 5) Press the ENT Key again or use the large FMS Knob to move the cursor to the field next to ‘Type’. 6) Turn the small FMS Knob to select the message alert type: • Event—Message issued at the specified date/time • One-time—Message issued when the message timer reaches zero (default setting) • Periodic—Message issued each time the message timer reaches zero 7) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field. 8) For periodic and one-time message, enter the timer value (HHH:MM:SS) from which to countdown and press the ENT Key. 9) For event-based messages: a) Enter the desired date (DD-MMM-YYY) and press the ENT Key. b) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field. c) Enter the desired time (HH:MM) and press the ENT Key. 10) Press the ENT Key again or use the large FMS Knob to move the cursor to enter the next message. Deleting a scheduler message: 1) Use the FMS Knob to select the AUX - Utility Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the name field of the scheduler message to be deleted. 4) Press the CLR Key to clear the message text. If the CLR Key is pressed again, the message is restored. 5) Press the ENT Key to confirm message deletion. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 57 SYSTEM OVERVIEW Scheduler messages appear in the Messages Window on the PFD. Pressing the MSG Softkey opens the Messages Window and acknowledges the scheduler message. When MSG Softkey is pressed again, the Messages Window is removed from the display and the scheduler message is deleted from the message queue. Figure 1-42 PFD Message Window 58 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A SYSTEM OVERVIEW 1.8 DISPLAY BACKLIGHTING The system display and control backlighting can be adjusted either automatically or manually. Backlighting intensity ranges from 0.14% to 100% on the PFDs and 0.80% to 100.00% on the MFD. AUTOMATIC ADJUSTMENT The existing instrument panel dimmer bus normally controls the PFD and MFD backlighting as well as the PFD and MFD bezels, MFD Control Unit, AFCS Control Unit and audio panel key annunciator lighting. When the dimmer bus is not used by the system, photocell technology automatically controls backlighting adjustments. Photocell calibration curves are pre-configured to optimize display appearance through a broad range of cockpit lighting conditions. MANUAL ADJUSTMENT NOTE: The avionics dimming knob may also be used to adjust backlighting. Refer to the AFM for details. NOTE: In normal mode, backlighting can only be adjusted from PFD1 or PFD2. In reversionary mode, it can also be adjusted from the MFD. NOTE: No other window can be displayed on the PFD while the PFD Setup Menu Window is displayed. Backlighting may also be adjusted manually for all of the displays and the associated bezels. The audio panel key backlighting is directly tied to the on-side PFD key backlighting setting. Adjust display backlighting manually: 1) Press the MENU Key on the PFD to display the PFD Setup Menu Window. ‘AUTO’ becomes highlighted to the right of ‘PFD1 DSPL’. Figure 1-43 Manual Display Backlighting Adjustment 2) Turn the small FMS Knob to display the selection box. Turn the FMS Knob to select ‘MANUAL’, then press the ENT Key. The intensity value becomes highlighted. 3) Turn the small FMS Knob to select the desired backlighting, then press the ENT Key. 4) Turn the large FMS Knob to highlight ‘AUTO’ to the right of ‘MFD DSPL’ or ‘PFD2 DSPL’, respectively, and repeat steps 2 and 3. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 59 SYSTEM OVERVIEW 5) Press the CLR or MENU Key to remove the PFD Setup Menu Window from the display. Adjust key backlighting manually: 1) Press the MENU Key on the PFD to display the PFD Setup Menu Window. ‘AUTO’ becomes highlighted to the right of ‘PFD1 DSPL’. Figure 1-44 Manual Key Lighting Adjustment 2) Turn the large FMS Knob to highlight ‘PFD1 DSPL’. Turn the small FMS Knob in the direction of the green arrowhead to display ‘PFD1 KEY’. 3) Turn the large FMS Knob to highlight ‘AUTO’ and turn the small FMS Knob to display the selection box. 4) Turn the FMS Knob to select ‘MANUAL’, then press the ENT Key. The intensity value becomes highlighted. 5) Turn the small FMS Knob to select the desired backlighting, then press the ENT Key. 6) Turn the large FMS Knob to highlight ‘MFD DSPL’ or ‘PFD2 DSPL’ and turn the small FMS Knob in the direction of the green arrowhead to display ‘MFD KEY’ or ‘PFD2 KEY’, respectively. 7) Repeat steps 3 to 5. 8) Press the CLR or MENU Key to remove the PFD Setup Menu Window from the display. 60 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT INSTRUMENTS SECTION 2 FLIGHT INSTRUMENTS WARNING: If the airspeed, attitude, altitude, or heading indications become unusable, refer to the backup instruments. NOTE: The Automatic Flight Control System (AFCS) provides additional readouts and indicators (bug) on selected flight instruments. Refer to the AFCS Section for details on these indicators (bug) and readouts, as they appear on the display during certain AFCS flight director modes. Increased situational awareness is provided by replacing the traditional instruments on the panel with two easyto-scan Primary Flight Displays (PFDs) that feature large horizons, airspeed, attitude, altitude, vertical speed, and course deviation information. In addition to the flight instruments, navigation, communication, terrain, traffic, and weather information are also presented on the PFDs and explained in other sections of this Pilot’s Guide. The following flight instruments and supplemental flight data are displayed on each PFD: • Static Air Temperature (SAT) • Airspeed Indicator, showing • Horizontal Situation Indicator, showing – Indicated airspeed – True airspeed – Turn Rate Indicator – Airspeed awareness ranges – Bearing pointers and information windows – Vspeed reference bugs – Navigation source – Groundspeed – Course Deviation Indicator (CDI) – Mach number – Bearing pointers and information windows – Airspeed reference and bug – DME Information Windows • Attitude Indicator with slip/skid indication • Transponder Mode, Code, and Ident/Reply • Altimeter, showing • Course Deviation Indicator (CDI) • Timer/References Window, showing – Trend vector – Barometric setting – Generic timer – Selected Altitude – Vspeed values – Barometric minimum descent altitude (MDA) • Vertical Deviation, Glideslope, and Glidepath Indicators • Wind data • Vertical Speed Indicator (VSI) • Radar Altimeter (RA) (optional) • Vertical Navigation (VNV) indications • Total Air Temperature (TAT) The PFDs also display various alerts and annunciations. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 61 FLIGHT INSTRUMENTS 27 26 25 24 23 1 2 22 21 20 3 19 4 5 6 18 7 17 8 16 9 15 10 14 11 13 12 1 NAV Frequency Box 15 Transponder Status Box 2 Airspeed Reference 16 Heading Bug 3 Airspeed Indicator 17 Turn Rate Indicator 4 Airspeed Reference Bug 18 Barometric Altimeter Setting 5 Mach Number 19 Vertical Speed Indicator (VSI) 6 Groundspeed 20 Selected Altitude Bug 7 Current Heading 21 Altimeter 8 Current Track Indicator 22 Selected Altitude 9 Course Deviation Indicator (CDI) 23 COM Frequency Box 10 Horizontal Situation Indicator (HSI) 24 Navigation Status Box 11 Total Air Temperature (TAT) 25 AFCS Status Box 12 Static Air Temperature (SAT) 26 Slip/Skid Indicator 13 Softkeys 27 Attitude Indicator 14 System Time Figure 2-1 Primary Flight Display (Default) 62 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT INSTRUMENTS 15 14 13 1 12 11 10 9 2 8 3 7 4 5 6 5 1 Vspeed Reference 9 CAS Annunciation Window 2 Selected Heading 11 Desired Track 3 Wind Data 11 Radar Altimeter (optional) 4 Inset Map 12 Current Vertical Speed 5 DME Information Windows 13 Glidepath Indicator 6 Bearing Information Windows 14 TAWS Annunciation 7 Flight Plan Window 15 Traffic Annunciation 8 Minimum Descent Altitude/ Decision Height Figure 2-2 Additional PFD Information 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 63 FLIGHT INSTRUMENTS 2.1 FLIGHT INSTRUMENTS AIRSPEED INDICATOR NOTE: Refer to the Airplane Flight Manual (AFM) for speed criteria and Vspeed values. The Airspeed Indicator displays airspeed on a moving tape rolling number gauge. The numeric labels and major tick marks on the moving tape represent intervals of 10 knots. The minor tick marks on the moving tape represent intervals of five knots. Speed indication starts at 20 knots, with 80 knots of airspeed scale viewable at any time. The indicated airspeed is displayed inside the black pointer. The pointer remains black until reaching maximum operating speed (VMO/MMO), at which point it turns red along with the Mach number readout. The Mach number is displayed below the Airspeed Indicator (Figure 2-3) for airspeeds at or above Mach 0.4 or at altitudes above 28,007 feet. The color of the readout is the same as the color of the airspeed pointer. Airspeed Reference Airspeed Trend Vector Vspeed References Indicated Airspeed 1.3VS1 Airspeed Ranges Airspeed Reference Bug Mach Number Ground Speed Red Pointer Showing Overspeed Airspeed Indicator Figure 2-3 Airspeed Indicator Speeds above the maximum operating speed, VMO or MMO depending on aircraft altitude, appear in the high speed awareness range, shown on the airspeed tape by a red/white barber pole. An aural overspeed warning tone is generated if the airspeed exceeds the high airspeed limit. Yellow and red ranges are also present for low speed awareness velocity (VLSA). If the indicated airspeed is within the yellow range, the airspeed readout is displayed in yellow. If the indicated airspeed is within the red range, the airspeed pointer is displayed in red. An aural stall warning is generated if the airspeed falls below VLSA. An open green circle on the airspeed tape represents 1.3VS1. The green circle is displayed when in the air below 18,000 feet, and it indicates the stall warning system is functioning correctly. The Airspeed Trend Vector is a vertical magenta line that appears to the right of the color-coded speed range strip when airspeed is either accelerating or decelerating. One end of the magenta line is anchored to the tip of the airspeed pointer while the other end moves continuously up or down corresponding to the rate of acceleration or deceleration. For any constant rate of acceleration or deceleration, the moving end of the line 64 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT INSTRUMENTS shows approximately what the indicated airspeed value will be in six seconds. If the trend vector crosses VMO/ MMO, the airspeed readout and the Mach readout change to yellow. If the trend vector crosses the red VLSA range, the airspeed readout is displayed in yellow. The trend vector is absent if the speed remains constant or if any data needed to calculate airspeed is not available due to a system failure. The Airspeed Reference is displayed above the Airspeed Indicator in the box indicated by a selection bug symbol. A bug corresponding to this speed is shown on the tape. If the Airspeed Reference exceeds the range shown on the tape, the bug appears at the upper or lower edge of the tape. See the AFCS Section for more information about the Airspeed Reference. Landing Takeoff Vspeeds can be changed and their bugs enabled/disabled from the Timer/References Window. When active (on), the Vspeeds are displayed at their respective locations to the right of the airspeed scale. Vspeed Bug V1 1 VR R V2 2 VFS FS VAP AP VREF RF VAC AC VFS FS Table 2-1 Vspeed Bug Labels Vspeeds are categorized as either takeoff or landing. Takeoff Vspeed bugs are automatically removed when airspeed reaches 160 knots. The order in which the categories are displayed is determined by whether the aircraft is on the ground or in the air. If the aircraft is on the ground, the takeoff Vspeeds are displayed at the top of the Vspeed list. If the aircraft is in the air, the landing Vspeeds are displayed at the top. Changing Vspeeds and enabling/disabling Vspeed bugs: 1) Press the TMR/REF Softkey. 2) Turn the large FMS Knob to highlight the desired Vspeed. 3) Use the small FMS Knob to change the Vspeed in 1-kt increments (when a speed has been changed from a default value, an asterisk appears next to the speed). 4) Press the ENT Key or turn the large FMS Knob to highlight the ON/OFF field. 5) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF. 6) To remove the window, press the CLR Key or press the TMR/REF Softkey. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 65 FLIGHT INSTRUMENTS Figure 2-4 Takeoff and Landing Vspeeds (Timer/References Window) Vspeed bugs can be enabled or disabled all at once or by category (takeoff and landing). Default values for all or a category of Vspeeds can also be restored. Modifying Vspeeds (on, off, restore defaults): 1) Press the TMR/REF Softkey. 2) Press the MENU Key. 3) Turn the FMS Knob to highlight the desired selection (Figure 2-5). 4) Press the ENT Key. 5) To remove the window, press the CLR Key or press the TMR/REF Softkey. Figure 2-5 Timer/References Window Menu 66 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT INSTRUMENTS ATTITUDE INDICATOR Attitude information is displayed over a virtual blue sky and brown ground with a white horizon line. The Attitude Indicator displays the pitch, roll, and slip/skid information. 9 8 1 7 2 1 Roll Pointer 2 Roll Scale 3 Horizon Line 4 5 Aircraft Symbol (Formatted for Single-cue Command Bars) Land Representation 6 Pitch Scale 7 Slip/Skid Indicator 8 Sky Representation 9 Roll Scale Zero 6 3 4 5 Figure 2-6 Attitude Indicator The horizon line is part of the pitch scale. Above and below the horizon line, major pitch marks and numeric labels are shown for every 10˚, up to 80˚. Minor pitch marks are shown for intervening 5˚ increments, up to 25˚ below and 45˚ above the horizon line. Between 20˚ below to 20˚ above the horizon line, minor pitch marks occur every 2.5˚. When the Synthetic Vision Technology (SVT) system is activated, the pitch scale is reduced to 10˚ up and 7.5˚ down; refer to the Additional Features section. The inverted white triangle indicates zero on the roll scale. Major tick marks at 30˚ and 60˚ and minor tick marks at 10˚, 20˚, and 45˚ are shown to the left and right of the zero. Angle of bank is indicated by the position of the pointer on the roll scale. The Slip/Skid Indicator is the bar beneath the roll pointer. One bar displacement is equal to one ball displacement on a traditional inclinometer. The indicator bar moves with the roll pointer and moves laterally away from the pointer to indicate uncoordinated flight. Slip (inside the turn) or skid (outside the turn) is indicated by the location of the bar relative to the pointer. In TCAS II installations, the Attitude Indicator also provides pitch cues to comply with TCAS II Resolution Advisories; see the Hazard Avoidance Section for details. Figure 2-7 Slip/Skid Indication 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 67 FLIGHT INSTRUMENTS The yellow symbolic aircraft on the Attitude Indicator changes appearance based on selection of AFCS flight director Command Bar format (see the AFCS Section for details). Both PFDs show the same Command Bar format and Aircraft Symbol. The Command Bar format (single-cue or cross-pointer) may be selected from the AUX - System Setup Page Figure 2-8. Changing Command Bar and Aircraft Symbol format: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the Format Active selection in the Flight Director box. 4) Turn the small FMS Knob to highlight the desired setting and press the ENT Key. 5) Select the SNGL CUE option to display Command Bars as a single cue (Figure 2-8). Or: Select the X POINTR option to display Command Bars as a cross pointer shown below. Single-cue Cross-pointer Figure 2-8 Flight Director Format (AUX - System Setup Page) 68 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT INSTRUMENTS ALTIMETER The altimeter displays 600 feet of barometric altitude values at a time on a moving tape rolling number gauge. Numeric labels and major tick marks are shown at intervals of 100 feet. Minor tick marks are at intervals of 20 feet. The indicated altitude is displayed inside the black pointer. The Selected Altitude is displayed above the altimeter in the box indicated by a selection bug symbol. A bug corresponding to this altitude is shown on the tape. If the Selected Altitude exceeds the range shown on the tape, the bug appears at the upper or lower edge of the tape. When the metric value is selected it is displayed in a separate box above the Selected Altitude (Figure 2-10). See the AFCS Section for more information about Selected Altitude. A magenta Altitude Trend Vector extends up or down the left of the altitude tape. The end extends to the approximate altitude to be reached in six seconds at the current vertical speed. The trend vector is not shown if altitude remains constant or if data needed for calculation is not available due to a system failure. Setting the Selected Altitude: T urn the ALT SEL Knob to set the Selected Altitude in 100-ft increments. When meters are displayed, Selected Altitude is adjusted in 50 meter increments. If a Minimum Descent Altitude/Decision Height (MDA/DH) value has been set, this value is also available as a Selected Altitude setting when turning the ALT SEL Knob. Selected Altitude Altitude Trend Vector Indicated Altitude Selected Altitude Bug Barometric Setting Box (In Hg) MDA/DH Altitude Bug Figure 2-9 Altimeter Settings, In Hg 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 69 FLIGHT INSTRUMENTS Selected and current altitudes can also be displayed in meters (readouts displayed above the normal readouts in feet; Figure 2-10). Note that the altitude tape does not change scale. Displaying altitude in meters: 1) Press the PFD Softkey to display the second-level softkeys. 2) Press the ALT UNIT Softkey. 3) Press the METERS Softkey to turn on metric altitude readouts. 4) Press the BACK Softkey twice to return to the top-level softkeys. Selected Altitude (Meters) Selected Altitude Bug Indicated Altitude (Meters) Barometric Setting Box (Hectopascals) Figure 2-10 Altimeter Setting in hPa and Altitude in Meters The barometric pressure setting is displayed below the altimeter in inches of mercury (in Hg) or hectopascals (hPa). Adjusting the altimeter barometric setting creates discontinuities in VNV vertical deviation, moving the descent path. For large adjustments, it may take several minutes for the aircraft to re-establish on the descent path. If the change is made while nearing a waypoint with a VNV Target Altitude, the aircraft may not re‑establish on the descent path in time to meet the vertical constraint. Changing altimeter barometric pressure setting units: 1) Press the PFD Softkey to display the second-level softkeys. 2) Press the ALT UNIT Softkey. 3) Press the IN Softkey to display the barometric pressure setting in inches of mercury (in Hg) (Figure 2-9). Or: Press the HPA Softkey to display the barometric pressure setting in hectopascals (hPa) (Figure 2-10). 4) Press the BACK Softkey twice to return to the top-level softkeys. 70 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT INSTRUMENTS Selecting the altimeter barometric pressure setting: Turn the BARO Knob to select the desired setting. Selecting standard barometric pressure (29.92 in Hg): Press the BARO Knob to select standard pressure. Or: 1) Press the PFD Softkey to display the second-level softkeys. 2) Press the STD BARO Softkey; STD BARO is displayed in barometric setting box. Figure 2-11 Standard Barometric Altimeter Setting If the barometric altimeter settings differ between PFDs by more than 0.02 in Hg, the readouts are yellow. Once the settings are synchronized (BARO turned on), they remain synchronized until the setting is turned off. Synchronizing the altimeter barometric pressure settings: 1) Select the AUX - System Setup Page using the FMS Knob. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight Baro in the Synchronization box. 4) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF. 5) Press the FMS Knob to remove the cursor. Barometric Settings not Synchronized on PFD Displayed in Yellow Figure 2-12 Baro Sync Setting (AUX - System Setup Page) 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 71 FLIGHT INSTRUMENTS A Baro Transition Alert is provided to notify the pilot to change the barometric pressure setting when crossing the baro transition altitude. If the aircraft is at least 500 feet below the transition altitude and then climbs through this altitude and the STD BARO Softkey has not been pressed, the barometric pressure setting flashes in light blue until the pressure setting is changed. If the aircraft is at least 500 feet above the transition altitude and then descends through this altitude and the barometric pressure setting has not been changed from STD BARO, the setting flashes in light blue until it is changed. Setting the Baro Transition Alert: 1) Use the FMS Knob to select the AUX - System Setup Page on the MFD. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight Altitude in the Baro Transition Alert box. 4) Turn the small FMS Knob to turn the alert OFF or ON and press the ENT Key. 5) Turn the small FMS Knob to change the desired altitude and press the ENT Key. 6) To cancel the selection, press the FMS Knob. Figure 2-13 Baro Transition Alert (AUX - System Setup Page) VERTICAL SPEED INDICATOR (VSI) The Vertical Speed Indicator (VSI) displays the aircraft vertical speed on a fixed scale with labels at 2000 and 4000 fpm and minor tick marks every 1000 fpm. Digits appear in the pointer when the climb or descent rate is greater than 100 fpm. If the rate of ascent/descent exceeds 4000 fpm, the pointer appears at the edge of the tape and the rate appears inside the pointer. A magenta chevron is displayed on the VSI to indicate the Required Vertical Speed for reaching a VNV target altitude once the “TOD [Top of Descent] within 1 minute” alert has generated. See the Flight Management and AFCS sections for details on VNV features. Refer to Section 2.2, Supplemental Flight Data, for more 72 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT INSTRUMENTS information about VNV indications on the PFD. In TCAS II installations, the VSI also provides vertical speed guidance during TCAS II Resolution Advisories; see the Hazard Avoidance section for details. VERTICAL DEVIATION The Vertical Deviation Indicator (VDI) (Figure 2-14) is a magenta chevron indicating the baro-VNV vertical deviation when Vertical Navigation (VNV) is being used. The VDI appears in conjunction with the “TOD within 1 minute” alert. The VDI is removed from the display if vertical deviation becomes invalid. See the Flight Management Section for details on VNV features, and refer to Section 2.2, Supplemental Flight Data, for more information about VNV indications on the PFD. The Glideslope Indicator (Figure 2-15) appears to the left of the altimeter whenever an ILS frequency is tuned in the active NAV field and the aircraft heading and selected course are within 107˚. A green diamond acts as the Glideslope Indicator, like a glideslope needle on a conventional indicator. If a localizer frequency is tuned and there is no glideslope, “NO GS” is displayed in place of the diamond. The Glidepath Indicator (Figure 2-16) is analogous to the glideslope for GPS approach service levels supporting SBAS vertical guidance (LNAV+V, L/VNV, LPV). When a supported approach is loaded into the flight plan and GPS is the selected navigation source, the Glidepath Indicator appears as a magenta diamond. Full-scale deflection (two dots), is angular with upper and lower limits. The upper limit is +/-150 meters and lower limits depend on approach service level. • LNAV+V and L/VNV is +/- 45 meters. • LPV is +/- 15 meters. If the approach type downgrades past the final approach fix (FAF), “NO GP” is displayed in place of the diamond. VNV Target Altitude Marker Beacon Annunciation Vertical Speed Indicator Vertical Deviation Indicator Vertical Glideslope Speed Indicator Pointer Glipepath Indicator Required Vertical Speed Figure 2-14 Vertical Speed and Deviation Indicator (VSI and VDI) 190-00728-06 Rev. A Figure 2-15 Glideslope Indicator Embraer Prodigy® Flight Deck 100 Pilot’s Guide Figure 2-16 Glidepath Indicator 73 FLIGHT INSTRUMENTS While executing a GPS approach with LNAV/VNAV service levels, while the aircraft is between the FAF and MAP, excessive deviation indicators appear as yellow vertical lines (Figure 2-17) to indicate an area where the vertical deviation exceeds ±75 feet. If the glidepath indicator is within an area of excessive deviation, the glidepath indicator becomes yellow. Magenta Glipepath Indicator shown within normal deviation range Yellow Glidepath Indicator shown when within Excessive Vertical Deviation Range Yellow Excessive Vertical Deviation Ranges Figure 2-17 Glidepath Indicator with Excessive Vertical Deviation Indications (LNAV/VNAV Approach Service Levels) HORIZONTAL SITUATION INDICATOR (HSI) The Horizontal Situation Indicator (HSI) displays a rotating compass card in a heading-up orientation. Letters indicate the cardinal points with numeric labels every 30˚. Major tick marks are at 10˚ intervals and minor tick marks are at 5˚ intervals. A digital reading of the current heading appears on top of the HSI, and the current track is represented on the HSI by a magenta diamond. The HSI also presents turn rate, course deviation, bearing, and navigation source information. The HSI is available in two formats, a 360˚ compass rose and a 140˚ arc. Changing the HSI display format: 1) Press the PFD Softkey. 2) Press the HSI FRMT Softkey. 3) Press the 360 HSI or ARC HSI Softkey. The 360˚ HSI contains a Course Deviation Indicator (CDI), with a Course Pointer, To/From Indicator, and a sliding deviation bar and scale. The course pointer is a single line arrow (GPS, VOR1, and LOC1) or a double line arrow (VOR2 and LOC2) which points in the direction of the set course. The To/From arrow rotates with the course pointer and is displayed when the active NAVAID is received. 74 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT INSTRUMENTS 16 15 14 1 2 13 3 4 5 12 6 11 7 10 8 9 1 Turn Rate Indicator 9 To/From Indicator 2 Selected Heading 10 Course Pointer 3 Current Track Indicator 11 Heading Bug 4 Lateral Deviation Scale 12 Flight Phase/Approach Service Level 5 Navigation Source 13 Selected Course 6 Aircraft Symbol 14 7 Course Deviation Indicator (CDI) 8 Rotating Compass Rose Turn Rate/Heading Trend Vector 15 Current Heading 16 Lubber Line Figure 2-18 Horizontal Situation Indicator (HSI) The Arc HSI is a 140˚ expanded section of the compass rose. The Arc HSI contains a Course Pointer, combined To/From Indicator and a sliding deviation indicator, and a deviation scale. Upon station passage, the To/From Indicator flips and points to the tail of the aircraft, just like a conventional To/From flag. Depending on the navigation source, the CDI on the Arc HSI can appear in two different ways, an arrowhead (GPS, VOR, OBS) or a diamond (LOC). Course Pointer Flight Phase Annunciation Navigation Source Course Deviation and To/From Indicator Lateral Deviation Scale Figure 2-19 Arc HSI 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 75 FLIGHT INSTRUMENTS A digital reading of the current heading appears on top of the HSI. The current track is represented on the HSI by a magenta diamond. To the upper left of the HSI, the Selected Heading is shown in light blue; the light blue bug on the compass rose corresponds to the Selected Heading. The Desired Track (DTK) is shown in magenta to the upper right of the HSI when the selected navigation source is GPS and OBS mode is not active. The Selected Course (CRS) is shown to the upper right of the HSI in green when the selected navigation source is VOR or LOC and in magenta when the selected navigation source is GPS with OBS mode active. Adjusting the Selected Heading: Turn the HDG Knob to set the Selected Heading on both PFDs. Press the HDG Knob to synchronize the bug to the current heading. Adjusting the Selected Course: Turn the CRS Knob to set the Selected Course (for each PFD). Press the CRS Knob to re-center the CDI and return the course pointer to the bearing of the active waypoint or navigation station. Current Track Indicator Current Heading Selected Course Selected Heading Heading Bug Figure 2-20 Heading and Course Indications Navigation angles (track, heading, course, bearing) are corrected to the computed magnetic variation (Mag Var) or referenced to true north (T), set on the AUX - System Setup Page. When an approach referenced to true north has been loaded into the flight plan, the system generates a message to change the navigation angle setting to True at the appropriate time. Figure 2-21 Heading and Course Indications (True) 76 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT INSTRUMENTS Changing the navigation angle true/magnetic setting: 1) Use the FMS Knob to select the AUX - System Setup Page on the MFD. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight Nav Angle in the Display Units box. 4) Turn the small FMS Knob to highlight the desired setting and press the ENT Key. • TRUE - References angles to true north (T) • MAGNETIC - Angles corrected to the computed magnetic variation (Mag Var) Figure 2-22 System Setup Page, Navigation Angle Settings TURN RATE INDICATOR The Turn Rate Indicator is located directly above the rotating compass rose. Tick marks to the left and right of the lubber line denote half-standard and standard turn rates. A magenta Turn Rate Trend Vector shows the current turn rate. The end of the trend vector gives the heading predicted in six seconds, based on the present turn rate. A standard-rate turn is shown on the indicator by the trend vector stopping at the standard turn rate tick mark, corresponding to a predicted heading of 18˚ from the current heading. At rates greater than 4 deg/sec, an arrowhead appears at the end of the magenta trend vector and the prediction is no longer valid. Half-standard Turn Rate Standard Turn Rate Arrow Shown for Turn Rate > 4 deg/sec Figure 2-23 Turn Rate Indicator and Trend Vector 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 77 FLIGHT INSTRUMENTS BEARING POINTERS AND INFORMATION WINDOWS Two bearing pointers and associated information can be displayed on the HSI for NAV, GPS, and ADF sources. The bearing pointers are light blue and are single-line (BRG1) or double-line (BRG2). A pointer symbol is shown in the information window to indicate the navigation source. The bearing pointers never override the CDI and are visually separated from the CDI by a white ring. Bearing pointers may be selected but not necessarily visible due to data unavailability. Tuning Mode Frequency Bearing 1 Pointer Distance Bearing 2 Pointer Tuning Mode Frequency No Signal DME1 Information Window Distance to Bearing Source Bearing Source DME2 Information Window No Waypoint Selected Station Identifier Pointer Icon Pointer Icon Bearing 1 Information Window Bearing Source Bearing 2 Information Window Figure 2-24 HSI with Bearing and DME Information When a bearing pointer is displayed, the associated information window is also displayed. The Bearing Information windows are displayed at the lower sides of the HSI and give the following information: • Bearing source (NAV, GPS, ADF) • Station/waypoint identifier (NAV, GPS) • Pointer icon (BRG1 = single line, BRG2 = double line) • GPS-derived great circle distance to bearing source • Frequency (NAV, ADF) When the NAV radio is tuned to an ILS frequency the bearing source and the bearing pointer is removed from the HSI. When NAV1 or NAV2 is the selected bearing source, the frequency is replaced by the station identifier when the station is within range. If GPS is the bearing source, the active waypoint identifier is displayed instead of a frequency. The bearing pointer is removed from the HSI and ‘NO DATA’ is displayed in the information window if the NAV radio is not receiving a VOR station or if GPS is the bearing source and an active waypoint is not selected. When the Arc HSI is displayed, the Bearing Information windows and pointers are disabled. 78 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT INSTRUMENTS Selecting bearing display and changing sources: 1) Press the PFD Softkey. 2) Press a BRG Softkey to display the desired bearing pointer and information window with a NAV source. 3) Press the BRG Softkey again to change the bearing source to GPS. 4) Press the BRG Softkey a third time to change the bearing source to ADF (ADF Radio installation is optional). 5) To remove the bearing pointer and information window, select the BRG Softkey again. DME INFORMATION WINDOWS The DME Information Windows are displayed above each BRG Information Window on the 360˚ HSI and in boxes along side and above the Arc HSI. It shows the DME label, tuning mode (NAV1, NAV2, or HOLD), frequency, and distance. When a signal is invalid, the distance is replaced by –.– – NM Refer to the Audio Panel and CNS Section for information on DME tuning.. Displaying the DME Information Window: 1) Press the PFD Softkey. 2) Press the DME1 or DME2 Softkey to display the DME Information Windows. 3) To remove the DME Information Windows, press the applicable DME Softkey again. COURSE DEVIATION INDICATOR (CDI) NOTE: During a heading change of greater than 105˚ with respect to the course, the CDI on the Arc HSI switches to the opposite side of the deviation scale and displays reverse sensing. The Course Deviation Indicator (CDI) moves left or right from the course pointer along a lateral deviation scale to display aircraft position relative to the course. If the course deviation data is not valid, the CDI is not displayed. 360º HSI Navigation Source Arc HSI Flight Phase Navigation Source Flight Phase Scale Crosstrack Error CDI CDI CDI Scale Figure 2-25 Course Deviation Indicator 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 79 FLIGHT INSTRUMENTS The CDI can display two sources of navigation: GPS or NAV (VOR/LOC). The color indicates the current navigation source: magenta for GPS or green for VOR and LOC. The full scale limits for the CDI are defined by a GPS-derived distance when navigating GPS. When navigating using a VOR or localizer (LOC), the CDI has the same angular limits as a mechanical CDI. If the CDI exceeds the maximum deviation on the scale (two dots) while navigating with GPS, the crosstrack error (XTK) is displayed below the white aircraft symbol. Yellow Indicates Navigation Source Selected on Both PFDs not Synchronized Figure 2-26 Navigation Sources CHANGING NAVIGATION SOURCES: 1) Press the CDI Softkey to change from GPS to VOR1 or LOC1. This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD. 2) Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2. This places the light blue tuning box over the NAV2 standby frequency. 3) Press the CDI Softkey a third time to return to GPS. NAV2 Selected for Tuning NAV1 Selected for Tuning GPS Selected LOC1 Selected VOR2 Selected Pressing the CDI Softkey Cycles through Navigation Sources Figure 2-27 Selecting a Navigation Source 80 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT INSTRUMENTS The system automatically switches from GPS to LOC navigation source and changes the CDI scaling accordingly when all of the following occur: • A localizer or ILS approach has been loaded into the active flight plan • The Final Approach Fix (FAF) is the active leg, the FAF is less than 15 nm away, and the aircraft is moving toward the FAF • A valid localizer frequency has been tuned • The GPS CDI deviation is less than 1.2 times full-scale deflection GPS steering guidance is still provided after the CDI automatically switches to LOC until LOC capture, up to the Final Approach Fix (FAF) for an ILS approach, or until GPS information becomes invalid. Activating a Vector-to-Final (VTF) also causes the CDI to switch to LOC navigation source. GPS steering guidance is not provided after the switch. If the same VOR/LOC navigation source is selected on both PFDs, the navigation source annunciation is yellow on both displays if not synchronized (Figure 2-26). Once the CDIs are synchronized (CDI Synchronization turned on), they remain synchronized until the selection is changed. When turning on the system for use, the system remembers the last CDI synchronization setting Synchronizing the CDIs: 1) Select the AUX - System Setup Page using the FMS Knob. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight CDI in the Synchronization box. 4) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF. 5) Press the FMS Knob to remove the cursor. Figure 2-28 System Setup Page, CDI Synchronization 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 81 FLIGHT INSTRUMENTS GPS CDI SCALING When GPS is the selected navigation source, the flight plan legs are sequenced automatically and annunciations appear on the HSI for the flight phase. Flight phase annunciations are normally shown in magenta, but when cautionary conditions exist the color changes to yellow. If the current leg in the flight plan is a heading leg, HDG LEG is annunciated in magenta beneath the aircraft symbol. The current GPS CDI scale setting is displayed as System CDI on the AUX - System Setup Page and the fullscale deflection setting may also be changed (2.0 nm, 1.0 nm, 0.3 nm, or Auto) from this page. If the selected scaling is smaller than the automatic setting for enroute and terminal phases, the CDI is scaled accordingly and the selected setting is displayed rather than the flight phase annunciation. Changing the selected GPS CDI setting: 1) Use the FMS Knob to select the AUX - System Setup Page on the MFD. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight Selected in the GPS CDI box. 4) Turn the small FMS Knob to highlight the desired setting and press the ENT Key. 5) To cancel the selection, press the FMS Knob or the CLR Key. Figure 2-29 System Setup Page, GPS CDI Setting When set to Auto (default), the GPS CDI scale automatically adjusts to the desired limits based upon the current phase of flight (Figure 2-30, Table 2-2). 82 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A Departure Terminal Enroute Terminal Refer to accompanying approach CDI scaling figures Approach 0.3 nm 1.0 nm 1.0 nm 2.0 nm 1.0 nm 0.3 nm CDI Full-scale Deflection FLIGHT INSTRUMENTS Missed Approach Figure 2-30 Automatic CDI Scaling • Once a departure procedure is activated, the CDI is scaled for departure (0.3 nm). • The system switches from departure to terminal CDI scaling (1.0 nm) under the following conditions: - The next leg in the departure procedure is not aligned with the departure runway - The next leg in the departure procedure is not a CA, CD, CF, CI, CR, DF, FA, FC, FD, FM, IF, or TF leg (see Glossary for leg type definitions) - After any leg in the departure procedure that is not a CA or FA leg • At 30 nm from the departure airport the enroute phase of flight is automatically entered and CDI scaling changes to 2.0 nm over a distance of 1.0 nm, except under the following conditions: - When navigating with an active departure procedure, the flight phase and CDI scale does not change until the aircraft arrives at the last departure waypoint (if more than 30 nm from the departure airport) or the leg after the last departure waypoint has been activated or a direct-to waypoint is activated. • If after completing the departure procedure the nearest airport is more than 200 nm away from the aircraft and the approach procedure has not yet commenced, the CDI is scaled for oceanic flight (4.0 nm). • Within 31 nm of the destination airport (terminal area), the CDI scale gradually ramps down from 2.0 nm to 1.0 nm over a distance of 1.0 nm, except under the following conditions: - Upon reaching the first waypoint of an arrival route that is more than 31 nm from the destination airport, the flight phase changes to terminal and the CDI scale begins to transition down from 2.0 nm to 1.0 nm over a distance of 1.0 nm. • During approach, the CDI scale ramps down even further (Figures 2-28 and 2-29). This transition normally occurs within 2.0 nm of the Final Approach Fix (FAF). The CDI switches to approach scaling automatically once the approach procedure is active or if Vectors-To-Final (VTF) are selected. - If the active waypoint is the FAF, the ground track and the bearing to the FAF must be within 45° of the final approach segment course. - If the active waypoint is part of the missed approach procedure, the active leg and the preceding missed approach legs must be aligned with the final approach segment course and the aircraft must not have passed the turn initiation point. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 83 2 nm FAF FAF CDI scale varies if VTF is activated 0.3 nm 1.0 nm angle based on database information course width 2 nm CDI Full-scale Deflection 0.3 nm angle set by system 350 ft CDI scale is set to the smaller of 0.3 nm or an angle set by the system 1.0 nm CDI Full-scale Deflection FLIGHT INSTRUMENTS Landing Threshold CDI scale varies if VTF is activated Figure 2-31 Typical LNAV and LNAV+V Approach Service Level CDI Scaling Figure 2-32 Typical LNAV/VNAV, LP, LP+V and LPV Approach Service Level CDI Scaling • When a missed approach is activated, the CDI scale changes to 0.3 nm. • The system automatically switches back to terminal mode under the following conditions: - The next leg in the missed approach procedure is not aligned with the final approach path - The next leg in the missed approach procedure is not a CA, CD, CF, CI, CR, DF, FA, FC, FD, FM, IF, or TF leg - After any leg in the missed approach procedure that is not a CA or FA leg Flight Phase Departure Terminal Enroute Oceanic Annunciation* DPRT TERM ENR OCN Approach (Non-precision) LNAV Approach (Non-precision with Vertical Guidance) Approach (LNAV/VNAV) Approach (LP) Approach (LP+V) Approach (LPV) Missed Approach Automatic CDI Full-scale Deflection 0.3 nm 1.0 nm 2.0 nm 4.0 nm 1.0 nm decreasing to 350 feet depending on variables (see Figure 2-31) LNAV + V L/VNAV LP LP+V 1.0 nm decreasing to a specified course width, then 0.3 nm, depending on variables (see Figure 2-32) LPV MAPR 0.3 nm * Flight phase annunciations are normally shown in magenta, but when cautionary conditions exist the color changes to yellow. Table 2-2 Automatic GPS CDI Scaling 84 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT INSTRUMENTS OBS MODE NOTE: VNV is inhibited while automatic waypoint sequencing has been suspended. Enabling Omni-bearing Selector (OBS) Mode suspends the automatic sequencing of waypoints in a GPS flight plan (GPS must be the selected navigation source), but retains the current Active-to waypoint as the navigation reference even after passing the waypoint. OBS is annunciated to the lower right of the aircraft symbol when OBS Mode is selected. While OBS Mode is enabled, a course line is drawn through the Active-to waypoint on the moving map. If desired, the course to/from the waypoint can now be adjusted. When OBS Mode is disabled, the GPS flight plan returns to normal operation with automatic sequencing of waypoints, following the course set in OBS Mode. The flight path on the moving map retains the modified course line. GPS Selected Extended Course Line OBS Mode Enabled Pressing the OBS Softkey Enables OBS Mode Pressing the OBS Softkey Again Disables OBS Mode Figure 2-33 Omni-bearing Selector (OBS) Mode Enabling/disabling OBS Mode while navigating a GPS flight plan: 1) Press the OBS Softkey to select OBS Mode. 2) Turn the CRS Knob to select the desired course to/from the waypoint. Press the CRS Knob to synchronize the Selected Course with the bearing to the next waypoint. 3) Press the OBS Softkey again to return to automatic waypoint sequencing. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 85 FLIGHT INSTRUMENTS As the aircraft crosses the missed approach point (MAP), automatic approach waypoint sequencing is suspended. SUSP appears on the HSI at the lower right of the aircraft symbol. The OBS Softkey label changes to indicate the suspension is active as shown in Figure 2-34. Selecting the SUSP Softkey, deactivates the suspension and resumes automatic sequencing of approach waypoints. SUSP Annunciation SUSP Softkey Figure 2-34 Suspending Automatic Waypoint Sequencing 86 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT INSTRUMENTS 2.2 SUPPLEMENTAL FLIGHT DATA NOTE: Selecting the DFLTS Softkey turns off the metric altimeter display, the Inset Map, and wind data display. In addition to the flight instruments, the PFDs also display various supplemental information, including temperatures, wind data, and Vertical Navigation (VNV) indications. TEMPERATURE DISPLAYS The Total and Static air temperatures (TAT and SAT) are displayed in the lower left of the PFD under normal conditions, or underneath the Airspeed Indicator in reversionary display mode. Both are displayed in degrees Celsius (°C) or Fahrenheit (°F) as configured by the installation personnel. Normal Display Reversionary Mode Figure 2-35 Total and Static Air Temperatures 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 87 FLIGHT INSTRUMENTS WIND DATA Wind direction and speed in knots can be displayed relative to the aircraft in a window to the upper left of the HSI. When the window is selected for display, but wind information is invalid or unavailable, the window displays ‘NO WIND DATA’. Valid wind data can be displayed in three different ways: Option 1 Option 2 Option 3 No Data Figure 2-36 Wind Data Displaying wind data: 1) Press the PFD Softkey. 2) Press the WIND Softkey to display wind data below the Selected Heading. 3) Press one of the OPTN softkeys to change how wind data is displayed: • OPTN 1: Wind direction arrows with numeric headwind/tailwind and crosswind components • OPTN 2: True wind direction arrow with numeric True direction and numeric speed • OPTN 3: Wind direction arrow with headwind (H) or tailwind (T) and crosswind (X) speed components 4) To remove the window, press the OFF Softkey. 88 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT INSTRUMENTS VERTICAL NAVIGATION (VNV) INDICATIONS When a VNV flight plan has been activated, VNV indications (VNV Target Altitude, RVSI, VDI) appear on the PFD in conjunction with the “TOD within 1 minute” visual annunciation and “Vertical track” voice alert. See the Flight Management and AFCS sections for details on VNV features. VNV indications are removed from the PFD according to the criteria listed in Table 2-3. Top of Descent Message VNV Target Altitude Vertical Deviation Indicator Required Vertical Speed Indicator GPS is Selected Navigation Source Enroute Phase of Flight Figure 2-37 Vertical Navigation Indications (PFD) VNV Indication Removed Required Vertical Vertical VNV Target Speed (RVSI) Deviation (VDI) Altitude Aircraft > 1 min before the next TOD due to flight plan change X X X VNV cancelled (CNCL VNV Softkey selected on MFD) X X X Distance to active waypoint cannot be computed due to unsupported flight plan leg type (see Flight Management X X X Section) Aircraft > 250 feet below active VNV Target Altitude X X X Current crosstrack or track angle error has exceeded limit X X X Active altitude-constrained waypoint can not be reached within X X maximum allowed flight path angle and vertical speed Criteria Table 2-3 VNV Indication Removal Criteria 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 89 FLIGHT INSTRUMENTS 2.3 PFD ANNUNCIATIONS AND ALERTING FUNCTIONS The following annunciations and alerting functions are displayed on the PFD. Refer to Appendix A for more information on alerts and annunciations. SYSTEM ANNUNCIATIONS The System Messages Window conveys messages to the flight crew regarding problems with the Prodigy® System. When a new message is issued, the MSG Softkey flashes to alert the flight crew. It continues to flash until selected, which opens the System Messages Window and acknowledges the message(s) which initiated the flashing. When the window is open, messages for which the trigger conditions no longer exist turn gray. Messages generated while the window is open are not automatically displayed, but cause the MSG Softkey to begin flashing again. Pressing the MSG Softkey while the System Messages Window is open closes the window, unless the MSG Softkey is flashing. Critical values generated by redundant sensors are monitored by comparators. If differences in the sensors exceed a specified amount, the Comparator Window appears in the upper right corner of the PFD and the discrepancy is annunciated in the Comparator Window as a MISCOMP (miscompare). If one or both of the sensed values are unavailable, it is annunciated as a NO COMP (no compare). Reversionary sensor selection is annunciated in a window on the right side of the PFD. These annunciations reflect reversionary sensors selected on one or both PFDs. Pressing the SENSOR Softkey accesses the ADC1, ADC2, ADCSTBY, AHRS1, AHRS2, and ATTSTBY softkeys. These softkeys allow switching of the sensors being viewed on each PFD. With certain types of sensor failures, the system may make sensor selections automatically. The GPS sensor cannot be switched manually. Comparator Window Reversionary Sensor Window CAS Annunciation Window Messages Window Softkey Annunciation Figure 2-38 Prodigy Alerting System 90 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT INSTRUMENTS MARKER BEACON ANNUNCIATIONS Marker Beacon Annunciations are displayed on the PFD to the left of the Selected Altitude. Outer marker reception is indicated in blue, middle in yellow, and inner in white. Refer to the Audio Panel and CNS Section for more information on Marker Beacon Annunciations. Outer Marker Middle Marker Inner Marker Altimeter Figure 2-39 Marker Beacon Annunciations TRAFFIC ANNUNCIATIONS Traffic is displayed symbolically on the Inset Map (PFD), the Navigation Map Page (MFD), and various other MFD page maps. Refer to the Hazard Avoidance Section and Appendix F for more details about the Traffic Information Service (TIS) and optional Traffic Collision Avoidance System II (TCAS II). When a Traffic Advisory (TA) or TCAS II Resolution Advisory (RA) detected, the following automatically occur: • The PFD Inset Map is enabled, displaying traffic. • A flashing black-on-yellow (TA) TRAFFIC annunciation or white-on red (RA) TRAFFIC annunciation appears to the top left of the Attitude Indicator for five seconds and remains displayed until no TAs or RAs are detected in the area. • One or more traffic voice alerts are generated. • For TCAS II installations with an active RA, vertical guidance pitch cues will appear on the Attitude Indicator and Vertical Speed Indicator; see the Hazard Avoidance Section for details about TCAS II. PFD TA Annunciation Traffic Symbols PFD RA Annunciation (TCAS II Only) PFD Inset Map with TIS Traffic Displayed Figure 2-40 Traffic Annunciation and Inset Map with Traffic Displayed 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 91 FLIGHT INSTRUMENTS TAWS ANNUNCIATIONS Terrain Awareness and Warning System (TAWS) annunciations appear on the PFD to the left of the Selected Altitude readout. In TAWS-A installations, additional annunciations also appear above the Roll Scale. Refer to the Hazard Avoidance Section and Appendix A for information on TAWS alerts and annunciations. Figure 2-41 Example TAWS-A Annunciations ALTITUDE ALERTING The Altitude Alerting function provides visual and audio alerts when approaching the Selected Altitude. Whenever the Selected Altitude is changed, Altitude Alerting is reset. Altitude Alerting is based on the altitude information shown on PFD1. Altitude Alerting is independent of the AFCS. The following occur when approaching the Selected Altitude: • Upon passing through 1000 feet of the Selected Altitude, the Selected Altitude Box changes to black text on a light blue background, flashes for five seconds, and an aural tone is generated. • When the aircraft passes within 200 feet of the Selected Altitude, the Selected Altitude changes to light blue text on a black background and flashes for five seconds. • After reaching the Selected Altitude, if the aircraft flies outside the deviation band (±200 feet of the Selected Altitude), the Selected Altitude Box changes to yellow text on a black background, flashes for five seconds. In addition, two aural tones are generated followed by an “Altitude” voice alert. Within 1000 ft Within 200 ft Deviation of ±200 ft Figure 2-42 Altitude Alerting Visual Annunciations 92 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT INSTRUMENTS LOW ALTITUDE ANNUNCIATION NOTE: A Low Altitude Annunciation is available only when SBAS is available, and TAWS alerting is inhibited, has failed, or is unavailable. When the Final Approach Fix (FAF) is the active waypoint in a RNAV GPS approach using vertical guidance, a Low Altitude Annunciation may appear if the current aircraft altitude is at least 164 feet below the prescribed altitude at the FAF. A black-on-yellow LOW ALT annunciation appears to the top left of the altimeter, flashing for several seconds then remaining displayed until the condition is resolved. Figure 2-43 Low Altitude on GPS SBAS Approach MINIMUM DESCENT ALTITUDE/DECISION HEIGHT ALERTING For altitude awareness, a Minimum Descent Altitude (MDA) or Decision Height (DH), based on barometric altitude, temperature compensated barometric altitude, or optional radar altimeter height. When active, the altitude setting is displayed to the lower left of the altimeter and with a bug at the corresponding altitude along the altimeter (once the altitude is within the visible range of the tape). The following visual annunciations alert the pilot when approaching MDA or DH: • When the aircraft altitude descends to within 2500 feet of the MDA/DH setting, the BARO MIN, RA MIN, or COMP MIN box appears with the altitude in light blue (or magenta for COMP MIN) text. The bug appears on the altitude tape in light blue (or magenta for COMP MIN) once in range. • When the aircraft passes through 100 feet of the MDA/DH, the bug and text appear white. • Once the aircraft reaches MDA/DH, the bug and text appear yellow and the system issues a “Minimums. Minimums” voice alert. Within 2500 ft Within 100 ft Altitude Reached Barometric Minimum Bug Barometric Minimum Box Figure 2-44 Barometric MDA/DH Alerting Visual Annunciations 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 93 FLIGHT INSTRUMENTS Alerting is inhibited while the aircraft is on the ground and until the aircraft reaches 150 feet above the setting for the alert. If the aircraft proceeds to climb after having reached the MDA/DH, once it reaches 50 feet above the MDA/DH, alerting is disabled. The MDA/DH may be set from either PFD and is synchronized on both PFDs. The function is reset when the power is cycled. NOTE: The temperature at the destination can be entered in the REFERENCES Window on the PFD, or TEMPERATURE COMPENSATION Window on the MFD. There is only one compensation temperature for the system, therefore, changing the temperature will affect both the loaded approach altitudes and the minimums. Refer to the Flight Management section for information about applying temperature compensation to approach altitudes. Setting the Minimum Descent Altitude/Decision Height: 1) Press the TMR/REF Softkey. 2) Turn the large FMS Knob to highlight the Minimums field (Figure 2-45). 3) Turn the small FMS Knob to select from barometric altitude (BARO), barometric altitude with temperature compensation (TEMP COMP), or radar altimeter (RAD ALT). OFF is selected by default. Press the ENT Key or turn the large FMS Knob to highlight the next field. 4) Use the small FMS Knob to enter the desired altitude (BARO or TEMP COMP from zero to 16,000 feet, RAD ALT from zero to 2,500 feet ). If TEMP COMP was selected, a field for entering the airport temperature appears. Press the ENT Key or turn the large FMS Knob to highlight this field, and use the small FMS Knob to enter the temperature. 5) To remove the window, press the CLR Key or press the TMR/REF Softkey. Figure 2-45 BARO and TEMP COMP MDA/DH 94 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT INSTRUMENTS RADAR ALTIMETER When the radar height (the aircraft altitude above ground level detected by the radar altimeter) is between zero and 2500 feet, the current value is displayed in green above the selected course/desired track box (Figure 2-46). Display of radar height becomes more sensitive as the height above ground decreases (Table 2-4). Radar Altimeter Figure 2-46 Current Radar Height Radar Height Range Shown to Nearest 0 to 200 feet 5 feet 200 to 1500 feet 10 feet 1500 to 2500 feet 50 feet Table 2-4 Radar Altimeter Sensitivity When the radar altimeter is selected as the altitude source for the minimum descent altitude/decision height alerting function (Figure 2-47), the color of the radar height readout changes from green to yellow upon descent to or below this altitude (Figure 2-48). Refer to the Minimum Descent Altitude/Decision Height Alerting discussion in this section for more information about this function. Figure 2-47 RAD ALT Setting (Timer/References Window) Figure 2-48 RA as Altitude Source for MDA/DH 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 95 FLIGHT INSTRUMENTS A ground line (Figure 2-49) is shown on the Altimeter to display the aircraft’s height relative to the ground. Gray diagonal lines appear below the ground line. If the radar altimeter data becomes invalid, the message ‘RA FAIL’ is displayed in yellow instead of the current radar height (Figure 2-47). Radar Altimeter Ground Line Radar Altimeter Minimums Box Figure 2-49 Altimeter Displaying the Ground Line (RAD ALT) Figure 2-50 Radar Altimeter Invalid Data 96 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT INSTRUMENTS 2.4 ABNORMAL OPERATIONS ALTITUDE ALERTING Under normal conditions, the Altitude Alerting function is based on the Selected Altitude shown on PFD1. If the MFD is operating in Reversionary Mode, the Selected Altitude shown on the MFD will be used for Altitude Alerting instead. If the MFD has also failed, then Altitude Alerting will be based on the PFD 2 Selected Altitude. ABNORMAL GPS CONDITIONS The annunciations listed in Table 2-5 can appear on the HSI when abnormal GPS conditions occur. Refer to the Flight Management Section for more information on Dead Reckoning (DR) Mode. Annunciation LOI INTEG OK DR Location Lower left of aircraft symbol Lower left of aircraft symbol Upper right of aircraft symbol Description Loss of Integrity Monitoring–GPS integrity is insufficient for the current phase of flight Integrity OK–GPS integrity has been restored to within normal limits (annunciation displayed for five seconds) Dead Reckoning–System is using projected position rather than GPS position to compute navigation data and sequence active flight plan waypoints Table 2-5 Abnormal GPS Conditions Annunciated on HSI Figure 2-51 Example HSI Annunciations DR Mode causes the CDI to be removed from the display (when GPS is the selected navigation source) and the following items on the PFD to be shown in yellow: • Current Track Bug • Wind data and pointers in the Wind Data Box on the PFD • Distances in the Bearing Information windows • GPS bearing pointers • Groundspeed It is important to note that estimated navigation data supplied by the system in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation. See the Flight Management section for more information about DR Mode 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 97 FLIGHT INSTRUMENTS HEADING FAILURE MODES If the system is unable to determine the aircraft heading, but GPS-based track information is available, the HSI displays the ground track instead of heading using HSI Track Mode. In this mode, a magenta ‘TRK’ annunciation and track readout appear on the HSI. In addition, a yellow ‘HDG’ annunciation with a red X appear above the ‘TRK’ annunciation to indicate the HSI is displaying track instead of heading. If both the heading and track are unavailable, the HSI displays a yellow ‘HDG’ annunciation with a red X over the heading readout box. The system also removes directional numbers and letters from the HSI. HSI Track Mode (Heading Unavailable, Track Available) Heading and Track Unavailable Figure 2-52 Heading Failure Displays on the HSI NOTE: When heading information is unavailable, the system removes the bearing pointers from the HSI, and removes wind data from the PFD and navigation maps. UNUSUAL ATTITUDES When the aircraft enters an unusual pitch attitude, red extreme pitch warning chevrons pointing toward the horizon are displayed on the Attitude Indicator, starting at 50˚ above and 30˚ below the horizon line. Nose High Nose Low Figure 2-53 Pitch Attitude Warnings 98 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT INSTRUMENTS If pitch exceeds +30˚/-20˚ or bank exceeds 65˚, some information displayed on the PFD is removed. The Altimeter and Airspeed, Attitude, Vertical Speed, and Horizontal Situation indicators remain on the display and the Bearing Information, Alerts, and Annunciation windows can be displayed during such situations. The following information is removed from the PFD (and corresponding softkeys are disabled) when the aircraft experiences unusual attitudes: • Traffic Annunciations • Transponder Status Box – ADF/DME Tuning • AFCS Annunciations • System Time • Flight director Command Bars • PFD Setup Menu • Minimum Descent Altitude/ Decision Height readout • Inset Map • Outside air temperature (OAT) • Windows displayed in the lower right corner of the PFD: • Vertical Deviation, Glideslope, and Glidepath Indicators • DME Information Window – Timer/References • Altimeter Barometric Setting • Wind data – Nearest Airports • Selected Altitude • Selected Heading Box – Flight Plan • VNV Target Altitude • Selected Course/Desired Track Box – Messages • Airspeed Reference 190-00728-06 Rev. A – Procedures Embraer Prodigy® Flight Deck 100 Pilot’s Guide 99 FLIGHT INSTRUMENTS Blank Page 100 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ENGINE & AIRFRAME SYSTEMS SECTION 3 ENGINE AND AIRFRAME SYSTEMS NOTE: Refer to the Airplane Flight Manual (AFM) for limitations. The Prodigy® Integrated Flight Deck offers improved flight operations and reduces crew workload by automatically monitoring critical system parameters and providing system alerts during all phases of flight using the following: • The Engine Indication System (EIS) displays electrical, fuel, engine, pressurization, and flight control information on the left side of the Multi Function Display (MFD). • Synoptics pages are provided for monitoring the status of the doors, brakes, hydraulics, oxygen, pressurization, environmental control, electrical, fuel, and de-icing systems. In combination with these, aural alerts, additional avionics messages, and master indicators are used to inform the crew of aberrant flight conditions. The system also provides maintenance data for the ground crew. MFD EIS Display Figure 3-1 EICAS (Normal) 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 101 ENGINE & AIRFRAME SYSTEMS In the event of a display failure, depending on the failed display(s), the operating display(s) may be re-configured to present Primary Flight Display (PFD) symbology together with condensed EIS information (refer to the System Overview for more information about Reversionary Mode). CAS Window EIS Display Figure 3-2 EICAS (Reversionary Mode) The SYSTEM Softkey accesses the EIS softkeys. The STATUS, ECS, ELEC, FUEL, ICEPROT, and ENG MNT softkeys or the small FMS Knob access the Synoptic pages (see Section 3.2). To return to the previous softkey level and exit the Synoptics pages, select the BACK Softkey, press the CLR Key, or turn the large FMS Knob. SYSTEM ENG SET CPDLC LFE STATUS ECS CON CLB OAT OAT ELEC FUEL ICEPROT ENG MNT BACK ATR ON ATR OFF ACCEPT BACK CHKLIST Press the BACK Softkey to return to the previous level softkeys. FMS LFE CPDLC +500 FT -500 FT +50 FT ACCEPT -50 FT CLEAR E1 CLEAR E2 BACK BACK CHKLIST Figure 3-3 EIS and Synoptics Softkeys 102 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ENGINE & AIRFRAME SYSTEMS Accesses the FADEC settings softkeys; displays the Takeoff Data Set Window when aircraft is parked or taxiing Selects the continuous thrust rating CON* Selects the maximum climb thrust rating CLB* Increases the takeoff outside air temperature (OAT) setting in one-degree Celsius (°C) OAT ** increments Decreases the takeoff OAT setting in one-degree Celsius (°C) increments OAT ** Enables Automatic Thrust Reserve (ATR) ATR ON** Disables ATR ATR OFF** Confirms the selected takeoff settings ACCEPT** Accesses softkeys for manually setting the Landing Field Elevation (LFE) • LFE Sets current flight plan destination elevation as displayed LFE FMS LFE Increases currently displayed LFE value by 500 ft +500 FT Decreases currently displayed LFE value by 500 ft -500 FT Increases currently displayed LFE value by 50 ft +50 FT Decreases currently displayed LFE value by 50 ft -50 FT Confirms the LFE setting and returns to the previous softkey level ACCEPT Displays the Status Synoptics Page • STATUS Displays the Environmental Control System (ECS) Synoptics Page • ECS Displays the Electrical Synoptics Page • ELEC Displays the Fuel Synoptics Page • FUEL Displays the Ice Protection Synoptics Page • ICEPROT • ENG MNT*** Displays the Engine Maintenance Page CLEAR E1*** Clears Engine 1 exceedances and long time dispatch faults CLEAR E2*** Clears Engine 2 exceedances and long time dispatch faults • ENG SET * Softkey disabled while aircraft is on the ground ** Softkey disabled while aircraft is in the air *** Enabled only while the aircraft is on the ground and engines are turned off 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 103 ENGINE & AIRFRAME SYSTEMS 3.1 ENGINE INDICATION SYSTEM (EIS) EIS information is presented using gauges and digital readouts. During normal operating conditions, gauge pointers and readout text appear in green. When unsafe operating conditions occur, gauge pointers and readouts change color to indicate caution (yellow) or warning (red). Refer to each indicator description for additional details on display behavior. If the time limit for an unsafe condition is exceeded, the color of the pointers and digits may change to denote an increase in priority level. Parameters out of the range of the readout display as a red “X”. If sensor data for a parameter becomes invalid or unavailable, a red “X” is displayed across the indicator and/or readout. 1 1 2 2 3 3 4 4 5 5 6 6 7 7 8 9 9 10 8 10 11 11 Figure 3-5 EIS Display (Reversionary) Figure 3-4 EICAS Display (Normal) 1 Engine Fan Rotation Speed 4 Oil Pressure and Temperature 8 Spoiler Status 2 Interstage Turbine Temperature (ITT) Engine High Pressure Compressor Rotation Speed 5 Fuel Display 9 Landing Gear Status 6 Battery Voltmeter 10 Flap Indicator 7 Cabin Display 11 Trim Indicator 3 104 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ENGINE & AIRFRAME SYSTEMS TAKEOFF DATA SET WINDOW When the aircraft is parked or is taxiing, the Outside Air Temperature (OAT) for the departure airport can be set and Automatic Thrust Reserve (ATR) enabled/disabled in the Takeoff Data Set Window. Figure 3-6 Takeoff Data Set Window Setting the Outside Air Temperature (OAT): 1) Select the SYSTEM Softkey. 2) Select the ENG SET Softkey to display the Takeoff Data Set Window. 3) To adjust the temperature in 1 °C increments, use the OAT and OAT softkeys, 4) If desired, change the ATR status while the Takeoff Data Set Window is displayed. 5) To confirm the selected takeoff settings and close the Takeoff Data Set Window, select the ACCEPT Softkey, Or: To cancel the operation, select the BACK Softkey. On aircraft electrical power-up, Automatic Thrust Reserve (ATR) is enabled by default. ATR status (defined in Table 3-1) is shown at the top of the EIS Display (Figure 3-7). Indication* ATR ATR TO - RSV Description ATR enabled in both engines ATR armed in both engines, but inactive ATR activated in at least one engine * When no indication is shown, ATR has not been enabled or armed in both engines. Table 3-1 Automatic Thrust Reserve (ATR) Status 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 105 ENGINE & AIRFRAME SYSTEMS Disabling/enabling Automatic Thrust Reserve (ATR): 1) Select the SYSTEM Softkey. 2) Select the ENG SET Softkey to display the Takeoff Data Set Window. 3) To disable ATR, select the ATR OFF Softkey; Or: To enable ATR, select the ATR ON Softkey. 4) If desired, change the OAT while the Takeoff Data Set Window is displayed. 5) To confirm the selected takeoff settings and close the Takeoff Data Set Window, select the ACCEPT Softkey, Or: To cancel the operation, select the BACK Softkey. ENGINE INDICATIONS Automatic Thrust Reserve Status Thrust Rating Commanded N1 Rating Engine Fan Speed N1 Transient Limit Current Speed Control Arc Thrust Rating Max Speed N1 for Thrust Rating Max Speed ITT Steady State Limit ITT Transient Limit Interstage Turbine Temperature Ignition Status Engine High Pressure Compressor Speed Oil Pressure Oil Temperature Figure 3-7 Engine and Oil Indications The upper portion of the EIS Display is devoted to showing indications for the engines: engine stage rotation speeds (N1 and N2; shown as percentages), ATR status, thrust rating information, Interstage Turbine Temperatures (ITT; degrees Celsius, °C), and oil pressure (pounds per square inch, psi) and temperature (°C). The N1 gauges indicate the engine fan rotation speeds, while the N2 readouts show the engine high pressure compressor rotation speeds. Both are shown as percentages. Values and limits are obtained from the Full Authority Digital Engine Controller (FADEC). 106 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ENGINE & AIRFRAME SYSTEMS On the N1 gauges, the following indications can be displayed: • Commanded N1 Rating (based on Thrust Lever Angle, TLA, position) – When the current N1 value is below the commanded rating, a light blue arc is drawn from the current to the commanded N1 value. • N1 value corresponding to the Thrust Rating Maximum Speed (shown as a light blue T-shaped bug) • Current Speed Control N1 value (shown as a green arc) • Engine shutdown (normal operations) – When the engines are shutting down normally, the N1 gauges display a light blue “OFF” annunciation (Figure 3-8). Figure 3-8 Engine Shutdown Indication Interstage Turbine Temperatures (ITT) values and limits are obtained from the Full Authority Digital Engine Control (FADEC). Ignition status appears below the ‘IGN’ label beside the ITT scales (A, B, AB, or OFF). THRUST RATING The thrust rating for the engines is shown at the center top of the EIS Display, above and between the N1 gauges (see Table 3-2 for indications). The maximum value of the speed range (in %) for the displayed thrust rating is shown above each N1 gauge. While the aircraft is in the air, the rating can be changed to suit the conditions for maximum climb or continuous thrust. Indication CRZ CLB CON TO GA Thrust Rating Cruise Climb Continuous Takeoff Go Around Table 3-2 Thrust Rating Indications Selecting a thrust rating: 1) Select the SYSTEM Softkey. 2) Select the ENG SET Softkey 3) To choose the continuous thrust rating, select the CON Softkey, Or: To choose the maximum climb thrust rating, select the CLB Softkey. 4) Select the BACK Softkey to return to the previous softkey level. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 107 ENGINE & AIRFRAME SYSTEMS CURRENT SPEED CONTROL (CSC) Current Speed Control (CSC), if available, can be activated while the autopilot is engaged and Altitude Hold Mode is active. During CSC, the FADEC varies engine thrust to maintain the desired airspeed (green airspeed bug), within a certain control range. When CSC is active, a green arc appears on the N1 gauges, at values corresponding to the current speed selected (Figure 3-9). The N1 gauge flashes ‘LIM’ (black text on yellow background) if the CSC maximum authority limit has been reached for the corresponding engine. Figure 3-9 N1 Current Speed Control Limit Selecting Current Speed Control (CSC): 1) With the autopilot engaged, select Altitude Hold Mode (see the AFCS Section for details). 2) Press the CSC Key (on the AFCS Control Unit). FUEL AND ELECTRICAL INDICATIONS The fuel display is located beneath the oil indicators and shows the fuel flow in pounds per hour (pph) and the fuel quantity in pounds (lb) for each engine, the total fuel quantity, and the fuel tank temperature in °C. Fuel display can also be configured by the factory for kilograms. Engine Fuel Flow Tank Fuel Quantity Total Fuel Quantity Fuel Temperature Figure 3-10 Fuel Display Voltages for batteries 1 and 2 are shown as readouts below the fuel indications. Figure 3-11 Electrical Display 108 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ENGINE & AIRFRAME SYSTEMS CABIN PRESSURIZATION The Cabin Display shows cabin pressurization information (cabin altitude and rate of change, differential cabin pressure) along with the Landing Field Elevation (LFE) and oxygen system pressure. The trend of cabin pressure altitude rate change is indicated by a green arrow beside the rate readout. The LFE is set automatically based on the destination in the active flight plan by pressing the FMS LFE Softkey, but can also be adjusted manually by the pilot. Automatically entered values appear in green; if the value is entered by the pilot, it changes to light blue. Pilot selected LFE flashes yellow for 30 seconds when a difference of >5 feet occurs. A red “X” is displayed if the LFE is out of range or the data source is invalid. If the landing field elevation is high enough, the indication “HI FIELD” is shown at the top of the Cabin Display and the cabin altitude caution and warning thresholds are increased to avoid generation of nuisance alert indications. High Landing Field Elevation Pressure Altitude Pressure Change Rate Pressure Differential Landing Field Elevation Oxygen System Pressure Figure 3-12 Cabin Display Setting the displayed landing field elevation: 1) Select the SYSTEM Softkey. 2) Select the LFE Softkey. 3) Select the FMS LFE Softkey to set the LFE to the value for the destination airport in the current flight plan. Or: Use the ±500 and ±50 FT softkeys to set the desired elevation between -1,000 and 14,000 feet. 4) To confirm the new LFE value, select the ACCEPT Softkey. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 109 ENGINE & AIRFRAME SYSTEMS SPOILER AND LANDING GEAR Spoiler and landing gear statuses are shown using the indications in Tables 3-3 and 3-4, respectively. Spoiler Status Indication Spoiler not Configured Nose Landing Gear Description Landing Gear Down Right-side Main Landing Gear Left-side Main Landing Gear Landing Gear Up Figure 3-13 Spoiler and Landing Gear Indications Indication SPDBRK FAIL CLOSED GND SPLR SPDBRK Landing Gear Transitioning (Normal) Description Invalid information Landing Gear Locked Down (Abnormal) Spoilers out of takeoff configuration Spoilers failed Landing Gear Locked Up (Abnormal) Spoilers retracted Ground spoilers deployed Speedbrakes deployed Landing Gear Transitioning (Abnormal) Table 3-4 Landing Gear Position Indications Table 3-3 Spoiler Indications FLAPS AND TRIM Flap deflection is normally displayed beneath the trim indications using a rotating pointer and a green readout indicating the flap lever setting (0, 1, 2, 3, or FULL). A light blue bug marks the selected flap position. When the flap is in motion, the readout is dashed. If the position data becomes invalid, the flap pointer is removed from the display, and the readout is displayed with a red “X”. Pitch, roll, and yaw trim indications are shown along scales at the bottom of the EIS Display. If the trim information becomes invalid, the pointers are removed and the readout (for pitch) is displayed with a red “X”. Flap Position Flap Lever Setting Flap Selected Bug Figure 3-14 Flap and Trim Indications 110 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ENGINE & AIRFRAME SYSTEMS 3.2 SYNOPTICS The Synoptics pages show current conditions of certain aircraft functionalities on aviation system diagrams, reducing workload by allowing the flight crew to rapidly analyze the situation. Aircraft systems graphically depicted in the synoptic diagrams include: • Ice protection system • Fuel system • Brake system • Hydraulics system • Doors • Oxygen system • Electrical system • Pressurization system • Environmental system SYSTEM STATUS The Status Synoptics Page is displayed after the power-up splash screen is acknowledged on the MFD. The aircraft diagram displays open passenger and emergency doors in red and open baggage doors in yellow. 5 4 6 3 7 2 8 1 11 9 10 1 True Airspeed (TAS) 7 Hydraulic Pressure 2 International Standard Atmosphere (ISA) 8 Oxygen 3 Total Air Temperature (TAT) 9 Emergency Brake Accumulator Pressure 4 Static Air Temperature (SAT) 10 Door Status 5 Flight ID 11 Electrical Status 6 Engine Short Dispatch Message Box Figure 3-15 System Status Synoptics Page 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 111 ENGINE & AIRFRAME SYSTEMS ENVIRONMENTAL CONTROL SYSTEM (ECS) 2 1 3 5 4 6 8 7 10 9 12 11 13 14 15 16 17 18 19 20 1 Cockpit Temperature Setting 11 Bleed Line 1 (Left) Pressure 2 Actual Cockpit Temperature 12 Bleed Line 2 (Right) Pressure 3 Cockpit Evaporator Fan 13 Heat Exchanger Pack Cooling Circuit 4 Cabin Temperature Setting 14 Cockpit Duct Temperature Setting 5 Actual Cabin Temperature 15 Cabin Duct Temperature Setting 6 Cabin Evaporator Fan 16 Pressure Regulating Shutoff Valve (PRSOV) 1 7 Ram Air Duct 17 Pressure Regulating Shutoff Valve (PRSOV) 2 8 Ram Air Valve (RAV) 18 Ground Cooling Fan (GCF) 9 Flow Control Shutoff Valve (FCV) 1 19 Vapor Cycle System (VCS) 10 Flow Control Shutoff Valve (FCV) 2 20 Outflow Valve (OFV) Status* * Outflow valve (OFV) status is displayed only while the aircraft is parked or taxiing. Figure 3-16 Environmental Control System Synoptics Page 112 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ENGINE & AIRFRAME SYSTEMS Lines between icons on the diagram denote ducting. Icons shown in green are operating normally. A white icon may indicate that a unit is off or not otherwise operating normally (see Table 3-5). A red “X” indicates failure of a unit. Unit Icons and Descriptions Fan On Off On Off On Off Heat Exchanger Vapor Cycle System PRSOV Open with flow Open, no flow Closed Ram Air Duct From NACA Scoop Airborne On ground Ram Air Valve Closed Open, airborne Open, on ground Table 3-5 Environmental Control System Unit Status Indications 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 113 ENGINE & AIRFRAME SYSTEMS ELECTRICAL The Electrical Synoptics Page uses a diagram of the aircraft’s electrical system to display the system status. The generators, ground power supply (GPU), batteries, and buses are shown in green to denote normal operation. Color of the units changes depending on the condition (Table 3-6). A red “X” over a component indicates invalid data or a failed unit. Battery Bus Generator Ground Power Unit Figure 3-17 Electrical Synoptics Page Unit Icons and Descriptions Generator On Bus Off bus Off Normal Abnormal Normal Abnormal Battery Table 3-6 Electrical System Unit Status Indications 114 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ENGINE & AIRFRAME SYSTEMS FUEL The Fuel Synoptics Page displays the status of the fuel tanks and feed system. A red “X” over a component indicates invalid data or a failed unit. 1 2 3 4 5 6 7 1 Total Fuel 9 Right Feed Ejector 8 9 2 Fuel Used 10 Fuel 1 SOV 10 11 3 Fuel Transfer SOV 11 Fuel 2 SOV 12 13 4 Left Tank Fuel Quantity 12 LH Pressure Switch 5 Right Tank Fuel Quantity 13 RH Pressure Switch 14 15 6 Left DC Pump 14 Left Engine Feed Line 7 Right DC Pump 15 Right Engine Feed Line 8 Left Feed Ejector Figure 3-18 Fuel Synoptics Page Unit Icons and Descriptions Fuel Line Operating Not operating Feed Ejector Not operating Operating Fuel Pressure Switch Operating Valve Not operating Open with flow Open, no flow In transit Closed DC Pump Not operating Operating Fuel Transfer Valve Open with flow In transit Closed Table 3-7 Fuel System Unit Status Indications 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 115 ENGINE & AIRFRAME SYSTEMS ICE PROTECTION SYSTEM When the ice protection system is operating normally, all components are shown in green on the system diagram. Items in white indicate components which are off. A red “X” over a component indicates invalid data or a failed unit. 1 1 2 2 3 4 5 6 7 8 9 10 11 12 2 1 Windshield Heaters 7 EAI 1 Valve and Bleed Line 2 Boot Lines and Valves 8 EAI 2 Valve and Bleed Line 3 Inboard Ejector Flow Control Valve (EFCV) 9 Pressure Regulating Shut-Off Valve 1 (PRSOV 1) 4 Outboard Ejector Flow Control Valve (EFCV) 10 Pressure Regulating Shut-Off Valve 2 (PRSOV 2) 5 Engine Anti Ice 1 Bleed Duct and Lip Skin 11 STAB Ejector Flow Control Valve (EFCV) 6 Engine Anti Ice 2 Bleed Duct and Lip Skin 12 Ice Protection Bleed Duct Figure 3-19 Ice Protection Synoptics Page 116 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ENGINE & AIRFRAME SYSTEMS Unit Inboard/Outboard EFCV and PRSOV STB EFCV and EAI Valve Icons and Descriptions Open with flow Open, no flow Closed Open with flow Open, no flow Closed Table 3-8 Ice Protection System Unit Status Indications 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 117 ENGINE & AIRFRAME SYSTEMS ENGINE MAINTENANCE NOTE: Refer to the Airplane Flight Manual (AFM) for required actions. The Engine Maintenance Synoptics Page can only displayed when the aircraft is on the ground and both engines are off. Maintenance personnel can view status messages for engine dispatch items and the following engine parameter exceedance peaks and durations recorded by the FADEC for the last engine start-shutdown cycle: • Engine fan rotation speed (N1) • Inter Turbine Temperature (ITT) • Engine high pressure compressor rotation speed (N2) • Main oil temperature and Pressure • Fuel temperature If no peaks are detected, the values and times are displayed as dashes The data is cleared from the display using the CLEAR E1 and CLEAR E2 softkeys. The Engine Maintenance Page also displays the ITT and N1 trims that are loaded in each Engine Data Collection Unit (EDCU) Figure 3-20 Engine Maintenance Synoptics Page 118 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ENGINE & AIRFRAME SYSTEMS 3.3 ABNORMAL OPERATIONS NOTE: Refer to the Airplane Flight Manual (AFM) for corrective pilot actions. ENGINE If an engine failure occurs, besides the CAS message corresponding to the failed engine (“E1 FAIL” or “E2 FAIL”), the corresponding N1 gauge displays the annunciation “FAIL” in yellow inverse video with black text (Figure 3-23). Detection of an engine fire causes a CAS message corresponding to the engine on fire (“E1 FIRE” or “E2 FIRE”) in addition to the red inverse video annunciation “FIRE” to be displayed over the ITT gauge in white text (Figure 3-24). Figure 3-23 Engine Failure Indication Figure 3-24 Engine Fire Indication CABIN PRESSURIZATION If the cabin altitude (ALT) reaches a caution level, the readout displays black text on a yellow background. When cabin altitude is 10,000 feet or greater, the readout displays as a warning with white text on a red background, and the corresponding CAS message “CAB ALTITUDE HI” is issued. If low flow or a cabin leak is detected, the cabin pressure change rate readout displays white text on a red background, and the trend arrow turns red. Excessive cabin differential pressure (DELTA-P) causes the pressure readout to display a yellow background and black text; warnings are indicated with red background with white readout text. The CAS message “CAB DELTA-P FAIL” accompanies this condition. When oxygen system pressure (OXY) drops below 1590 PSI, the readout is indicated with black text on a white background; pressure below 730 PSI is shown with yellow text on a black background. The CAS message “OXY LO PRES” is also displayed. If the pilot selected landing field elevation (LFE) differs by more than five feet from the FMS LFE value, the LFE readout flashes yellow for 30 seconds. A red “X” is displayed over any readout on the Cabin Display that is invalid or out of range. Figure 3-25 Cabin Display with Excessive Change Rate 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 119 ENGINE & AIRFRAME SYSTEMS FLAPS The following denote abnormal flap conditions: • Flaps not in position for takeoff – Flap pointer and readout turn red with white text (Figures 3-26 and 3-27). • Flaps have failed or become jammed – Flap pointer and readout turn yellow with black text (Figure 3-28) • Flaps unavailable – Flap pointer is removed and readout turns white with black text (Figure 3-29) • Flaps position data invalid – Flap pointer and readout displayed with a red “X” Figure 3-26 Flaps Retracted at Takeoff Figure 3-27 Flaps at FULL (Landing) Position at Takeoff Figure 3-28 Flaps Failed Figure 3-29 Flaps Unavailable TRIM Aileron or rudder mistrim are denoted with yellow arrows pointing in the direction of mistrim on the Roll and Yaw Trim indicators (Figure 3-30). If takeoff configuration has been selected and the pitch trim position is not within the green band on the pitch trim scale, the pointers and readout turn red with white text (Figure 3-31). If an asymmetrical pitch trim condition exists, the pointers turn yellow and the readout is displayed with a Red “X” (Figure 3-32). Aileron Mistrim Rudder Mistrim Figure 3-30 Mistrim 120 Figure 3-31 Pitch Trim Outside Takeoff Configuration Embraer Prodigy® Flight Deck 100 Pilot’s Guide Figure 3-32 Asymmetrical Pitch Trim Condition 190-00728-06 Rev. A AUDIO PANEL AND CNS SECTION 4 AUDIO PANEL AND CNS 4.1 OVERVIEW The Communication/Navigation/Surveillance (CNS) system includes the Audio Panels, communication radios, navigation radios, and Mode S transponders. The System Overview Section provides a block diagram description of the Audio Panels and CNS system interconnection. CNS operation in the Embraer Phenom 100 is performed by the following: • Primary Flight Display (PFD) (2) • Multi Function Display (MFD) • Mode S Transponder (2) or TCAS II Mode S Transponder • Integrated Avionics Unit (2) • MFD Control Unit • Audio Panel (2) • GDR 66 VHF Data Link Transceiver • Controller Pilot Data Link Communications System (CPDLC) The MFD/PFD controls are used to tune the communication transceivers and navigation radios. The two Audio Panels provide the traditional audio selector functions of microphone and receiver audio selection. Each Audio Panel includes an intercom system (ICS) between the pilot, copilot, and passengers, a marker beacon receiver, and a COM clearance recorder. Ambient noise from the aircraft radios is reduced by a feature called Master Avionics Squelch (MASQ). When no audio is detected, MASQ processing further reduces the amount of background noise from the radios. The Mode S Transponders are controlled with softkeys and the FMS Knob located on the PFD. The Transponder Data Box is located to the left of the System Time Box. The data box displays the active four-digit code, mode, and a reply status (Figure 4-1). The Controller Pilot Data Link Communications System (CPDLC) provides data link communication between the aircraft and an Air Traffic Control facility. Communication is normally in the form of text message elements that resemble phraseology used in voice communications with ATC. The CPDLC system is intended for use in Europe with the Link 2000+ DLS (Data Link System) and will communicate with the ATN (Aeronautical Telecommunications Network) only. AUDIO PANEL VOLUME CONTROL Adjusting the master volume control affects all radio audio volume and airframe type warnings that are heard in the headsets (not the speaker) for the pilot or copilot side Audio Panel. Radio adjustments made on the MFD/PFD controls to compensate for the master volume change on the Audio Panel, also affect the radio levels for the other pilot. Independent radio volume adjustments made using the Audio Panel Master Volume controls affect only the audio heard in the corresponding crew position headset. Radio volume adjustments may be overridden by each crew position independently using the master volume control on the Audio Panel for the respective crew position. In addition, the master volume control for each Audio Panel affects all other system audio output to its designated crew position headset much like volume adjustments found on many aviation headsets. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 121 AUDIO PANEL AND CNS MFD/PFD CONTROLS AND FREQUENCY DISPLAY 1 2 3 4 5 6 7 8 9 10 11 12 Figure 4-1 MFD/PFD Controls, COM/NAV Frequency Tuning Boxes, and ADF/DME Tuning 122 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS 1 NAV VOL/ID Knob – Controls NAV audio volume level. Press to turn the Morse code identifier audio on and off. Volume level is shown in the NAV frequency field as a percentage. 2 NAV Frequency Transfer Key – Transfers the standby and active NAV frequencies. 3 NAV Knob – Tunes the standby frequencies for the NAV receiver (large knob for MHz; small knob for kHz). Press to move the tuning box (light blue box) and Frequency Transfer Arrow between NAV1 and NAV2. 4 NAV Frequency Box – Displays NAV standby and active frequency fields, volume, and station ID. The frequency of the NAV radio selected for navigation is displayed in green. 5 COM Frequency Box – Displays COM standby and active frequency fields and volume. The selected COM transceiver frequency is displayed in green. 6 COM Knob – Tunes the standby frequencies for the COM transceiver (large knob for MHz; small knob for kHz). Press to move the tuning box (light blue box) and Frequency Transfer Arrow between COM1 and COM2. 7 COM Frequency Transfer Key – Transfers the standby and active COM frequencies. Press and hold this key for two seconds to tune the emergency frequency (121.500 MHz) automatically into the active frequency field. 8 COM VOL/SQ Knob – Controls COM audio volume level. Press to turn the COM automatic squelch on and off. Volume level is shown in the COM frequency field as a percentage. 9 ADF/DME Tuning Window – Displays ADF frequencies and modes, and DME tuning selection. Display by selecting the ADF/DME Softkey. 10 ENT Key – Validates or confirms an ADF frequency or ADF/DME mode and Auto-tune selection. 11 FMS Knob – Flight Management System Knob, used to enter ADF frequencies and select ADF/DME modes, enter transponder codes, and Auto-tune entries when ADF/DME Tuning Window or NRST Window is present. Press the FMS Knob to turn the selection cursor on and off. The large knob moves the cursor in the window. The small knob selects individual characters for the highlighted cursor location. 12 Transponder Data Box – Indicates the selected transponder code, operating mode, reply, and ident status for the applicable transponder. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 123 AUDIO PANEL AND CNS AUDIO PANEL CONTROLS 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 Figure 4-2 Audio Panel Controls NOTE: When a key is selected, a triangular annunciator above the key is illuminated. 124 1 COM1 MIC – Selects the #1 transmitter for transmitting. COM1 receive is simultaneously selected when this key is pressed allowing received audio from the #1 COM receiver to be heard. COM2 receive can be added by pressing the COM2 Key. 2 COM1 – When selected, audio from the #1 COM receiver can be heard. 3 COM2 MIC – Selects the #2 transmitter for transmitting. COM2 receive is simultaneously selected when this key is pressed allowing received audio from the #2 COM receiver to be heard. COM1 receive can be added by pressing the COM1 Key. 4 COM2 – When selected, audio from the #2 COM receiver can be heard. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS 5 COM3 MIC – Selects the #3 transmitter (HF), if installed, for transmitting. COM3 receive is simultaneously selected when this key is pressed allowing received audio from the #3 COM receiver to be heard. 6 COM3 – When selected, audio from the #3 COM receiver (HF), if installed, can be heard. 7 PA – Selects the passenger address system. The selected COM transmitter is deselected when the PA Key is pressed. 8 TEL – When selected, activates the SATCOM transceiver. 9 MUSIC – Toggles the Music 1 input on or off. Pressing and holding toggles music muting on or off. 10 SPKR – Selects and deselects the on-side cockpit speaker. COM and NAV receiver audio can be heard on the speaker. 11 MKR/MUTE – Selects marker beacon receiver audio. Mutes the currently received marker beacon receiver audio. Unmutes automatically when new marker beacon audio is received. 12 HI SENS – Press to increase marker beacon receiver sensitivity. Press again to return to low sensitivity. 13 DME – Turns optional DME 1 audio on or off. 14 NAV1 – When selected, audio from the #1 NAV receiver can be heard. 15 ADF – Pressing turns on or off the audio from the ADF receiver, if installed. 16 NAV2 – When selected, audio from the #2 NAV receiver can be heard. 17 AUX – Turns optional DME 2 audio on or off.. 18 MAN SQ – Enables manual squelch for the intercom. When the intercom is active, press the ICS Knob to illuminate SQ. Turn the ICS Knob to adjust squelch. 19 PLAY – Press once to play the last recorded COM audio. Press again to stop playing. Press twice within 0.5 second while audio is playing and the previous block of recorded audio is played. Each subsequent two presses within 0.5 second plays each previously recorded block. 20 INTR COM – Selects and deselects the pilot/copilot intercom on both Audio Panels. 21 CABIN – Initiates intercom communications with passengers in the cabin. 22 ICS Knob – Turn to adjust intercom volume or squelch. Press to switch between volume and squelch control as indicated by illumination of VOL or SQ. The MAN SQ Key must be selected to allow squelch adjustment. 23 MSTR Knob – The Master Volume Control adjusts volume for the blended NAV, COM, intercom audio, and alert warnings. 24 DISPLAY BACKUP Button – Manually selects Reversionary Mode. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 125 AUDIO PANEL AND CNS 4.2 COM OPERATION COM TRANSCEIVER SELECTION AND ACTIVATION NOTE: During PA Mode, the COM MIC Annunciator is extinguished and the COM active frequency color changes to white, indicating that neither COM transmitter is active. NOTE: When turning on the system for use, the system remembers the last frequencies used and the active COM transceiver state prior to shutdown. The COM Frequency Box is composed of four fields; the two active frequencies are on the left side and the two standby frequencies are on the right. The COM transceiver is selected for transmitting by pressing the COM MIC Keys on the Audio Panel. An active COM frequency displayed in green indicates that the COM transceiver is selected on the Audio Panel (COM1 MIC or COM2 MIC Key). When the PA Key is selected on the Audio Panel, both active COM frequencies appear in white indicating that no COM radio is selected for transmitting. Frequencies in the standby fields are displayed in white. Active Fields Standby Fields Top Section of the Audio Panel Tuning Box COM2 Radio is Selected on the Audio Panel Figure 4-3 Selecting a COM Radio for Transmit COM3 is reserved for the optional HF radio. The active HF frequency is not shown on the system. The active COM frequency displayed in green on the MFD is the same as on PFD1. 126 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS TRANSMIT/RECEIVE INDICATIONS During COM transmission, a white TX appears by the active COM frequency replacing the Frequency Transfer Arrow. On the Audio Panel, when the active COM is transmitting, the active transceiver COM MIC Key Annunciator flashes approximately once per second. During COM signal reception, a white RX appears by the active COM frequency replacing the Frequency Transfer Arrow. Transmit and Receive Indicators Annunciator Flashes During Transmission Figure 4-4 COM Radio Transmit and Receive Indications When the same COM radio is selected on both Audio Panels, the pilot has transmit priority on COM1, the copilot has transmit priority on COM2. COM TRANSCEIVER MANUAL TUNING The COM frequency controls and frequency boxes are on the right side of each PFD and the MFD. The MFD frequency controls and displays are linked to the pilot side PFD (PFD1) only. Manually tuning a COM frequency: 1) Turn the COM Knob to tune the desired frequency in the COM Tuning Box (large knob for MHz; small knob for kHz). 2) Press the Frequency Transfer Key to transfer the frequency to the active field. 3) Adjust the volume level with the COM VOL/SQ Knob. 4) Press the COM VOL/SQ Knob to turn automatic squelch on and off. Turn the VOL/SQ Knob to adjust volume. Press the Knob to Turn Automatic Squelch On or Off Press the Frequency Transfer Key to Transfer COM Frequencies Between Active and Standby Frequency Boxes Turn the COM Knob to Tune the Frequency in the Tuning Box Figure 4-5 COM Frequency Tuning 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 127 AUDIO PANEL AND CNS SELECTING THE RADIO TO BE TUNED Press the small COM Knob to transfer the frequency tuning box and Frequency Transfer Arrow between the upper and lower radio frequency fields. Press the COM Knob to Switch the Tuning Box From One COM Radio to the Other Figure 4-6 Switching COM Tuning Boxes QUICK-TUNING AND ACTIVATING 121.500 MHZ Pressing and holding the COM Frequency Transfer Key for two seconds automatically loads the emergency COM frequency (121.500 MHz) in the active field of the COM radio selected for tuning (the one with the transfer arrow). In the example shown, pressing the Audio Panel COM2 MIC Key activates the transceiver. Press for Two Seconds to Load 121.500 MHz Figure 4-7 Quickly Tuning 121.500 MHz 128 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS AUTO-TUNING THE COM FREQUENCY COM frequencies can be automatically tuned from the following: • Nearest Airports Window (PFD) • NRST – Nearest Frequencies Page (ARTCC, FSS, WX) • WPT – Airport Information Page • NRST – Nearest Airspaces Page • NRST – Nearest Airports Page AUTO-TUNING FROM THE PFD COM frequencies for the nearest airports can be automatically tuned from the Nearest Airports Window on the PFD. When the desired frequency is entered, it becomes a standby frequency. Pressing the Frequency Transfer Key places this frequency into the COM Active Frequency Field. Auto-tuning a COM frequency for a nearby airport from the PFD: 1) Select the NRST Softkey on the PFD to open the Nearest Airports Window. A list of 25 nearest airport identifiers and COM frequencies is displayed. 2) Turn the FMS Knob to scroll through the list and highlight the desired COM frequency. 3) Press the ENT Key to load the COM frequency into the COM Standby Tuning Box. 4) Press the Frequency Transfer Key to transfer the frequency to the COM Active Frequency Field. Figure 4-8 Nearest Airports Window (PFD) 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide Select the NRST Softkey to Open the Nearest Airports Window 129 AUDIO PANEL AND CNS AUTO-TUNING FROM THE MFD Frequencies can be automatically loaded into the COM Frequency Box from pages in the NRST or WPT page group by highlighting the frequency and pressing the ENT Key (Figures 4-9, 4-10, and 4-11). Auto-tuning a COM frequency from the WPT and NRST Pages: 1) From any page that the COM frequency can be auto-tuned, activate the cursor by pressing the FMS Knob or selecting the appropriate softkey. 2) Turn the FMS Knob to place the cursor on the desired COM frequency. 3) Press the ENT Key to load the COM frequency into the standby field of the selected COM radio. 4) Press the Frequency Transfer Key to transfer the frequency to the COM Active Frequency Field. Press the ENT Key to Load a Highlighted Frequency into the COM Standby Frequency Box Turn the FMS Knob to Scroll Through a List of Frequencies Figure 4-9 Frequency Auto-Tuning from the MFD Or: 1) On the Nearest Airports, Frequencies, or Airspaces page, press the MENU Key to display the page menu (Figure 4-10). 2) Turn the large FMS Knob to scroll through the menu options. 3) Press the ENT Key to place the cursor on the desired selection. 4) Scroll through the frequency selections with the FMS Knob. 5) Press the ENT Key to load the COM frequency into the standby field of the selected COM radio. 6) Press the Frequency Transfer Key to transfer the frequency to the COM Active Frequency Field. Nearest Airports Menu Nearest Frequencies Menu Nearest Airspaces Menu Figure 4-10 Nearest Pages Menus 130 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS On the WPT - Airport Information Page, the cursor can be placed on the frequency field by pressing the FMS Knob and scrolling through the list. The frequency is transferred to the COM Standby Field with the ENT Key. Press Frequency Transfer Key to Load Frequency into COM Active Tuning Box Selected Airport Identifier and Information Runway Information Press ENT Key to load frequency into COM Standby Field. Cursor then advances to the next frequency. Figure 4-11 WPT – Airport Information Page 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide Press INFO Softkey for AIRPORT, RUNWAYS, and FREQUENCIES Windows 131 AUDIO PANEL AND CNS COM frequencies can also be auto-tuned from the NRST – Nearest Airspaces, NRST – Nearest Frequencies, and NRST – Nearest Airports Pages on the MFD in a similar manner using the appropriate softkeys or MENU Key, the FMS Knob, and the ENT Key. Figure 4-12 NRST – Nearest Airspaces, NRST – Nearest Airports, and NRST – Nearest Frequencies Pages 132 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS FREQUENCY SPACING The COM radios can tune either 25-kHz spacing (118.000 to 136.975 MHz) or 8.33-kHz spacing (118.000 to 136.990 MHz) for 760-channel or 3040-channel configuration. When 8.33-kHz channel spacing is selected, all of the 25-kHz channel spacing frequencies are also available in the complete 3040-channel list. Variable rate tuning is provided with 8.33-kHz spacing to achieve faster selection of the decimal digits. COM channel spacing is set on the System Setup Page of the AUX Page Group. 8.33-kHz Channel Spacing 25-kHz Channel Spacing Figure 4-13 COM Channel Spacing Changing COM frequency channel spacing: 1) Select the AUX – System Setup Page. 2) Press the FMS Knob to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the Channel Spacing Field in the COM Configuration Box. 4) Turn the small FMS Knob to select the desired channel spacing. 5) Press the ENT Key to complete the channel spacing selection. While the COM CONFIG Box is selected, the softkeys are blank. Select 8.33-kHz or 25.0-kHz COM Frequency Channel Spacing Figure 4-14 AUX – System Setup Page 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 133 AUDIO PANEL AND CNS AUTOMATIC SQUELCH Automatic Squelch quiets unwanted static noise when no audio signal is received, while still providing good sensitivity to weak COM signals. To disable Automatic Squelch, press the VOL/SQ Knob. When Automatic Squelch is disabled, COM audio reception is always on. Continuous static noise is heard over the headsets and speaker, if selected. Pressing the VOL/SQ Knob again enables Automatic Squelch. When Automatic Squelch is disabled, a white SQ appears next to the COM frequency. Squelch Indication Press the COM VOL/ SQ Knob to turn off Automatic Squelch. Press again to restore Automatic Squelch. Figure 4-15 Overriding Automatic Squelch VOLUME COM radio volume level can be adjusted from 0 to 100% using the VOL/SQ Knob. Turning the knob clockwise increases volume, turning the knob counterclockwise decreases volume. When adjusting volume, the level is displayed in place of the standby frequencies. Volume level indication remains for two seconds after the change. COM Volume Level Remains for Two Seconds Figure 4-16 COM Volume Level 134 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS 4.3 CONTROLLER PILOT DATA LINK COMMUNICATIONS (CPDLC) NOTE: The CPDLC system requires pilot certification and training. The GDR 66 VHF Data Link Transceiver (used for data communication only) provides the link from the G1000 Integrated Avionics System to the Controller Pilot Data Link Communications system (CPDLC). The CPDLC system provides data link communication between the aircraft and an Air Traffic Control facility. Communication is normally in the form of text message elements that resemble phraseology used in voice communications with ATC. The CPDLC system is intended for use in Europe with the Link 2000+ DLS (Data Link System) and will communicate with the ATN (Aeronautical Telecommunications Network) only. Eurocontrol is responsible for the technical coordination of the integration of the airborne and ground based components of the Link 2000+ DLS. Eurocontrol has termed this project the Link 2000+ Programme. The Link 2000+ DLS is designed to meet the requirements of the European Commission Regulation No. 29/2009, which is commonly referred to as the Data Link System Implementing Rule (DLSIR) or the European mandate for CPDLC. CPDLC SESSION OVERVIEW The Link 2000+ DLS will manage a CPDLC session with an ATC end system. Once a successful logon has been completed the Link 2000+ DLS will go into a CPDLC waiting state. In this state the Link 2000+ DLS is waiting for a CPDLC session to be initiated by the ATC end system. When an ATC end system sends a CPDLC session start command the flight crew will have the ability send CPDLC downlink messages. CPDLC downlink messages are messages initiated by the flight crew to ATC. CPDLC uplink messages are messages initiated by ATC to the flight crew. The ground system manages handoffs between ATC end systems. When the aircraft is nearing the coverage boundary of the CDA (Current Data Authority) or current facility, the Link 2000+ DLS will be assigned a NDA (Next Data Authority) or next facility. The NDA is the ATC end system that is waiting to take control of the aircraft. Upon crossing the boundary between the two ATC end systems, a transfer instruction will be sent to the Link 2000+ DLS making the NDA the new CDA. In the event that the CPDLC session is lost and the logon is still active, the Link 2000+ will accept future CPDLC start commands from ATC. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 135 AUDIO PANEL AND CNS CPDLC SYSTEM STATUS The Link 2000+ DLS will reflect the connection status at all times in the Status Window on the CPDLC Messages Page. The following is a list of possible system states: • Router Not Initialized – The Link 2000+ router has not been initialized. This is typical upon power up. This state should clear after initialization. Persistence of this state would indicate a failure. • Link Not Available/Waiting for Link – The Link 2000+ DLS has initialized the router but does not have an air-ground connection. • Establishing Link – The Link 2000+ DLS has detected a viable ground station and is attempting to establish an air-ground connection. • Link Available – The Link 2000+ DLS has established a connection capable of supporting ATN (Aeronautical Telecommunications Network) traffic. This state indicates that a network logon can be attempted to establish CPDLC communications. • Connecting – The Link 2000+ DLS has initiated a network logon with an ATC facility. • Waiting for CPDLC – The Link 2000+ DLS has successfully completed the network logon procedure. During this state the Link 2000+ DLS is waiting for an ATC facility to initiate a CPDLC session. This state will exist during initial connection or if a CPDLC session has been closed and the network logon is still valid. • Connected – The Link 2000+ DLS has successfully established a CPDLC session with a ground facility. CPDLC messages can be exchanged in this state. • Logon Failed – The Link 2000+ DLS was unable to establish a network logon. • CPDLC Disconnected – The Link 2000+ DLS has disconnected from a CPDLC connection. If the network logon is still valid, the Link 2000+ DLS will accept another CPDLC session from an ATC facility. Connection Status Current ATC Facility Next ATC Facility Message Status Icon Message Status Text ATC Facility Figure 4-17 CPDLC Messages 136 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS CPDLC MESSAGE STATUS ICONS The CPDLC Messages Page contains a combination of status icons and text to indicate the current status of each message. Icon Text Description Sent Message sent to ATC. Standby ‘Standby’ message response sent to ATC. The exclamation point notifies the flight crew that an action is needed to close the message. Send Failed / Expired Message failed to send or the message timed out. Closed Message sent to ATC and message thread closed. Table 4-1 Downlink CPDLC Status Icons Icon Text Description Standby Unopened ‘Standby’ message response sent by ATC. (message not opened) Standby (message opened) Opened ‘Standby’ message response sent by ATC. Need Response Unopened message that requires a response to ATC. (message not opened) Need Response (message opened) Opened message that requires a response to ATC. Expired Unopened expired message sent by ATC. (message not opened) Expired (message opened) Opened expired message sent by ATC. Closed Unopened message that closed the message thread. (message not opened) Closed (message opened) Opened message that closed the message thread. Table 4-2 Uplink CPDLC Status Icons 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 137 AUDIO PANEL AND CNS CONNECTING TO THE CPDLC SYSTEM A flight plan must be filed prior to logging on to the CPDLC system. The information entered in the CPDLC Log-On display must match the filed flight plan. After entering flight plan information in the required fields and successfully logging on to the system, messages may be sent and received. The following parameters are used to log on to the system: • Facility • Flight ID or Aircraft Registration as filed (populated from the active flight plan) • Destination Airport (populated from the active flight plan if available) • Filed Departure Airport • File Departure Time (Optional) Performing the system log-on: 1) From the MFD, select the CPDLC Softkey. 2) Select the LOGON Softkey. LOGON Softkey Figure 4-18 CPDLC Log-On Softkey 3) Turn the large FMS Knob to place the selection cursor over the Facility field. 138 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS Facility Field Flight ID Field Destination Airport Field Filed Departure Airport Field Filed Departure Time Field Send Button Figure 4-19 CPDLC Log-On Display 4) Turn the small FMS Knob to select the desired ATC facility to which the CPDLC connection will be established. 5) Press the ENT Key to complete the entry. 6) Turn the large FMS Knob to place the selection cursor over the Flight ID field. 7) The Flight ID Field is populated with the Flight ID or Aircraft Registration as filed. Changing this field will also change the Mode S Flight ID output. To change to Flight ID field, turn the small FMS Knob to enter the Flight ID or aircraft registration number. 8) Press the ENT Key to complete the entry. 9) Turn the large FMS Knob to place the selection cursor over the Destination Airport field. 10) The Destination Airport field is populated with the destination airport corresponding to the active flight plan if available. If the flight plan was filed using a different airport identifier, enter the identifier of the destination airport used in the filed flight plan and press the ENT Key. 11) The Filed Departure Airport field is populated with the airport identifier corresponding to the current aircraft location. If the flight plan was filed using a different airport identifier, turn the large FMS Knob to place the selection cursor over the Filed Departure Airport field, enter the departure airport, and press the ENT Key. 12) (Optional) Turn the large FMS Knob to place the selection cursor over the Filed Departure Time field. 13) (Optional) Enter the departure time used in the filed flight plan and press the ENT Key. 14) Turn the large FMS Knob to place the selection cursor over SEND and press the ENT Key. The Status immediately indicates ‘Connecting’. After successful log-on, the Status indicates ‘Waiting For CPDLC’. Once a CPDLC session is initiated by ATC, the Status indicates ‘Connected’ and the Current Facility field is populated with the name of the facility. If a transfer to another facility is needed, the Next Facility field is populated. Pressing the LOGOFF Softkey terminates the log-on process. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 139 AUDIO PANEL AND CNS CREATING A MESSAGE Once a CPDLC session has been successfully initiated, a message can be created by choosing from a predetermined list of requests, entering the required information, and sending the request. To create messages: 1) From the MFD, select the CPDLC Softkey. 2) Select the NEW Softkey. The CPDLC Thread Window appears. NEW Softkey Figure 4-20 CPDLC New Softkey 3) With the Response/Request field highlighted, turn the small FMS Knob to select the desired request from the list and press the ENT Key. For discussion purposes, ‘Request [level]’ is selected. Figure 4-21 CPDLC Request 140 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS 4) Highlight the Level field and enter the desired altitude. To toggle between multiple units of measure (FT or FL), highlight the first numeric position and turn the small FMS Knob counterclockwise. Figure 4-22 CPDLC Request Parameters 5) Press the ENT Key to complete the entry. 6) (Optional) Highlight the Reason field and enter the desired reason from the list. 7) Press the ENT Key to complete the entry. 8) Highlight the SEND Button and press the ENT Key. RESPONDING TO AN ATC MESSAGE Responding to an ATC message consists of choosing from a pre-determined list of responses or acknowledgements, then sending the response or acknowledgement. When a CPDLC message is received, an ATC Alert message will appear above the airspeed tape on the PFD. The Alert message will flash five times and then remain steady. The ATC Alert message will persist as long as there are unopened messages, or until a response has been provided for any messages requiring a response. CPDLC Alert Figure 4-23 CPDLC PFD Alert 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 141 AUDIO PANEL AND CNS To respond to a message: 1) From the MFD, select the CPDLC Softkey. 2) Turn the large FMS Knob to place the selection cursor over the desired message and press the ENT Key. 3) Turn the small FMS Knob to select the desired Response/Request from the list and press the ENT Key. 4) Highlight the SEND Button and press the ENT Key. VIEWING AN ATC MESSAGE Some ATC messages do not require a response, however they do need to be viewed. To view an ATC message: 1) From the MFD, select the CPDLC Softkey. 2) Turn the large FMS Knob to place the selection cursor over the desired message to view and press the ENT Key. Figure 4-24 CPDLC Response VIEWING CPDLC MESSAGE DIALOGS The status of a string of messages, or dialog, may be checked and past message dialogs from the current flight may be viewed. To view message dialogs: 1) From the MFD, select the CPDLC Softkey. 2) Turn the large FMS Knob to place the selection cursor over the desired message to view and press the ENT Key. 3) Press the ENT Key to view the CPDLC Thread. 142 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS DELETING MESSAGE DIALOGS The system will automatically delete the list of messages when the power is cycled, or when the system detects a transition from an airborne to a gound state. Individual message dialogs may also be deleted manually. Message dialogs must be considered closed in order to be deleted. DELETE Softkey Delete All (DEL ALL) Softkey Figure 4-25 Delete Message Dialogs To delete a single message dialog: 1) From the MFD, select the CPDLC Softkey. 2) Turn the large FMS Knob to place the selection cursor over the desired message to delete. 3) Select the DELETE Softkey. A confirmation window appears. 4) Highlight ‘OK’ and press the ENT Key. To delete all closed message dialogs: 1) From the MFD, select the CPDLC Softkey. 2) Select the DEL ALL Softkey. A confirmation window appears. Figure 4-26 Delete All Closed Messages Confirmation Window 3) Highlight ‘OK’ and press the ENT Key. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 143 AUDIO PANEL AND CNS DISCONNECTING FROM THE CPDLC SYSTEM After successfully initiating a CPDLC session, the LOGOFF Softkey becomes available. To Log-off the CPDLC System: 1) From the MFD, select the CPDLC Softkey. 2) Select the LOGOFF Softkey. DISABLING DATA MODE The Link 2000+ will only operate when the GDR 66 is in data mode. There are times when it may be desirable to disable the VDL (VHF Data Link) connection, such as during testing. To disable data mode on the GDR 66: 1) From the MFD, select the CPDLC Softkey. 2) Press the Menu Key to display the page menu. 3) Turn the small FMS Knob to highlight ‘Disable Data Mode’ and press the ENT Key. CPDLC SYSTEM FAILURE A CAS message and a red “X” over the Status Window on the CPDLC Messages Page indicate that the Link 2000+ DLS is unavailable. The failure or loss of connectivity can result from a power loss, a data path loss, or improper configuration. Refer to the system messages in the Appendices for additional information describing the source of the failure. Figure 4-27 CPDLC Failure 144 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS 4.4 NAV OPERATION NAV RADIO SELECTION AND ACTIVATION The NAV Frequency Box is composed of four fields; two standby fields and two active fields. The active frequencies are on the right side and the standby frequencies are on the left. A NAV radio is selected for navigation by selecting the CDI Softkey located on the PFD. The active NAV frequency selected for navigation is displayed in green. Selecting the CDI Softkey once selects NAV1 as the navigation radio. Selecting the CDI Softkey a second time selects NAV2 as the navigation radio. Selecting the CDI Softkey a third time activates GPS mode. Selecting the CDI Softkey again cycles back to NAV1. While cycling through the CDI Softkey selections, the NAV Tuning Box and the Frequency Transfer Arrow are placed in the active NAV Frequency Field and the active NAV frequency color changes to green. The three navigation modes that can be cycled through are: • VOR1 (or LOC1) – If NAV1 is selected, a green single line arrow (not shown) labeled either VOR1 or LOC1 is displayed on the HSI and the active NAV1 frequency is displayed in green. • VOR2 (or LOC2) – If NAV2 is selected, a green double line arrow (shown) labeled either VOR2 or LOC2 is displayed on the HSI and the active NAV2 frequency is displayed in green. • GPS – If GPS Mode is selected, a magenta single line arrow (not shown) appears on the HSI and neither NAV radio is selected. Both active NAV frequencies are then displayed in white. Standby Fields Active Fields Tuning Box The NAV Radio is Selected by Selecting the CDI Softkey Figure 4-28 Selecting a NAV Radio for Navigation The active NAV frequency displayed in green on the MFD is the same as on PFD1. See the Flight Instruments Section for selecting the DME and Bearing Information windows and using VOR as the source for the bearing pointer. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 145 AUDIO PANEL AND CNS NAV radios are selected for listening by pressing the corresponding keys on the Audio Panel. Pressing the NAV1, NAV2, ADF, DME, or AUX Key selects and deselects the navigation radio source. The DME Key selects and deselects optional DME 1 audio. The AUX Key selects and deselects optional DME 2 audio. Selected audio can be heard over the headset and the speakers (if selected). All radios can be selected individually or simultaneously. Figure 4-29 Selecting a NAV Radio Receiver NAV RECEIVER MANUAL TUNING The NAV frequency controls and frequency boxes are on the left side of the PFD and MFD. The MFD frequency controls and displays are linked to the pilot side PFD (PFD1) only. Manually tuning a NAV frequency: 1) Turn the NAV Knob to tune the desired frequency in the NAV Tuning Box. 2) Press the Frequency Transfer Key to transfer the frequency to the NAV Active Frequency Field. 3) Adjust the volume level with the NAV VOL/ID Knob. 4) Press the NAV VOL/ID Knob to turn the Morse code identifier audio on and off. Turn VOL/ID Knob to adjust volume. Press Knob to Turn Morse Code On or Off. Press the Frequency Transfer Key to Transfer NAV Frequencies Between Active and Standby Frequency Fields Turn the NAV Knob to Tune the Frequency in the Tuning Box Figure 4-30 NAV Frequency Tuning 146 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS SELECTING THE RADIO TO BE TUNED Press the small NAV Knob to transfer the frequency tuning box and Frequency Transfer Arrow between the upper and lower radio frequency fields. Press the NAV Knob to Switch the Tuning Box From One NAV Radio to the Other Figure 4-31 Switching NAV Tuning Boxes VOR/LOC ID When the Morse code Identifier audio is on for a NAV radio, a white ID appears to the left of the active NAV frequency. In the example shown, in order to listen to either station identifier, press the NAV1 or NAV2 Key on the Audio Panel. Pressing the VOL/ID Knob turns off the Morse code audio only in the radio with the NAV Tuning Box. To turn off both NAV IDs, transfer the NAV Tuning Box between NAV1 and NAV2 by pressing the small NAV Knob and pressing the VOL/ID Knob again to turn the Morse code off in the other radio. The Morse Code Identifiers for the GHM and BNA VORs are On Station Identifier Figure 4-32 NAV Radio ID Indication VOLUME NAV Radio volume level can be adjusted from 0 to 100% using the VOL/ID Knob. Turning the knob clockwise increases volume, counterclockwise decreases volume. When adjusting, the level is displayed in place of the standby frequencies. Volume level indication remains for two seconds after the change. NAV Volume Level Remains for Two Seconds Figure 4-33 NAV Volume Levels 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 147 AUDIO PANEL AND CNS AUTO-TUNING A NAV FREQUENCY FROM THE MFD NAV frequencies can be selected and loaded from the following MFD pages: • WPT – Airport Information • NRST – Nearest VOR • WPT – VOR Information • NRST – Nearest Frequencies (FSS, WX) • NRST – Nearest Airports • NRST – Nearest Airspaces The MFD provides auto-tuning of NAV frequencies from waypoint and nearest pages. During enroute navigation, the NAV frequency is entered automatically into the NAV standby frequency field. During approach activation the NAV frequency is entered automatically into the NAV active frequency field. Frequencies can be automatically loaded into the NAV Frequency Box from pages in the NRST or WPT page group by highlighting the frequency and pressing the ENT Key. Auto-tuning a NAV frequency from the WPT and NRST Pages: 1) From any page that the NAV frequency can be auto-tuned, activate the cursor by pressing the FMS Knob or selecting the appropriate softkey. 2) Turn the FMS Knob to place the cursor on the desired NAV identifier or NAV frequency. 3) On the Nearest VOR, Nearest Airspaces, and Nearest Airports pages, select the FREQ Softkey to place the cursor on the NAV frequency. 4) Press the ENT Key to load the NAV frequency into the standby field of the selected NAV radio. 5) Press the Frequency Transfer Key to transfer the frequency to the NAV Active Frequency Field. Turn the FMS Knob to Scroll Through a List of Frequencies Press the ENT Key to Load a Highlighted Frequency into the NAV Standby Frequency Box Figure 4-34 NAV Frequency Auto-Tuning from the MFD Or: 1) When on the NRST pages, press the MENU Key to display the page menu. 2) Turn the large FMS Knob to scroll through the menu options. 3) Press the ENT Key to place the cursor in the desired window. 4) Scroll through the frequency selections with the FMS Knob. 5) Press the ENT Key to load the NAV frequency into the standby field of the selected NAV radio. 6) Press the Frequency Transfer Key to transfer the frequency to the NAV Active Frequency Field. 148 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS Nearest Airports Menu Nearest VOR Menu Nearest Frequencies Menu Nearest Airspaces Menu Figure 4-35 Nearest Pages Menus In the example shown, the VOR list is selected with the VOR Softkey or from the page menu. The FMS Knob or ENT Key is used to scroll through the list. The cursor is placed on the frequency with the FREQ Softkey and loaded into the NAV Tuning Box with the ENT Key. Press the ENT Key to Load the Frequency into the NAV Standby Field. Select the VOR Softkey to Place the Cursor on the VOR Identifier Select the FREQ Softkey to Place the Cursor on the VOR Frequency Figure 4-36 Loading the NAV Frequency from the NRST – Nearest VOR Page 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 149 AUDIO PANEL AND CNS While enroute, NAV frequencies can also be auto-tuned from the NRST – Nearest Airports, WPT – Airport Information, WPT – VOR Information, and NRST – Nearest Frequencies Pages on the MFD in a similar manner using the appropriate softkeys or MENU Key, the FMS Knob, and the ENT Key. Figure 4-37 NRST – Nearest Frequencies, WPT – VOR Information, WPT – Airport Information, and NRST – Nearest Airports Pages 150 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS AUTO-TUNING NAV FREQUENCIES ON APPROACH ACTIVATION NOTE: The primary NAV frequency is auto-tuned upon loading a VOR or ILS/Localizer approach. NOTE: When an ILS/LOC approach has been activated in GPS Mode, the system switches to NAV Mode as the final approach course is intercepted (within 15 nm of the FAF). See the Flight Management Section for details. NAV frequencies are automatically loaded into the NAV Frequency Box on approach activation. When loading or activating a VOR or ILS/LOC approach, the approach frequency is automatically transferred to a NAV frequency field as follows: • If the current CDI navigation source is GPS, the approach frequency is transferred to the NAV1 or NAV2 active frequency fields. The frequency that was previously in the NAV1 or NAV2 active frequency fields are transferred to standby. • If the current CDI navigation source is GPS, and if the approach frequency is already loaded into the NAV1 or NAV2 standby frequency field, the standby frequency is transferred to active. • If the current CDI navigation source is NAV1 or NAV2, the approach frequency is transferred to the standby frequency fields of the selected CDI NAV radio. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 151 AUDIO PANEL AND CNS MARKER BEACON RECEIVER NOTE: The marker beacon indicators operate independently of marker beacon audio and cannot be turned off. The marker beacon receiver is used as part of the ILS. The marker beacon receiver is always on and detects any marker beacon signals within the reception range of the aircraft. The receiver detects the three marker tones – outer, middle, and inner – and provides the marker beacon annunciations located to the left of the Altimeter on the PFD. Outer Marker Indication Middle Marker Indication Inner Marker Indication Figure 4-38 Marker Beacon Annunciations on the PFD Figure 4-39 Marker Beacon Keys The Audio Panels provide three different states of marker beacon operation; On, Muted, and Deselected. Pressing the MKR/MUTE Key selects and deselects marker beacon audio. The key annunciator indicates when marker beacon audio is selected. During marker beacon audio reception, pressing the MKR/MUTE Key mutes the audio but does not affect the marker annunciations (Figure 4-38). The marker tone is silenced, then waits for the next marker tone. The MKR/MUTE Key Annunciator is illuminated, indicating audio muting. The audio returns when the next marker beacon signal is received. If the MKR/MUTE Key is pressed during signal reception (O, M, I indication) while marker beacon audio is muted, the audio is deselected and the MKR/MUTE Key Annunciator is extinguished. Pressing the HI SENS Key switches between high and low marker beacon receiver sensitivity. The HI SENS function (annunciator illuminated) is used to provide an earlier indication when nearing a marker during an approach. The LO SENS function (annunciator extinguished) results in a narrower marker dwell while over a station. 152 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS ADF/DME TUNING NOTE: When another auxiliary window is turned on, the ADF/DME Tuning Window is replaced on the PFD. See the Flight Instruments Section for displaying the DME and bearing information windows (ADF) and using the ADF as the source for the bearing pointer. The system tunes the optional ADF receiver and DME transceiver. The ADF is tuned by entering the frequency in the ADF standby frequency field of the ADF/DME Tuning Window. (The softkey may be labeled ADF/DME or DME, depending on installed equipment.) The UHF DME frequency is tuned by pairing with a VHF NAV frequency. DME frequency pairing is automatic and only the VHF NAV frequency is shown. The following ADF/DME information is displayed in the ADF/DME Tuning Window: • Active and standby ADF frequencies • ADF receiver mode • DME tuning mode (DME transceiver pairing) When the ADF/DME Tuning Window is displayed, the selection cursor is placed over the standby ADF frequency field. Turning the large FMS Knob moves the selection cursor through the various fields (standby ADF frequency, ADF receiver mode, and DME tuning mode). Pressing the FMS Knob activates/deactivates the selection cursor in the ADF/DME Tuning Window. The ADF frequency is entered using the FMS Knob and the ENT Key. Active ADF Frequency Standby ADF Frequency ADF Mode DME Tuning Mode Figure 4-40 ADF/DME Tuning Window 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 153 AUDIO PANEL AND CNS ADF TUNING ADF frequencies in the 190.0-kHz to 1799.5-kHz range are entered in the standby ADF frequency field of the ADF/DME Tuning Window. The system does not tune the ADF emergency frequency, 2182.0‑kHz. Tuning an ADF frequency: 1) Select the ADF/DME Softkey to display the ADF/DME Tuning Window. 2) Turn the large FMS Knob to place the selection cursor over the standby ADF frequency field. 3) Turn the small FMS Knob to begin data entry and change each digit. 4) Turn the large FMS Knob to move the cursor to the next digit position. 5) Press the ENT Key to complete data entry for the standby frequency. Press the ENT Key to Complete ADF Frequency Entry Turn the Small FMS Knob to Enter Data in the Standby ADF Frequency Field Turn the Large FMS Knob to Move the Cursor to the Next Character Figure 4-41 Entering ADF Standby Frequencies Pressing the CLR Key before completing frequency entry cancels the frequency change and reverts back to the previously entered frequency. Pressing the CLR Key when the cursor is flashing, clears the frequency and replaces the standby field with ‘0000.0’. Transferring the active and standby ADF frequencies: 1) Turn the large FMS Knob to place the selection cursor over the standby ADF frequency field. 2) Press the ENT Key to complete the frequency transfer. Press the ENT Key to Transfer the ADF Frequencies Figure 4-42 Transferring ADF Frequencies 154 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS SELECTING ADF RECEIVER MODE The following modes can be selected: (In all modes NDB audio can be heard by selecting the ADF Key on the Audio Panel.) • ANT (Antenna) – The ADF bearing pointer parks on the HSI at 90 degrees. Best mode for listening to NDB audio. • ADF (Automatic Direction Finder) – The ADF pointer points to the relative bearing of the NDB station. • ADF/BFO (ADF/Beat Frequency Oscillator) – The ADF pointer points to the relative bearing of the NDB station and an audible tone confirms signal reception. This mode allows identification of the interrupted carrier beacon stations used in various parts of the world. • ANT/BFO (Antenna/Beat Frequency Oscillator) – The ADF bearing pointer parks on the HSI at 90 degrees while an audible tone is provided when a signal is received. This mode also allows identification of the interrupted carrier beacon stations and confirms signal reception. Selecting an ADF receiver mode: 1) Turn the large FMS Knob to place the selection cursor over the ADF mode field. 2) Turn the small FMS Knob to select the desired ADF receiver mode. Turn the Small FMS Knob to Select the Mode Figure 4-43 Selecting ADF Receiver Mode 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 155 AUDIO PANEL AND CNS DME TUNING NOTE: When turning on the system for use, the system remembers the last frequency used for DME tuning and the NAV1, NAV2, or HOLD state prior to shutdown. The DME transceiver is tuned by selecting NAV1, NAV2, or HOLD in the ADF/DME Tuning Window. DME Modes Figure 4-44 DME Tuning Window The following DME transceiver pairings can be selected: • NAV1 – Pairs the DME frequency from the selected NAV1 frequency. • NAV2 – Pairs the DME frequency from the selected NAV2 frequency. • HOLD – When in the HOLD position, the DME frequency remains paired with the last selected NAV frequency. Selecting DME transceiver pairing: 1) Select the ADF/DME Softkey to display the ADF/DME Tuning Window. 2) Turn the small FMS Knob to select the DME tuning mode. 3) Press the ENT Key to complete the selection. Pressing the CLR Key or FMS Knob while in the process of DME pairing cancels the data entry and reverts back to the previously selected DME tuning state. Pressing the FMS Knob activates/deactivates the cursor in the ADF/DME Tuning Window. 156 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS 4.5 MODE S TRANSPONDER The Mode S Transponders provide Mode A, Mode C, and Mode S interrogation and reply capabilities. Diversity incorporates antennas mounted on the top and bottom of the aircraft for dependable operation while maneuvering. Selective addressing or Mode Select (Mode S) capability includes the following features: • Level-2 reply data link capability (used to exchange information between aircraft and ATC facilities) • Surveillance identifier capability • Flight ID (Flight Identification) reporting – The Mode S Transponder reports aircraft identification as either the aircraft registration or a unique Flight ID. • Altitude reporting • Airborne status determination • Transponder capability reporting • Mode S Enhanced Surveillance (EHS) requirements • Mode S Elementary Surveillance (ELS) requirements • Acquisition squitter – Acquisition squitter, or short squitter, is the transponder 24-bit identification address. The transmission is sent periodically, regardless of the presence of interrogations. The purpose of acquisition squitter is to enable Mode S ground stations and aircraft equipped with a traffic avoidance system to recognize the presence of Mode S-equipped aircraft for selective interrogation. • Extended squitter (Optional) – If equipped with an extended squitter, the extended squitter is transmitted periodically and contains information such as altitude (barometric and GPS), GPS position, and aircraft identification. The purpose of extended squitter is to provide aircraft position and identification to ADS-B Ground-Based Transceivers (GBTs) and other aircraft. The Hazard Avoidance Section provides more details on traffic avoidance systems. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 157 AUDIO PANEL AND CNS GTX 33/33D TRANSPONDER CONTROLS Transponder function is displayed on three levels of softkeys on the PFD: Top-level, Mode Selection, and Code Selection. When the top-level XPDR Softkey is selected, the Mode Selection softkeys appear: XPDR1, XPDR2, STBY, ON, ALT, GND, VFR, CODE, IDENT, BACK. When the CODE Softkey is selected, the number softkeys appear: 0, 1, 2, 3, 4, 5, 6, 7, IDENT, BKSP, BACK. The digits 8 and 9 are not used for code entry. Selecting the numbered softkeys in sequence enters the transponder code. If an error is made, selecting the BKSP Softkey moves the code selection cursor to the previous digit. Selecting the BKSP Softkey again moves the cursor to the next previous digit. Selecting the BACK Softkey during code selection reverts to the Mode Selection Softkeys. Selecting the BACK Softkey during mode selection reverts to the top-level softkeys. The code can also be entered with the FMS Knob on either PFD. Code entry must be completed with either the softkeys or the FMS Knob, but not a combination of both. Selecting the IDENT Softkey while in Mode or Code Selection initiates the ident function and reverts to the top-level softkeys. After 45 seconds of transponder control inactivity, the system reverts back to the top-level softkeys. XPDR1 XPDR2 STBY ON ALT GND VFR XPDR IDENT CODE IDENT BACK MSG Selecting the BACK Softkey returns to the top-level softkeys. 0 1 2 3 4 5 6 7 IDENT BKSP BACK MSG Selecting the BACK Softkey returns to the mode selection softkeys. Figure 4-45 Transponder Softkeys (PFD) Selecting and activating Transponder 1 or Transponder 2: 1) Select the XPDR Softkey to display the Transponder Mode Selection Softkeys. 2) Select the XPDR1 or XPDR2 Softkey to select and activate the other transponder. When turning on the system for use, the system defaults to the transponder active prior to shutdown. When switching between Transponder 1 and Transponder 2, the code and mode remain the same. If a new code is entered in the active transponder, switching transponders does not bring back the previous code. 158 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS GTX 33/33D TRANSPONDER MODE SELECTION Mode selection can be automatic (Ground and Altitude Modes) or manual (Standby, On, and Altitude Modes). The STBY, ON, ALT, and GND Softkeys can be accessed by selecting the XPDR Softkey. Selecting a transponder mode: 1) Select the XPDR Softkey to display the Transponder Mode Selection Softkeys. 2) Select the desired softkey to activate the transponder mode. STANDBY MODE (MANUAL) NOTE: In Standby Mode, the IDENT function is inhibited. Standby Mode can be selected at any time by pressing the STBY Softkey. In Standby, the transponder is powered and new codes can be entered, but no replies or squitters are transmitted.. When Standby is selected, a white STBY indication and transponder code appear in the mode field of the Transponder Data Box. In all other modes, these fields appear in green. STBY Mode (White Code Number and Mode) Figure 4-46 Standby Mode ON MODE (MANUAL) ON Mode can be selected at any time by pressing the ON Softkey. ON Mode generates Mode A and Mode S replies as well as transmission of acquisition and extended squitters, including ADS-B out (if equipped). Mode C altitude reporting is inhibited. In ON Mode, a green ON indication and transponder code appear in the mode field of the Transponder Data Box. ON Mode (No Altitude Reporting) Figure 4-47 ON Mode 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 159 AUDIO PANEL AND CNS ALTITUDE MODE (AUTOMATIC OR MANUAL) Altitude Mode is automatically selected when the aircraft becomes airborne. Altitude Mode may also be selected manually by pressing the ALT Softkey. Altitude Mode generates Mode A, Mode C, and Mode S replies as well as transmissions of acquisition and extended squitters including ADS-B out (if equipped). If Altitude Mode is selected, a green ALT indication and transponder code appear in the mode field of the Transponder Data Box, and all transponder replies requesting altitude information are provided with pressure altitude information. ALT Mode (Mode C Altitude Reporting) Figure 4-48 Altitude Mode GROUND MODE Ground Mode is normally selected automatically when the aircraft is on the ground. The transponder powers up in the last mode it was in when shut down. Ground Mode can be overridden by selecting any one of the Mode Selection Softkeys. A green GND indication and transponder code appear in the mode field of the Transponder Data Box. Ground Mode generates Mode S replies to discrete interrogations as well as transmission of acquisition squitter and extended squitter, including ADS-B out (if equipped). Mode A, Mode C, and Mode S all-call replies are inhibited. When Standby Mode has been selected on the ground, the transponder can be returned to Ground Mode by selecting the GND Softkey. GND Mode Figure 4-49 Ground Mode REPLY STATUS When the transponder sends replies to interrogations, a white R indication appears momentarily in the reply status field of the Transponder Data Box. Reply to Interrogation Figure 4-50 Reply Indication 160 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS TCAS II TRANSPONDER CONTROLS (OPTIONAL) Transponder function is displayed on three levels of softkeys on the PFD: Top-level, Transponder/Traffic Selection, and Mode Selection or Code Entry. When the top-level XPDR/TFC Softkey is selected, the Function Select softkeys appear: XPDR1, XPDR2 (if TCAS XPDR2 option is loaded), MODE, TCAS, CODE, IDENT, BACK. When the MODE Softkey is selected, the Mode Selection softkeys appear: STBY, ON, ALT, TA ONLY, TA/ RA, BACK. When the CODE Softkey is selected, the number softkeys appear: 0, 1, 2, 3, 4, 5, 6, 7, IDENT, BKSP, BACK. The digits 8 and 9 are not used for code entry. Selecting the numbered softkeys in sequence enters the transponder code. If an error is made, selecting the BKSP Softkey moves the code selection cursor to the previous digit. Selecting the BKSP Softkey again moves the cursor to the next previous digit. Selecting the BACK Softkey returns to the previous level softkeys. The code can also be entered with the FMS Knob on either PFD. Code entry must be completed with either the softkeys or the FMS Knob, but not a combination of both. Selecting the IDENT Softkey while in Code Selection initiates the ident function and reverts to the top-level softkeys. After 45 seconds of transponder control inactivity, the system reverts back to the top-level softkeys. XPDR1 XPDR2 MODE TCAS XPDR/TFC IDENT CODE IDENT BACK MSG Selecting the BACK Softkey returns to the top-level softkeys. 0 1 2 3 4 5 6 IDENT 7 BKSP BACK MSG Selecting the BACK Softkey returns to the previous level softkeys. STBY ON ALT TA ONLY TA/RA BACK MSG Selecting the BACK Softkey returns to the previous level softkeys. Figure 4-51 Transponder Softkeys (with TCAS II option) 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 161 AUDIO PANEL AND CNS TCAS II TRANSPONDER MODE SELECTION (OPTIONAL) Mode selection can be automatic (Altitude Mode) or manual (Standby, On, and Altitude Modes). The STBY, ON, ALT, TA ONLY, and TA/RA Softkeys can be accessed by selecting the XPDR/TFC Softkey, then the MODE Softkey. Selecting a transponder mode: 1) Select the XPDR/TFC Softkey. 2) Select the MODE Softkey to display the Transponder Mode Selection Softkeys. 3) Select the desired softkey to activate the transponder mode (STBY, ON, or ALT). Selecting a TCAS II mode: 1) Select the XPDR/TFC Softkey. 2) Select the MODE Softkey to display the TCAS II Mode Selection Softkeys. 3) Select the desired softkey to activate the TCAS II mode (TA ONLY or TA/RA). STANDBY MODE (MANUAL) NOTE: In Standby Mode, the IDENT function is inhibited. TCAS II is switched to Standby Mode, because the transponder is not capable of supporting TCAS II operation in Standby Mode. Standby Mode can be selected at any time by selecting the STBY Softkey. In Standby, the transponder does not reply to interrogations, but new codes can be entered. When Standby is selected, a white STBY indication and transponder code appear in the mode field of the Transponder Data Box. In all other modes, these fields appear in green. STBY Mode (White Code Number and Mode) Figure 4-52 Standby Mode 162 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS ON MODE (MANUAL) NOTE: TCAS II is switched to Standby Mode, because the transponder is not capable of supporting TCAS II operation in On Mode. ON Mode can be selected at any time by selecting the ON Softkey. ON Mode generates Mode A replies, but Mode C altitude reporting is inhibited. Acquisition squitter and replies to discretely addressed Mode S interrogations are also permitted. In ON Mode, a green ON indication and transponder code appear in the mode field of the Transponder Data Box. ON Mode (No Altitude Reporting) Figure 4-53 ON Mode ALTITUDE MODE (AUTOMATIC OR MANUAL) NOTE: TCAS II is switched to Standby Mode when the altitude mode is manually selected using the ALT Softkey. Altitude Mode is automatically selected when the aircraft becomes airborne. Altitude Mode may also be selected manually by selecting the ALT Softkey. ALT Mode generates Mode A and Mode C replies. Acquisition squitter and replies to discretely addressed Mode S interrogations are also permitted. If Altitude Mode is selected, a green ALT indication and transponder code appear in the mode field of the Transponder Data Box, and all transponder replies requesting altitude information are provided with pressure altitude information. ALT C Altitude Reporting) Figure 4-54 Altitude Mode 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 163 AUDIO PANEL AND CNS ENTERING A TRANSPONDER CODE Entering a transponder code with softkeys: 1) Select the XPDR Softkey (or XPDR/TFC Softkey with optional TCAS II) to display the CODE Softkey. 2) Select the CODE Softkey to display the Transponder Code Selection Softkeys, for digit entry. 3) Select the digit softkeys to enter the code in the code field. When entering the code, the next softkey in sequence must be selected within 10 seconds, or the entry is cancelled and restored to the previous code. Selecting the BKSP Softkey moves the code selection cursor to the previous digit. Five seconds after the fourth digit has been entered, the transponder code becomes active. Entering a Code Figure 4-55 Entering a Code Entering a transponder code with the PFD FMS Knob: 1) Select the XPDR Softkey (or XPDR/TFC Softkey with optional TCAS II) to display the CODE Softkey. 2) Select the CODE Softkey. 3) Turn the small FMS Knob on the PFD to enter the first two code digits. 4) Turn the large FMS Knob to move the cursor to the next code field. 5) Enter the last two code digits with the small FMS Knob. 6) Press the ENT Key to complete code digit entry. Pressing the CLR Key or small FMS Knob before code entry is complete cancels code entry and restores the previous code. Waiting for 10 seconds after code entry is finished activates the code automatically. Turn the Small FMS Knob to Enter Two Code Digits at a Time Press the ENT Key to Complete Code Entry Turn the Large FMS Knob to Move the Cursor to the Next Code Field Figure 4-56 Entering a Code with the FMS Knob 164 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS VFR CODE The VFR code can be entered either manually or by selecting the XPDR Softkey, then the VFR Softkey. When the VFR Softkey is selected, the pre-programmed VFR code is automatically displayed in the code field of the Transponder Data Box. Selecting the VFR Softkey again restores the previous identification code. The pre-programmed VFR Code is set at the factory to 1200. If a VFR code change is required, contact a Garmin-authorized service center for configuration. VFR Code Figure 4-57 VFR Code IDENT FUNCTION NOTE: In Standby Mode, the IDENT Softkey is inoperative. Selecting the IDENT Softkey sends a distinct identity indication to Air Traffic Control (ATC). The indication distinguishes the identing transponder from all the others on the air traffic controller’s screen. The IDENT Softkey appears on all levels of transponder softkeys. When the IDENT Softkey is selected, a green IDNT indication is displayed in the mode field of the Transponder Data Box for a duration of 18 seconds. After the IDENT Softkey is selected while in Mode or Code Selection, the system reverts to the top-level softkeys. IDNT Indication Select the IDENT Softkey to Initiate the ID Function Figure 4-58 IDENT Softkey and Indication 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 165 AUDIO PANEL AND CNS FLIGHT ID REPORTING NOTE: If the Flight ID is required but the system is not configured for it, contact a Garmin-authorized service center for configuration. When the Flight ID must be entered before flight operation, the identifier is placed in the Timer/References Window on the PFD. The Flight ID can be up to eight characters. No space is needed when entering Flight ID. When a Flight ID contains a space, the system automatically removes it upon completion of Flight ID entry. The Flight ID is also displayed on the System - Status Page. Entering a Flight ID: 1) Select the TMR/REF Softkey to display the Timer/References Window. 2) Press the FMS Knob to activate the selection cursor, if not already activated. 3) Turn the large FMS Knob to scroll down to the Flight ID. 4) Turn the small FMS Knob to enter the desired Flight ID. 5) Press the ENT Key to complete Flight ID entry. The word “updating” appears until the new entry is completed. If an error is made during Flight ID entry, pressing the CLR Key returns to the original Flight ID entry. While entering a Flight ID, turning the FMS Knob counterclockwise moves the cursor back one space for each detent of rotation. If an incorrect Flight ID is discovered after the unit begins operation, reenter the correct Flight ID using the same procedure. Flight ID PFD Entry Figure 4-59 Timer/References Window, Entering Flight ID 166 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS 4.6 ADDITIONAL AUDIO PANEL FUNCTIONS POWER-UP The Audio Panels perform a self-test during power-up. During the self-test all Audio Panel annunciator lights illuminate for approximately two seconds. Once the self-test is completed, most of the settings are restored to those in use before the unit was last turned off. The exceptions are the speaker and intercom, which are always selected during power up. MONO/STEREO HEADSETS Stereo or mono headsets are recommended for use in the cockpit of the aircraft. Using a monaural headset in the jack panel of the cockpit shorts the right headset channel output to ground. While this does not damage the Audio Panel, a pilot listening on a monaural headset hears only the left channel in both ears. SPEAKER Each Audio Panel controls a separate cabin speaker. Pressing the SPKR Key selects and deselects the on-side speaker unless oxygen masks are in use. While using oxygen masks, the cross-side cabin speaker is always on, pilot audio is always heard on the speaker, and the SPKR Key can not be disabled (the speaker remains on) on the side in which the oxygen mask is in use. All of the radios can be heard over the cabin speakers. Speaker audio is muted when the PTT is pressed. The “Stall” aural warning is always heard on both speakers, since the SPWS automatically activate the pilot and copilot speakers (if they are not already turned on) in the event of Stall Warning activation.. Figure 4-60 Music and Speaker Keys 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 167 AUDIO PANEL AND CNS INTERCOM Pressing the INTR COM Key on either Audio Panel selects and deselects the intercom on both Audio Panels. The annunciator is lit when the intercom is active. The intercom connects the pilot and copilot together. Either the pilot or copilot may select or deselect the intercom. The CABIN Key initiates two way communication between the pilot or copilot and the passengers in the cabin. The annunciator is lit when the cabin intercom is active on either Audio Panel. When the flight crew wants to communicate with the passengers, the pilot or copilot presses the CABIN Key to signal that communication is desired. The cabin signal must be acknowledged to begin intercom conversation. When the passengers want to communicate with the pilot/copilot, they press the “COCKPIT CALL” switch at their seat in the cabin. The CABIN annunciator flashes on both Audio Panels to signal the pilot and copilot that cabin communication is desired. The cockpit call signal must be acknowledged by pressing the CABIN Key to begin intercom conversation. The MAN SQ Key allows either automatic or manual control of the intercom squelch setting. Pressing the MAN SQ Key enables manual squelch control, indicated by the MAN SQ annunciator. • When the MAN SQ Annunciator is extinguished (Automatic Squelch is on), the ICS Knob controls only the volume (pressing the ICS Knob has no effect on the VOL/SQ selection). • When the MAN SQ Annunciator is illuminated (Manual Squelch), the ICS Knob controls either volume or squelch (selected by pressing the ICS Knob and indicated by the VOL or SQ annunciation). Manual Squelch Annunciator; Off for Automatic Squelch, On for Manual Squelch Cabin Annunciator; On for Cabin Intercom, Flashes for Cabin to Flight Deck Hail Selects and Deselects Cabin Intercom Pilot/Copilot ICS Press to switch between VOL and SQ. Turn to adjust Squelch when SQ Annunciation is lit, Volume when VOL Annunciation is lit. Master Volume Control for Pilot Side or Copilot Side Volume Annunciation Squelch Annunciation Figure 4-61 Intercom Controls 168 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS PASSENGER ADDRESS (PA) SYSTEM A passenger address system is provided by pressing the PA Key to deliver messages to the headsets of the passengers (if installed). The message is heard by the other pilot on the headset only if the PA Key is enabled on both audio panels. PA messages are one way from the flight deck to the passengers. A Push-to-talk (PTT) must be pressed to deliver PA announcements to the passengers over their headphones. When PA is selected on the Audio Panel, the annunciator flashes about once per second while pressing the PTT, the COM MIC annunciator is no longer lit, and the active COM frequency for that Audio Panel changes to white, indicating that there is no COM selected. PA Key is Selected on the Audio Panel Figure 4-62 PA Key Selected for Cabin Announcements SIMULTANEOUS COM OPERATION NOTE: While a COM radio is transmitting during simultaneous COM operation, the signal received on the other COM radio is attenuated, which can result in temporary loss of audio reception from that radio. Both the pilot and the copilot can transmit and receive simultaneously over separate COM radios. The selected COM MIC Annunciator flashes when either pilot’s microphone PTT is pressed. If both pilots select the same COM radio, the pilot has priority on COM1 and the copilot has priority on COM2. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 169 AUDIO PANEL AND CNS CLEARANCE RECORDER AND PLAYER NOTE: Pressing the play key on the pilot’s Audio Panel plays recorded audio to the Pilot. Pressing the play key on the Copilot’s Audio Panel plays recorded audio to the Copilot. The Audio Panel contains a digital clearance recorder that continually records up to 2.5 minutes of the selected COM radio signal. Recorded COM audio is stored in separate memory blocks. Once 2.5 minutes of recording time have been reached, the recorder begins recording over the stored memory blocks, starting from the oldest block. The PLAY Key controls the play function. The PLAY annunciator remains lit to indicate when play is in progress. The PLAY annunciator turns off after playback is finished. Pressing the PLAY Key once plays the latest recorded memory block and then returns to normal operation. Pressing the PLAY Key again during play of a memory block stops play. If a COM input signal is detected during play of a recorded memory block, play is halted. Pressing the PLAY Key twice within one-half second while audio is playing plays the previous block of recorded audio. Each subsequent two presses of the PLAY Key within one-half second backtracks through the recorded memory blocks to reach and play any recorded block. Powering off the unit automatically clears all recorded blocks. PLAY Key Controls the Play Function Figure 4-63 Play Key 170 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS ENTERTAINMENT INPUTS NOTE: MUSIC 1 and MUSIC 2 inputs cannot be completely turned off. Audio level for MUSIC 1 and MUSIC 2 can be adjusted by a Garmin-authorized service center. The Audio Panel provides two stereo auxiliary entertainment inputs: MUSIC 1 and MUSIC 2. These inputs are compatible with popular portable entertainment devices such as MP3 and CD players. Two 3.5-mm stereo phone jacks are installed in convenient locations for audio connection. The headphone outputs of the entertainment devices are plugged into the MUSIC 1 or MUSIC 2 jacks. The availability of the Entertainment Inputs is as shown in the following table. Pilot Music In (Music 1) OFF* OFF ON ON Copilot Music In (Music 2) OFF ON** OFF ON Crew GDL 69A (XM Radio) Copilot Music In Pilot Music In Pilot Music In Passengers GDL 69A (XM Radio) Copilot Music In GDL 69A (XM Radio) Copilot Music In * OFF means no audio source is plugged into the respective Audio Jack Panel. **ON means an audio source (e.g. MP3 player) is plugged into the respective Audio Jack Panel. MUSIC 1 MUSIC 1 can be heard by the pilot and copilot when the MUSIC Key is selected. MUSIC 1 Muting MUSIC 1 muting occurs when aircraft radio, aural warning alerts, or marker beacon activity is heard. MUSIC 1 is always soft muted when an interruption occurs from an aircraft radio. Soft muting is the gradual return of MUSIC 1 to its original volume level. The time required for MUSIC 1 volume to return to normal is between one-half and four seconds. MUSIC 2 MUSIC 2 can be heard only by the passengers. announcements. MUSIC 2 is by default muted only during PA XM RADIO ENTERTAINMENT XM Radio audio from the Data Link Receiver may be heard by the pilot and passengers simultaneously (optional: requires subscription to XM Radio Service). Refer to the Additional Features Section for more details on the Data Link Receiver. Connecting a stereo input to either MUSIC 1 or MUSIC 2 jacks removes the XM Radio Audio from that input. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 171 AUDIO PANEL AND CNS 4.7 AUDIO PANELS PREFLIGHT PROCEDURE NOTE: If the pilot and/or copilot are using headsets that have a high/low switch or volume control knob, verify that the switch is in the high position and the volume control on the headsets are at maximum volume setting. On single‑pilot flights, verify that all other headsets are not connected to avoid excess noise in the audio system. NOTE: Adjusting the PILOT volume control affects ICS audio that is heard in the headset for the flight crew member that is performing the adjustment. Keep in mind that the intercom volumes on the Audio Panels are independent of one another, but the radio volumes are not. NOTE: When the MAN SQ Key is pressed, the ICS squelch can be set manually by the pilot and copilot. If manual squelch is set to minimum (SQ annunciated and the knobs turned counterclockwise), background noise is heard in the ICS system as well as during COM transmissions. After powering up the system, the following steps aid in maximizing the use of the Audio Panels as well as prevent pilot and copilot induced issues. These preflight procedures should be performed each time a pilot boards the aircraft to insure awareness of all audio levels in the Audio Panel and radios. Automatic/Manual Squelch Pilot/Copilot ICS Cabin ICS Master Volume Control ICS Volume and Squelch Control Volume Annunciation Squelch Annunciation Reversionary Mode for PFD1 and MFD Reversionary Mode for PFD2 and MFD Pilot Side Copilot Side Figure 4-64 Audio Panel Controls 172 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS Independent radio volume adjustments made using the MFD/PFD controls affect only the audio output for each radio selected for adjustment. Radio volume adjustment affects both crew positions equally for each radio that is adjusted. Turning the master volume control located on either Audio Panel affects only the audio heard in the corresponding crew position headset. Thus, radio volume adjustments may be overridden by each crew position independently using the master volume control on the Audio Panel for the respective crew position. The master volume control for each Audio Panel affects all other system audio output for the pilot or copilot headset. Setting the Audio Panel volume levels during preflight: 1) Verify the INTR COM Key is selected. 2) Verify manual squelch is set to minimum. 3) Turn the MSTR Knob (Master Volume Control) on both Audio Panels clockwise two full turns. This sets the headset audio level to max volume (least amount of attenuation). 4) Adjust radio volume levels (COM, NAV, etc.) to a suitable level. 5) Adjust the ICS volume Knob on each Audio Panel to the desired intercom level. 6) Reset squelch to automatic, or adjust to the appropriate level manually. Once this procedure has been completed, the master volume controls on both Audio Panels may now be adjusted. The flight crew can change settings, keeping in mind the notes above. Pilot Master Volume Control Radio Volume Knobs Adjust Radio Level Master Volume Knobs Adjust Headphone Volume Level COM Radio Audio NAV Radio Audio Copilot Master Volume Control Figure 4-65 Radio and Headphone Volume Controls 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 173 AUDIO PANEL AND CNS 4.8 ABNORMAL OPERATION Abnormal operation of the system includes failures of the system components and failure of associated equipment, including switches and external devices. STUCK MICROPHONE If the push-to-talk (PTT) Key becomes stuck, the COM transmitter stops transmitting after 35 seconds of continuous operation. An alert appears on the PFD to advise the crew of a stuck microphone. The COM1 MIC or COM2 MIC Key Annunciator on the Audio Panel flashes as long as the PTT Key remains stuck. Figure 4-66 Stuck Microphone Alert COM TUNING FAILURE In case of a COM system tuning failure, the emergency frequency (121.500 MHz) is automatically tuned in the radio in which the tuning failure occurred. Depending on the failure mode, a red X may appear on the frequency display. Emergency Channel Loaded Automatically Figure 4-67 COM Tuning Failure PFD FAILURE, DUAL SYSTEM If PFD1 fails, COM1 and NAV1 display a red X on both remaining displays. NAV1 is unavailable. COM1 automatically tunes 121.500 MHz, but the frequency is not shown. Emergency Channel Loaded Automatically Figure 4-68 Frequency Section of PFD2 Display after PFD1 Failure 174 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUDIO PANEL AND CNS If the HSDB switch is in NORMAL MODE and the MFD fails, COM2 and NAV2 display a red X on the remaining PFD display. NAV2 is unavailable. COM2 tunes 121.500 MHz, but the frequency is not shown. If the HSDB switch is in REV MODE and PFD2 fails, COM2 and NAV2 display a red X on the remaining PFD display. NAV2 is unavailable. COM2 tunes 121.500 MHz, but the frequency is not shown. Figure 4-69 PFD1 Display after PFD2 Failure with HSDB Switch in REV Mode AUDIO PANEL FAIL-SAFE OPERATION If there is a failure of both Audio Panels, a fail-safe circuit connects the pilot’s headset and microphone directly to the COM1 transceiver and the copilot’s headset directly to the COM2 transceiver. Audio is not available on the speakers. If there is a failure of one Audio Panel, that side only has access to their respective on-side failsafe COM. NOTE: Audio is not available on the speakers in case of an Audio Panel and its cross-side GIA unit simultaneous failure. If there is a failure of one Audio Panel, the remaining Audio Panel does not have access to the other side’s COM or NAV. For example, if the pilot side Audio Panel fails, the copilot side Audio Panel has access to all the radios except for COM1 and NAV1. In this case, the copilot can receive the audio from NAV2 and operate COM2 for transmission/reception. In addition, if there is a failure of one Audio Panel, the following functions are no longer available on the failed side; NAV/ILS audio, speaker, cockpit/cockpit-passengers intercom, aural warning alerts on headset, entertainment inputs, and digital recording radio. Also, if a stereo headset is in use, and an Audio Panel fails, only the left channel will be heard in the headphones. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 175 AUDIO PANEL AND CNS REVERSIONARY MODE The red DISPLAY BACKUP Button selects the Reversionary Mode. See the System Overview Section for more information on Reversionary Mode. Figure 4-70 Reversionary Mode Button 176 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT SECTION 5 FLIGHT MANAGEMENT 5.1 INTRODUCTION The Prodigy® Flight Deck 100 is an integrated flight, engine, communication, navigation and surveillance system. This section of the Pilot’s Guide explains flight management using the Prodigy® Flight Deck 100. The most prominent part of the system are the three full color displays: two Primary Flight Displays (PFD) and a Multi Function Display (MFD). The information to successfully navigate the aircraft using the GPS sensors is displayed on the PFD and the MFD. See examples in the Figure 5-1 and Figure 5-2. Detailed descriptions of flight management functions are discussed later in this section. A brief description of the GPS navigation data on the PFD and MFD follows. Navigation mode indicates which sensor is providing the course data (e.g., GPS, VOR) and the flight plan phase (e.g., Departure (DPRT), Terminal (TERM), Enroute (ENR), Oceanic (OCN), RNAV Approach (LNAV, LNAV+V, L/ VNAV, LP, LP+V, LPV), or Missed Approach (MAPR)). L/VNAV, LP, LP+V, and LPV approach service levels are only available with SBAS. L/VNAV will be flown as LNAV when SBAS is not available. The Inset Map is a small version of the MFD Navigation Map and can be displayed in the lower left corner of the PFD. When the system is in reversionary mode, the Inset Map is displayed in the lower right corner. The Inset Map is displayed by pressing the INSET Softkey. Pressing the INSET Softkey again, then pressing the OFF Softkey removes the Inset Map. The Navigation Map displays aviation data (e.g., airports, VORs, airways, airspaces), geographic data (e.g., cities, lakes, highways, borders), topographic data (map shading indicating elevation), and hazard data (e.g., traffic, terrain, weather). The amount of displayed data can be reduced by selecting the DCLTR Softkey. The Navigation Map can be oriented four different ways: North Up (NORTH UP), Track Up (TRK UP), Desired Track Up (DTK UP), or Heading Up (HDG UP). An aircraft icon is placed on the Navigation Map at the location corresponding to the calculated present position. The aircraft position and the flight plan legs are accurately based on GPS calculations. The basemap upon which these are placed are from a source with less resolution, therefore the relative position of the aircraft to map features is not exact. The leg of the active flight plan currently being flown is shown as a magenta line on the navigation map. The other legs are shown in white. There are 28 different map ranges available, from 500 feet to 2000 nm. The current range is indicated in the lower right corner of the map and represents the top-to-bottom distance covered by the map. To change the map range on any map, turn the Joystick counter-clockwise to zoom in ( -, decreasing), or clockwise to zoom out (+, increasing). The Direct-to Window, the Flight Plan Window, the Procedures Window, and the Nearest Airports Window can be displayed in the lower right corner of the PFD. Details of these windows are discussed in detail later in the section. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 177 FLIGHT MANAGEMENT Navigation Status Box Navigation Mode Inset Map Location of: - Direct To Window - Flight Plan Window - Procedures Window - Nearest Airports Window Figure 5-1 GPS Navigation Information on the PFD Navigation Status Box Map Orientation Navigation Page Title Navigation Map - Aviation Data - Geographic Data - Topographic Data - Hazard Data Aircraft Icon at Present Position Active Flight Plan Leg Flight Plan Leg Map Range Figure 5-2 GPS Navigation Information on the MFD Navigation Page NAVIGATION STATUS BOX The Navigation Status Box located at the top of the PFD contains two fields displaying the following information: PFD Navigation Status Box 178 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT • Active flight plan leg (e.g., ‘D-> KICT’ or ‘KIXD -> KCOS’) or flight plan annunciations (e.g., ‘Turn right to 021˚ in 8 seconds’) • Distance (DIS) and Bearing (BRG) to the next waypoint or flight plan annunciations (e.g., ‘TOD within 1 minute’) The symbols used in the PFD status bar are: Symbol Description Symbol Description Active Leg Left Holding Pattern Direct-to Vector to Final Right Procedure Turn Right DME Arc Left Procedure Turn Left DME Arc Right Holding Pattern The Navigation Status Box located at the top of the MFD contains four data fields, each displaying one of the following items: BRG DIS DTK END ENR ESA ETA ETE FOB FOD GS ISA LDG MSA TAS TKE TRK VSR XTK Bearing Distance Desired Track Endurance ETE to Final Destination Enroute Safe Altitude Estimated Time of Arrival Estimated Time Enroute Fuel on Board Fuel over Destination Ground Speed ISA Relative Temperature ETA at Final Destination Minimum Safe Altitude True Air Speed Track Angle Error Track Vertical Speed Required Crosstrack Error MFD Navigation Status Box The navigation information displayed in the four data fields can be selected on the MFD Data Bar Fields Box on the AUX - System Setup Page. The default selections (in order left to right) are GS, DTK, TRK, and ETE. Changing a field in the MFD Navigation Status Box: 1) Select the System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the desired field number in the MFD Data Bar Fields Box. 4) Turn the small FMS Knob to display and scroll through the data options list. 5) Select the desired data. 6) Press the ENT Key. Selecting the DFLTS Softkey returns all fields to the default setting. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 179 FLIGHT MANAGEMENT 5.2 USING MAP DISPLAYS Map displays are used extensively to provide situational awareness in flight. Most maps can display the following information: • Airports, NAVAIDs, airspaces, airways, land data (highways, cities, lakes, rivers, borders, etc.) with names • Map range •Wind direction and speed • Map orientation • Icons for enabled map features • Aircraft icon (representing present position) • Nav range ring • Obstacle data • Map Pointer information (distance and bearing to pointer, location of pointer, name, and other pertinent information) • Fuel range ring • Flight plan legs • User waypoints • Track vector • Topography scale • Topography data The information in this section applies to the following maps unless otherwise noted: • All Map Group Pages (MAP) • All Waypoint Group Pages (WPT) • AUX - Trip Planning • All Nearest Group Pages (NRST) • Flight Plan Pages (FPL) • Direct-to Window • PFD Inset Map • Procedure Loading Pages MAP ORIENTATION Maps are shown in one of four different orientation options, allowing flexibility in determining aircraft position relative to other items on the map (north up) or for determining where map items are relative to where the aircraft is going (track up, desired track up, or heading up). The map orientation is shown in the upper right corner of the map. Figure 5-3 Map Orientation • North up (NORTH UP) aligns the top of the map display to north (default setting). • Track up (TRK UP) aligns the top of the map display to the current ground track. 180 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT • Desired track up (DTK UP) aligns the top of the map display to the desired course. • Heading up (HDG UP) aligns the top of the map display to the current aircraft heading. NOTE: When panning or reviewing active flight plan legs in a non-North Up orientation, the map does not show the map orientation nor the wind direction and speed. NOTE: Map orientation can only be changed on the Navigation Map Page. Any other displays that show navigation data reflect the orientation selected for the Navigation Map Page. Changing the Navigation Map orientation: 1) With the Navigation Map Page displayed, press the MENU Key. The cursor flashes on the ‘Map Setup’ option. Map Setup Selection Figure 5-4 Navigation Map Page Menu Window 2) Press the ENT Key to display the Map Setup Window. 3) Turn the large FMS Knob, or press the ENT Key once, to select the ‘ORIENTATION’ field. Map Group Selection Orientation Field Auto North Up - On/Off - Minimum Range Figure 5-5 Map Setup Menu Window - Map Group 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 181 FLIGHT MANAGEMENT 4) Turn the small FMS Knob to select the desired orientation. 5) Press the ENT Key to select the new orientation. 6) Press the FMS Knob to return to the base page. The map can be configured to switch automatically to a north up orientation when the map range reaches a minimum range. Enabling/disabling Auto North Up and selecting the minimum switching range: 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘AUTO NORTH UP’ field. 6) Select ‘On’ or ‘Off’ using the small FMS Knob. 7) Press the ENT Key to accept the selected option. The flashing cursor highlights the range field. 8) Use the small FMS Knob to select the desired range. 9) Press the ENT Key to accept the selected option. 10) Press the FMS Knob to return to the Navigation Map Page. MAP RANGE There are 28 different map ranges available, from 500 feet to 2000 nm. The current range is indicated in the lower right corner of the map and represents the top-to-bottom distance covered by the map. When the map range is decreased to a point that exceeds the capability of the system to accurately represent the map, a magnifying glass icon is shown to the left of the map range. To change the map range turn the Joystick counter-clockwise to decrease the range, or clockwise to increase the range. Range Overzoom Figure 5-6 Map Range 182 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT AUTO ZOOM Auto zoom allows the system to change the map display range to the smallest range clearly showing the active waypoint. Auto zoom can be overridden by adjusting the range with the Joystick, and remains until the active waypoint changes, a terrain or traffic alert occurs, the aircraft takes off, or the manual override times out (timer set on Map Setup Window). Auto zoom is suspended while the map pointer is active. If a terrain caution or warning occurs, all navigation maps automatically adjust to the smallest map range clearly showing the potential impact points If a new traffic advisory alert occurs, any map page capable of displaying traffic advisory alerts automatically adjusts to the smallest map range clearly showing the traffic advisory. When terrain or traffic alerts clear, the map returns to the previous auto zoom range based on the active waypoint. The auto zoom function can be turned on or off independently for the PFDs and MFD. Control of the ranges at which the auto zoom occurs is done by setting the minimum and maximum ‘look forward’ times (set on the Map Setup Window for the Map Group). These settings determine the minimum and maximum distance to display based upon the aircraft’s ground speed. • Waypoints that are long distances apart cause the map range to increase to a point where many details on the map are decluttered. If this is not acceptable, lower the maximum look ahead time to a value that limits the auto zoom to an acceptable range. • Waypoints that are very short distances apart cause the map range to decrease to a point where situational awareness may not be what is desired. Increase the minimum look ahead time to a value that limits the auto zoom to a minimum range that provides acceptable situational awareness. • Flight plans that have a combination of long and short legs cause the range to increase and decrease as waypoints sequence. To avoid this, auto zoom can be disabled or the maximum/minimum times can be adjusted. • The ‘time out’ time (configurable on the Map Setup Page for the Map Group) determines how long auto zoom is overridden by a manual adjustment of the range knob. At the expiration of this time, the auto zoom range is restored. Setting the ‘time out’ value to zero causes the manual override to never time out. • When the maximum ‘look forward’ time is set to zero, the upper limit becomes the maximum range available (2000 nm). • When the minimum ‘look forward’ time is set to zero, the lower limit becomes 1.5 nm. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 183 FLIGHT MANAGEMENT Auto Zoom: MFD Only, PFD Only, All On Manual Range Override Expiration Time Maximum Look Forward Time Minimum Look Forward Time Figure 5-7 Map Setup Menu Window - Map Group, Auto Zoom Configuring automatic zoom: 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘AUTO ZOOM’ field. 6) Select ‘MFD Only’, ‘PFD Only’, or ‘ALL On’. 7) Press the ENT Key to accept the selected option. The flashing cursor highlights the ‘MAX LOOK FWD’ field. Times are from zero to 999 minutes. 8) Use the FMS Knobs to set the time. Press the ENT Key. 9) Repeat step 8 for ‘MIN LOOK FWD’ (zero to 99 minutes) and ‘TIME OUT’ (zero to 99 minutes). 10) Press the FMS Knob to return to the Navigation Map Page. 184 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT MAP PANNING Map panning allows the pilot to: • View parts of the map outside the displayed range without adjusting the map range • Highlight and select locations on the map • Review information for a selected airport, NAVAID or user waypoint • Designate locations for use in flight planning • View airspace and airway information When the panning function is selected by pressing the Joystick, the Map Pointer flashes on the map display. A window also appears at the top of the map display showing the latitude/longitude position of the pointer, the bearing and distance to the pointer from the aircraft’s present position, and the elevation of the land at the position of the pointer. Map Pointer Information Map Pointer Figure 5-8 Navigation Map - Map Pointer Activated NOTE: The map is normally centered on the aircraft’s position. If the map has been panned and there has been no pointer movement for about 60 seconds, the map reverts back to centered on the aircraft position and the flashing pointer is removed. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 185 FLIGHT MANAGEMENT When the Map Pointer is placed on an object, the name of the object is highlighted (even if the name was not originally displayed on the map). When any map feature or object is selected on the map display, pertinent information is displayed. Information about Point of Interest Map Pointer on POI Figure 5-9 Navigation Map - Map Pointer on Point of Interest When the Map Pointer crosses an airspace boundary, the boundary is highlighted and airspace information is shown at the top of the display. The information includes the name and class of airspace, the ceiling in feet above Mean Sea Level (MSL), and the floor in feet MSL. 186 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Information about Airspace Map Pointer on Airspace Figure 5-10 Navigation Map - Map Pointer on Airspace Panning the map: 1) Press the Joystick to display the Map Pointer. 2) Move the Joystick to move the Map Pointer around the map. 3) Press the Joystick to remove the Map Pointer and recenter the map on the aircraft’s current position. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 187 FLIGHT MANAGEMENT Reviewing information for an airport, NAVAID, or user waypoint: 1) Place the Map Pointer on a waypoint. 2) Press the ENT Key to display the Waypoint Information Page for the selected waypoint. 3) Select the GO BACK Softkey, the CLR Key, or the ENT Key to exit the Waypoint Information Page and return to the Navigation Map showing the selected waypoint. NAVAID Information GO BACK Softkey Figure 5-11 Navigation Map - Information Window - NAVAID 188 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Viewing airspace information for a special-use or controlled airspace: 1) Place the Map Pointer on an open area within the boundaries of an airspace. 2) Press the ENT Key to display an options menu. 3) ‘Review Airspaces’ should already be highlighted, if not select it. Press the ENT Key to display the Airspace Information Page for the selected airspace. 4) Press the CLR or ENT Key to exit the Airspace Information Page. Airspace Information Figure 5-12 Navigation Map - Information Window - Airspace 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 189 FLIGHT MANAGEMENT MEASURING BEARING AND DISTANCE Distance and bearing from the aircraft’s present position to any point on the viewable navigation map may be calculated using the ‘Measure Bearing and Distance’ selection from Navigation Map page menu. The bearing and distance tool displays a dashed Measurement Line and a Measure Pointer to aid in graphically identifying points with which to measure. Lat/Long, distance and elevation data for the Measure Pointer is provided in a window at the top of the navigation map. Measuring bearing and distance between any two points: 1) Press the MENU Key (with the Navigation Map Page displayed). 2) Highlight the ‘Measure Bearing/Distance’ field. 3) Press the ENT Key. A Measure Pointer is displayed on the map at the aircraft’s present position. 4) Move the Joystick to place the reference pointer at the desired location. The bearing and distance are displayed at the top of the map. Elevation at the current pointer position is also displayed. Pressing the ENT Key changes the starting point for measuring. 5) To exit the Measure Bearing/Distance option, press the Joystick; or select ‘Stop Measuring’ from the Page Menu and press the ENT Key. Pointer Lat/Long Measurement Information Measurement Line Figure 5-13 Navigation Map - Measuring Bearing and Distance 190 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT TOPOGRAPHY All navigation maps can display various shades of topography colors representing land elevation, similar to aviation sectional charts. Topographic data can be displayed or removed as described in the following procedures. Navigation Map Topographic Data Navigation Map Black Background TOPO Softkey Not Enabled Topographic Data on Profile Map TOPO Softkey Enabled TOPO Off TOPO On Figure 5-14 Navigation Map - Topographic Data Displaying/removing topographic data on all pages displaying navigation maps: 1) Select the MAP Softkey (the INSET Softkey for the PFD Inset Map). 2) Select the TOPO Softkey. 3) Select the TOPO Softkey again to remove topographic data from the Navigation Map. When topographic data is removed from the page, all navigation data is presented on a black background. Displaying/removing topographic data (TOPO DATA) using the Navigation Map Page Menu: 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘TOPO DATA’ field. 6) Select ‘On’ or ‘Off’. 7) Press the FMS Knob to return to the Navigation Map Page. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 191 FLIGHT MANAGEMENT TOPO DATA On/Off TOPO DATA Range Figure 5-15 Navigation Map Setup Menu - TOPO DATA Setup The topographic data range is the maximum map range on which topographic data is displayed. NOTE: Since the PFD Inset Map is much smaller than the MFD navigation maps, items are removed on the PFD Inset Map two range levels smaller than the range selected in the Map Setup pages (e.g., a setting of 100 nm removes the item at ranges above 100 nm on MFD navigation maps, while the PFD Inset Map removes the same item at 50 nm). Selecting a topographical data range (TOPO DATA): 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘TOPO DATA’ range field. TOPO ranges are from 500 ft to 2000 nm. 6) To change the TOPO range setting, turn the small FMS Knob to display the range list. 7) Select the desired range using the small FMS Knob. 8) Press the ENT Key. 9) Press the FMS Knob to return to the Navigation Map Page. In addition, the Navigation Map can display a topographic scale (located in the lower right hand side of the map) showing a scale of the terrain elevation and current elevation values. 192 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Maximum Displayed Elevation Minimum Displayed Elevation Aircraft Altitude (MSL) Range of Displayed Elevations Ground Elevation at Map Pointer Location (only visible when Map Pointer is displayed) Figure 5-16 Navigation Map - TOPO SCALE Displaying/removing the topographic scale (TOPO SCALE): 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Select the ‘Map’ group and press the ENT Key. 4) Highlight the ‘TOPO SCALE’ field. 5) Select ‘On’ or ‘Off’. 6) Press the FMS Knob to return to the Navigation Map Page. TOPO SCALE On/Off Figure 5-17 Navigation Map Setup Menu - TOPO SCALE Setup 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 193 FLIGHT MANAGEMENT MAP SYMBOLS This section discusses the types of land and aviation symbols that can be displayed. Each listed type of symbol can be turned on or off, and the maximum range to display each symbol can be set. The decluttering of the symbols from the map using the DCLTR Softkey is also discussed. LAND SYMBOLS The following items are configured on the land menu: Land Symbols (Text label size can be None, Small, Medium (Med), or Large (Lrg)) Symbol Latitude/Longitude (LAT/LON) Default Maximum Range (nm) Range (nm) Off 2000 Highways and Roads Interstate Highway (FREEWAY) 300 800 International Highway (FREEWAY) 300 800 US Highway (NATIONAL HWY) 30 80 State Highway (LOCAL HWY) 15 30 Local Road (LOCAL ROAD) 8 15 Railroads (RAILROAD) 15 30 LARGE CITY (> 200,000) 800 1500 MEDIUM CITY (> 50,000) 100 200 SMALL CITY (> 5,000) States and Provinces (STATE/PROV) 20 800 50 1500 Rivers and Lakes (RIVER/LAKE) 200 500 USER WAYPOINT 150 300 N/A Table 5-1 Land Symbol Information 194 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT AVIATION SYMBOLS The following items are configured on the aviation menu: Aviation Symbols (Text label size can be None, Small, Medium (Med), or Large (Lrg)) Symbol Default Maximum Range (nm) Range (nm) Active Flight Plan Leg (ACTIVE FPL) 2000 2000 Non-active Flight Plan Leg (ACTIVE FPL) 2000 2000 2000 250 150 50 3 Off 15 2000 500 300 100 20 100 30 Non-directional Beacon (NDB WAYPOINT) 15 30 VOR (VOR WAYPOINT) 150 300 Class B Airspace/TMA (CLASS B/TMA) 200 500 Class C Airspace/TCA (CLASS C/TCA) 200 500 Class D Airspace (CLASS D) 150 300 Restricted Area (RESTRICTED) 200 500 Military Operations Area [MOA(MILITARY)] 200 500 Other/Air Defense Interdiction Zone (OTHER/ADIZ) 200 500 Temporary Flight Restriction (TFR) 500 2000 Active Flight Plan Waypoint (ACTIVE FPL WPT) Large Airports (LARGE APT) Medium Airports (MEDIUM APT) Small Airports (SMALL APT) Taxiways (SAFETAXI) Runway Extension (RWY EXTENSION) Intersection (INT WAYPOINT) See Airports, NAVAIDs See Additional Features N/A Table 5-2 Aviation Symbol Information 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 195 FLIGHT MANAGEMENT SYMBOL SETUP All pages with maps can display land symbols (roads, lakes, borders, etc). Land symbols can be removed totally (turned off). Displaying/removing all land symbols: 1) Press the MENU Key with the Navigation Map Page displayed. The Page Menu is displayed and the cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Group Menu is displayed and the cursor flashes on the ‘Map’ option. 3) Highlight the ‘LAND DATA’ field. 4) Select ‘On’ or ‘Off’. 5) Press the FMS Knob to return to the Navigation Map Page. LAND DATA On/Off Figure 5-18 Navigation Map Setup Menu - LAND DATA Setup The label size (TEXT) sets the size at which labels appear on the display (none, small, medium, and large). The range (RNG) sets the maximum range at which items appear on the display. Selecting a ‘Land’ or ‘Aviation’ group item text size and range: 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Select the ‘Land’ or ‘Aviation’ group. 4) Press the ENT Key. The cursor flashes on the first field. 5) Select the desired land option. 6) Select the desired text size. 7) Press the ENT Key to accept the selected size. 8) Select the desired range. 9) Press the ENT Key to accept the selected range. 10) Press the FMS Knob to return to the Navigation Map Page. 196 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Text Label Size (None, Small, Med, or Lrg) Maximum Display Range Figure 5-19 Navigation Map Setup Menu - LAND GROUP Setup Text Label Size (None, Small, Med, or Lrg) Maximum Display Range Figure 5-20 Navigation Map Setup Menu - AVIATION GROUP Setup NOTE: Since the PFD Inset Map is much smaller than the MFD navigation maps, items are removed on the PFD Inset Map two range levels smaller than the range selected in the Map Setup pages (e.g., a setting of 100 nm removes the item at ranges above 100 nm on MFD navigation maps, while the PFD Inset Map removes the same item at 50 nm). 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 197 FLIGHT MANAGEMENT MAP DECLUTTER The declutter feature allows the pilot to progressively step through four levels of removing map information. The declutter level is displayed in the DCLTR Softkey and next to the Declutter Menu Option. Declutter Level DCLTR Softkey Navigation Map Page Menu Figure 5-21 Navigation Map - Declutter Level Indications Decluttering the map: Select the DCLTR Softkey with the Navigation Map Page displayed. The current declutter level is shown. With each softkey selection, another level of map information is removed. Or: 1) Press the MENU Key with the Navigation Map Page displayed. 2) Select ‘Declutter’. The current declutter level is shown. 3) Press the ENT Key. Decluttering the PFD Inset Map: 1) Press the INSET Softkey. 2) Press the DCLTR Softkey. The current declutter level is shown. With each selection, another level of map information is removed. 198 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Table 5-3 lists the items that are decluttered at each map detail level. The ‘X’ represents map items decluttered for each level of detail. Item Data Link Radar Precipitation Data Link Lightning Graphical METARs Airports Safe Taxi Runway Labels TFRs Restricted MOA (Military) User Waypoints Latitude/Longitude Grid NAVAIDs (does not declutter if used to define airway) Intersections (does not declutter if used to define airway) Class B Airspaces/TMA Class C Airspaces/TCA Class D Airspaces Other Airspaces/ADIZ Obstacles Cities Roads Railroads State/Province Boundaries Declutter-1 Declutter-2 Declutter-3 X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X X Table 5-3 Navigation Map Items Decluttered for each Detail Level 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 199 FLIGHT MANAGEMENT AIRWAYS This airways discussion is based upon the North American airway structure. The airway structure in places other than North America vary by location, etc. and are not discussed in this book. Low Altitude Airways (or Victor Airways) primarily serve smaller piston-engine, propeller-driven airplanes on shorter routes and at lower altitudes. Airways are eight nautical miles wide and start 1,200 feet above ground level (AGL) and extend up to 18,000 feet mean sea level (MSL). Low Altitude Airways are designated with a “V” before the airway number (hence the name “Victor Airways”) since they run primarily between VORs. High Altitude Airways (or Jet Routes) primarily serve airliners, jets, turboprops, and turbocharged piston aircraft operating above 18,000 feet MSL. Jet Routes start at 18,000 feet MSL and extend upward to 45,000 feet MSL (altitudes above 18,000 feet are called “flight levels” and are described as FL450 for 45,000 feet MSL). Jet Routes are designated with a “J” before the route number. Low Altitude Airways are drawn in gray (the same shade used for roads). High Altitude Airways are drawn in green. When both types of airways are displayed, High Altitude Airways are drawn on top of Low Altitude Airways. When airways are selected for display on the map, the airway waypoints (VORs, NDBs and Intersections) are also displayed. Low Altitude Airway (Victor Airway) High Altitude Airway (Jet Route) Figure 5-22 Airways on MFD Navigation Page 200 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Airways may be displayed on the map at the pilot’s discretion using either a combination of AIRWAYS Softkey presses, or menu selections using the MENU Key from the Navigation Map Page. The Airway range can also be programmed to only display Airways on the MFD when the map range is at or below a specific number. Displaying/removing airways: 1) Select the MAP Softkey. 2) Select the AIRWAYS Softkey. Both High and Low Altitude Airways are displayed (AIRWAY ON). 3) Select the softkey again to display Low Altitude Airways only (AIRWAY LO). 4) Select the softkey again to display High Altitude Airways only (AIRWAY HI). 5) Select the softkey again to remove High Altitude Airways. No airways are displayed (AIRWAYS). Or: 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Turn the small FMS Knob to select the ‘Airways’ group, and press the ENT Key. 4) Turn the large FMS Knob to highlight the ‘AIRWAYS’ field. 5) Turn the FMS Knob to select ‘Off’, ‘All’, ‘LO Only’, or ‘HI Only’, and press the ENT Key. 6) Press the FMS Knob to return to the Navigation Map Page. Airway Display Selection Off, All, LO Only, HI Only Low Altitude Airway Range High Altitude Airway Range Figure 5-23 Navigation Map Setup Menu - AIRWAYS Setup The airway range is the maximum map range on which airways are displayed. Selecting an airway range (LOW ALT AIRWAY or HI ALT AIRWAY): 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Turn the small FMS Knob to select the ‘Airways’ group, and press the ENT Key. 4) Highlight the ‘LOW ALT AIRWAY’ or ‘HI ALT AIRWAY’ range field. 5) To change the range setting, turn the small FMS Knob to display the range list. 6) Select the desired range using the small FMS Knob. 7) Press the ENT Key. 8) Press the FMS Knob to return to the Navigation Map Page. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 201 FLIGHT MANAGEMENT The following range items are configurable on the airways menu: Airway Type Symbol Default Maximum Range (nm) Range (nm) 200 500 Low Altitude Airway (LOW ALT AIRWAY) High Altitude Airway (HI ALT AIRWAY) 300 500 Table 5-4 Airway Range Information TRACK VECTOR The Navigation Map can display a track vector that is useful in minimizing track angle error. The track vector is a solid cyan line segment extended to a predicted location. The track vector look-ahead time is selectable (30 sec, 60 sec (default), 2 min, 5 min, 10 min, 20 min) and determines the length of the track vector. The track vector shows up to 90 degrees of a turn for the 30 and 60 second time settings. It is always a straight line for the 2 min, 5 min, 10 min and 20 min settings. Track Vector Figure 5-24 Navigation Map -Track Vector Displaying/removing the track vector: 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘TRACK VECTOR’ field. 6) Select ‘On’ or ‘Off’. Press the ENT Key to accept the selected option. The flashing cursor highlights the look ahead time field. Use the FMS Knob to select the desired time. Press the ENT Key. 7) Press the FMS Knob to return to the Navigation Map Page. 202 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Wind Vector On/Off Nav Range Ring On/Off Track Vector - On/Off - Look Ahead Time Fuel Range - On/Off - Fuel Reserve Time Figure 5-25 Navigation Map Setup Menu -TRACK VECTOR, WIND VECTOR, NAV RANGE RING, FUEL RANGE RING Setup WIND VECTOR The map displays a wind vector arrow in the upper right-hand portion of the screen. Wind vector information is displayed as a white arrow pointing in the direction in which the wind is moving for wind speeds greater than or equal to 1 kt. Wind Direction Wind Speed Figure 5-26 Navigation Map - Wind Vector NOTE: The wind vector is not displayed until the aircraft is moving. It is not displayed on the Waypoint Information pages. Displaying/removing the wind vector: 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘WIND VECTOR’ field. 6) Select ‘On’ or ‘Off’. 7) Press the FMS Knob to return to the Navigation Map Page. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 203 FLIGHT MANAGEMENT NAV RANGE RING The Nav Range Ring shows the direction of travel (ground track) on a rotating compass card. The range is determined by the map range. The range is 1/4 of the map range (e.g., 37.5 nm on a 150 nm map). Range (radius) Nav Range Ring Figure 5-27 Navigation Map - Nav Range Ring NOTE: The Nav Range Ring is not displayed on the Waypoint Information pages, Nearest pages, or Direct-to Window map. Displaying/removing the Nav Range Ring: 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘NAV RANGE RING’ field. 6) Select ‘On’ or ‘Off’. 7) Press the FMS Knob to return to the Navigation Map Page. NOTE: The Nav Range Ring is referenced to either magnetic or true north, based on the selection on the AUX - System Setup Page. 204 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT FUEL RANGE RING The map can display a fuel range ring which shows the remaining flight distance. A dashed green circle indicates the selected range to reserve fuel. A solid green circle indicates the total endurance range. If only reserve fuel remains, the range is indicated by a solid yellow circle. Time to Reserve Fuel Total Endurance Range Range to Reserve Fuel Figure 5-28 Navigation Map - Fuel Range Ring Displaying/removing the fuel range ring and selecting a fuel range time: 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘FUEL RNG (RSV)’ field. 6) Select ‘On’ or ‘Off’. 7) Highlight the fuel reserve time field. This time should be set to the amount of flight time equal to the amount of fuel reserve desired. 8) To change the reserve fuel time, enter a time (00:00 to 23:59; hours:minutes). The default setting is 00:45 minutes. 9) Press the ENT Key. 10) Press the FMS Knob to return to the Navigation Map Page. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 205 FLIGHT MANAGEMENT FIELD OF VIEW (SVS) The map can display the boundaries of the PFD Synthetic Vision System (SVS) lateral field of view. The field of view is shown as two dashed lines forming a V shape in front of the aircraft symbol on the map. This is only available if SVS is installed on the aircraft. Lateral Field of View Boundaries Figure 5-29 Navigation Map - Field of View Displaying/removing the field of view: 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘FIELD OF VIEW’ field. 6) Select ‘On’ or ‘Off’. 7) Press the FMS Knob to return to the Navigation Map Page. 206 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT SELECTED ALTITUDE INTERCEPT ARC The map can display the location along the current track where the aircraft will intercept the selected altitude. The location will be shown as a cyan arc when the aircraft is actually climbing or descending. Range to Altitude Arc Figure 5-30 Navigation Map - Range to Altitude Arc Displaying/removing the selected altitude intercept arc: 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘SEL ALT ARC’ field. 6) Select ‘On’ or ‘Off’. 7) Press the FMS Knob to return to the Navigation Map Page. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 207 FLIGHT MANAGEMENT 5.3 WAYPOINTS Waypoints are predetermined geographical positions (internal database) or pilot-entered positions, and are used for all phases of flight planning and navigation. Communication and navigation frequencies can be tuned “automatically” from various Waypoint Information (WPT) pages, Nearest (NRST) pages, and the Nearest Airports Window (on PFD). This auto-tuning feature simplifies frequency entry over manual tuning. Refer to the Audio Panel and CNS section for details on autotuning. Waypoints can be selected by entering the ICAO identifier, entering the name of the facility, or by entering the city name. See the System Overview section for detailed instructions on entering data. As a waypoint identifier, facility name, or location is entered, the Spell’N’Find™ feature scrolls through the database, displaying those waypoints matching the characters which have been entered to that point. A direct-to navigation leg to the selected waypoint can be initiated by pressing the Direct-to Key on any of the waypoint pages. Identifier Entry Field City Entry Field Facility Entry Field Map Area Showing Entered Waypoint - Waypoint Identifier - Type (symbol) - Facility Name - City Entered Waypoint on Map Waypoint Location Figure 5-31 Waypoint Information Window If duplicate entries exist for the entered facility name or location, additional entries may be viewed by continuing to turn the small FMS Knob during the selection process. If duplicate entries exist for an identifier, a Duplicate Waypoints Window is displayed when the ENT Key is pressed. 208 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Identifier with Duplicates Duplicate Waypoints Duplicate Message Figure 5-32 Waypoint Information Window - Duplicate Identifier AIRPORTS NOTE: ‘North Up’ orientation on the Airport Information Page cannot be changed; the pilot needs to be aware of proper orientation if the Navigation Map orientation is different from the Airport Information Page Map. The Airport Information Page is the first page in WPT group and allows the pilot to view airport information, load frequencies (COM, NAV, and lighting), review runways, and review instrument procedures that may be involved in the flight plan. See the Audio Panel and CNS Section for more information on loading frequencies (auto-tuning). After engine startup, the Airport Information Page defaults to the airport where the aircraft is located. After a flight plan has been loaded, it defaults to the destination airport. On a flight plan with multiple airports, it defaults to the airport which is the current active waypoint. In addition to displaying a map of the currently selected airport and surrounding area, the Airport Information Page displays airport information in three boxes labeled ‘AIRPORT’, ‘RUNWAYS’, and ‘FREQUENCIES’. For airports with multiple runways, information for each runway is available. This information is viewed on the Airport Information Page by pressing the INFO softkey until INFO-1 is displayed. The following descriptions and abbreviations are used on the Airport Information Page: • Usage type: Public, Military, Private, or Heliport • Runway surface type: Hard, Turf, Sealed, Gravel, Dirt, Soft, Unknown, or Water • Runway lighting type: No Lights, Part Time, Full Time, Unknown, or PCL Freq (for pilot-controlled lighting) • COM Availability: TX (transmit only), RX (receive only), PT (part time), i (additional information available) 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 209 FLIGHT MANAGEMENT Airport Information - ID/Facility/City - Usage Type/Region - Lat/Long/Elev - Fuel Available - Time Zone (UTC Offset) Navigation Map Showing Selected Airport Runway Information - Designation - Length/Width/Surface - Lighting Available Airport/Runway Diagram COM/NAV Freq. Info. - Identification - Frequency - Availability - Additional Information Softkeys Figure 5-33 Airport Information Page The directory information is viewed on the Airport Directory Page by pressing the INFO softkey until INFO2 is displayed. The following are types of airport directory information shown (if available) on the Airport Directory Page: • Airport: Identifier, Site Number, Name, City, State • Phones: Phone/Fax Numbers • Hours: Facility Hours, Light Hours, Tower Hours, Beacon Hours • Location: Sectional, Magnetic Variation • Frequencies: Type/Frequency • Transportation: Ground Transportation Type Available • Approach: Approach Facility Name, Frequency, Frequency Parameter 210 • Traffic Pattern Altitudes (TPA): Aircraft Class/Altitude • Weather: Service Type, Frequency, Phone Number • Flight Service Station (FSS): FSS Name, Phone Numbers • Runway: Headings, Length, Width, Obstructions, Surface • Obstructions: General Airport Obstructions • Special Operations at Airport • Instrument Approaches: Published Approach, Frequency • NAVAIDS: Type, Identifier, Frequency, Radial, Distance • Noise: Noise Abatement Procedures • Charts: Low Altitude Chart Number • Services Available: Category, Specific Service • Notes: Airport Notes • Pilot Controlled Lighting: High/Med/Low Clicks/Second • FBO: Type, Frequencies, Services, Fees, Fuel, Credit Cards, Phone/Fax Numbers Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Airport Information Airport Directory Information - ID/Facility/City - Usage Type/Region Softkeys Figure 5-34 Airport Directory Page Example Selecting an airport for review by identifier, facility name, or location: 1) From the Airport Information Page, press the FMS Knob. 2) Use the FMS Knobs and enter an identifier, facility name, or location. 3) Press the ENT Key. 4) Press the FMS Knob to remove the cursor. Selecting a runway: 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. 2) Turn the large FMS Knob to place the cursor in the ‘RUNWAYS’ Box, on the runway designator. 3) Turn the small FMS Knob to display the desired runway (if more than one) for the selected airport. 4) To remove the flashing cursor, press the FMS Knob. Viewing a destination airport: 190-00728-06 Rev. A From the Airport Information Page press the MENU Key. Select ‘View Destination Airport’. The Destination Airport is displayed. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 211 FLIGHT MANAGEMENT The Airport Frequencies Box uses the descriptions and abbreviations listed in the following table: Communication Frequencies Approach * Control Pre-Taxi Arrival * CTA * Radar ASOS Departure * Ramp ATIS Gate Terminal * AWOS Ground TMA * Center Helicopter Tower Class B * Multicom TRSA * Class C * Other Unicom Clearance Navigation Frequencies ILS LOC * May include Additional Information Table 5-5 Airport Frequency Abbreviations A departure, arrival, or approach can be loaded using the softkeys on the Airport Information Page. See the Procedures section for details. METARs or TAFs applicable to the selected airport can be selected for display (see the Hazard Avoidance section for details about weather). The system provides a NRST Softkey on the PFD, which gives the pilot quick access to nearest airport information (very useful if an immediate landing is required). The Nearest Airports Window displays a list of up to the 25 nearest airports (three entries can be displayed at one time). If there are more than three they are displayed in a scrollable list. If there are no nearest airports available, “NONE WITHIN 200NM” is displayed. Bearing/Distance to Airport Airport Identifier/ Type Approach Available Length of Longest Runway COM Freq. Info. - Identification - Frequency Additional Airports (within 200 nm) NRST Softkey Figure 5-35 Nearest Airports Window on PFD 212 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Pressing the ENT Key displays the PFD Airport Information Window for the highlighted airport. Pressing the ENT Key again returns to the Nearest Airports Window with the cursor on the next airport in the list. Continued presses of the ENT Key sequences through the information pages for all airports in the Nearest Airports list. Airport Information - ID/Type/City - Facility Airport Information - Usage/Time/Elev - Region Airport Information - Lat/Long Figure 5-36 Airport Information Window on PFD The Nearest Airports Page on the MFD is first in the group of NRST pages because of its potential use in the event of an in-flight emergency. In addition to displaying a map of the currently selected airport and surrounding area, the page displays nearest airport information in five boxes labeled ‘NEAREST AIRPORTS’, ‘INFORMATION’, ‘RUNWAYS’, ‘FREQUENCIES’, and ‘APPROACHES’. The selected airport is indicated by a white arrow, and a dashed white line is drawn on the navigation map from the aircraft position to the nearest airport. Up to five nearest airports, one runway, up to five frequencies, and up to six approaches are visible at one time. If there are more than can be shown, each list can be scrolled. If there are no items for display in a boxed area, text indicating that fact is displayed. The currently selected airport remains in the list until it is unselected. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 213 FLIGHT MANAGEMENT Nearest Airports - ID/Type - Bearing/Distance Nearest Airport Airport Information - Facility/City/Elevation Runway Information - Designation/Surface - Length/Width COM/NAV Freq. Info. - Identification - Frequency Navigation Map Showing Nearest Airport Approaches Available Window Selection Softkeys Figure 5-37 Nearest Airport Page LD APR Softkey (only available if an approach is highlighted) Viewing information for a nearest airport on the PFD: 1) Select the NRST Softkey to display the Nearest Airports Window. Press the FMS Knob to activate the cursor. 2) Highlight the airport identifier with the FMS Knob and press the ENT Key to display the Airport Information Window. 3) To return to the Nearest Airports Window press the ENT Key (with the cursor on ‘BACK’) or press the CLR Key. The cursor is now on the next airport in the nearest airports list. (Repeatedly pressing the ENT Key moves through the airport list, alternating between the Nearest Airports Window and the Airport Information Window.) 4) Press the CLR Key or the NRST Softkey to close the PFD Nearest Airports Window. Viewing information for a nearest airport on the MFD: 1) Turn the large FMS Knob to select the NRST page group. 2) Turn the small FMS Knob to select the Nearest Airports Page (it is the first page of the group, so it may already be selected). If there are no Nearest Airports available, “NONE WITHIN 200 NM” is displayed. 3) Select the APT Softkey; or press the FMS Knob; or press the MENU Key, highlight ‘Select Airport Window’ and press the ENT Key. The cursor is placed in the ‘NEAREST AIRPORTS’ Box. The first airport in the nearest airports list is highlighted. 4) Turn the FMS Knob to highlight the desired airport. (Pressing the ENT Key also moves to the next airport.) 5) Press the FMS Knob to remove the flashing cursor. 214 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Viewing runway information for a specific airport: 1) With the Nearest Airports Page displayed, select the RNWY Softkey; or press the MENU Key, highlight ‘Select Runway Window’; and press the ENT Key. The cursor is placed in the ‘RUNWAYS’ Box. 2) Turn the small FMS Knob to select the desired runway. 3) Press the FMS Knob to remove the flashing cursor. See the Audio Panel and CNS Section for frequency selection and the Procedures section for approaches. The Nearest Airports Box on the System Setup Page defines the minimum runway length and surface type used when determining the 25 nearest airports to display on the MFD Nearest Airports Page. A minimum runway length and/or surface type can be entered to prevent airports with small runways or runways that are not appropriately surfaced from being displayed. Default settings are 0 feet (or meters) for runway length and “HARD/SOFT” for runway surface type. Selecting nearest airport surface matching criteria: 1) Use the FMS Knob to select the System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the runway surface field in the Nearest Airports Box. 4) Turn the small FMS Knob to select the desired runway option (ANY, HARD ONLY, HARD/SOFT). 5) Press the ENT Key. 6) Press the FMS Knob to remove the flashing cursor. Selecting nearest airport minimum runway length matching criteria: 1) Use the FMS Knob to select the System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the minimum length field in the Nearest Airport Box. 4) Use the FMS Knob to enter the minimum runway length (zero to 25,000 feet) and press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor. Nearest Airport Criteria - Type of Runway Surface - Minimum Runway Length Figure 5-38 System Setup Page - Nearest Airport Selection Criteria 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 215 FLIGHT MANAGEMENT INTERSECTIONS NOTE: The VOR displayed on the Intersection Information Page is the nearest VOR, not necessarily the VOR used to define the intersection. The Intersection Information Page is used to view information about intersections. In addition to displaying a map of the currently selected intersection and surrounding area, the Intersection Information Page displays intersection information in three boxes labeled ‘INTERSECTION’, ‘INFORMATION’, and ‘NEAREST VOR’. Intersection Identifier Intersection Info - Region - Lat/Long Navigation Map Showing Selected Intersection Nearest VOR Info - Identifier/Type (symbol) - Radial to VOR - Distance to VOR Selected Intersection Figure 5-39 Intersection Information Page Selecting an intersection: 1) With the Intersection Information Page displayed, enter an identifier in the Intersection Box. 2) Press the ENT Key. 3) Press the FMS Knob to remove the flashing cursor. Or: 1) With the Nearest Intersections Page displayed, press the FMS Knob. 2) Press the ENT Key or turn either FMS Knob to select an identifier in the Nearest Intersection Box. 3) Press the FMS Knob to remove the flashing cursor. 216 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT The Nearest Intersections Page can be used to quickly find an intersection close to the flight path. In addition to displaying a map of the surrounding area, the page displays information for up to 25 nearest intersections in three boxes labeled ‘NEAREST INT’, ‘INFORMATION’, and ‘REFERENCE VOR’. The selected intersection is indicated by a white arrow. Up to sixteen intersections are visible at a time. If there are more than can be shown, the list can be scrolled. If there are no items for display, text indicating that fact is displayed. NOTE: The list only includes waypoints that are within 200 nm. Intersection Information - Identifier/Symbol - Bearing/Distance to intersection from aircraft position Navigation Map Showing Nearest Intersection Intersection Lat/Long Reference VOR Info Nearest Intersection - Identifier/Type (symbol) - VOR Frequency - Bearing/Distance to VOR Figure 5-40 Nearest Intersections Page 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 217 FLIGHT MANAGEMENT NDBS The NDB Information Page is used to view information about NDBs. In addition to displaying a map of the currently selected NDB and surrounding area, the page displays NDB information in four boxes labeled ‘NDB’, ‘INFORMATION’, ‘FREQUENCY’, and ‘NEAREST AIRPORT’. NDB Identifier/Type - Facility Name - Nearest City NDB Information - Type - Region - Lat/Long Navigation Map Showing Selected NDB NDB Frequency Nearest Airport Info Selected NDB - Identifier/Type (symbol) - Bearing/Distance to Airport Figure 5-41 NDB Information Page NOTE: Compass locator (LOM, LMM): a low power, low or medium frequency radio beacon installed in conjunction with the instrument landing system. When LOM is used, the locator is at the Outer Marker; when LMM is used, the locator is at the Middle Marker. Selecting an NDB: 1) With the NDB Information Page displayed, enter an identifier, the name of the NDB, or the city in which it’s located in the NDB Box. 2) Press the ENT Key. 3) Press the FMS Knob to remove the flashing cursor. Or: 1) With the Nearest NDB Page displayed, press the FMS Knob. 2) Press the ENT Key or turn either FMS Knob to select an identifier in the Nearest NDB Box. 3) Press the FMS Knob to remove the flashing cursor. 218 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT The Nearest NDB Page can be used to quickly find a NDB close to the flight path. In addition to displaying a map of the surrounding area, the page displays information for up to 25 nearest NDBs in three boxes labeled ‘NEAREST NDB’, ‘INFORMATION’, and ‘FREQUENCY’. A white arrow before the NDB identifier indicates the selected NDB. Up to sixteen NDBs are visible at a time. If there are more than can be shown, each list can be scrolled. The list only includes waypoints that are within 200nm. If there are no NDBs in the list, text indicating that there are no nearest NDBs is displayed. If there are no nearest NDBs in the list, the information and frequency fields are dashed. NDB Identifier/Symbol - Bearing/Distance to NDB from aircraft position Navigation Map Showing Selected NDB Nearest NDB NDB Information - Facility Name/City - Type - Lat/Long NDB Frequency Figure 5-42 Nearest NDB Page 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 219 FLIGHT MANAGEMENT VORS The VOR Information Page can be used to view information about VOR and ILS signals (since ILS signals can be received on a NAV receiver), or to quickly auto-tune a VOR or ILS frequency. Localizer information cannot be viewed on the VOR Information Page. If a VOR station is combined with a TACAN station it is listed as a VORTAC on the VOR Information Page and if it includes only DME, it is displayed as VOR-DME. In addition to displaying a map of the currently selected VOR and surrounding area, the VOR Information Page displays VOR information in four boxes labeled ‘VOR’, ‘INFORMATION’, ‘FREQUENCY’, and ‘NEAREST AIRPORT’. VOR Identifier/Type - Facility Name - Nearest City VOR Information Navigation Map Showing Selected VOR - Class/Magnetic Variation - Region - Lat/Long VOR Frequency Nearest Airport Info Selected VOR - Identifier/Type (symbol) - Bearing/Distance to Airport Figure 5-43 VOR Information Page The VOR classes used in the VOR information box are: LOW ALTITUDE, HIGH ALTITUDE, and TERMINAL. Selecting a VOR: 1) With the VOR Information Page displayed, enter an identifier, the name of the VOR, or the city in which it’s located in the VOR Box. 2) Press the ENT Key. 3) Press the FMS Knob to remove the flashing cursor. Or: 1) With the Nearest VOR Page displayed, press the FMS Knob or press the VOR Softkey. 2) Press the ENT Key or turn either FMS Knob to select an identifier in the Nearest VOR Box. 3) Press the FMS Knob to remove the flashing cursor. 220 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Or: 1) With the Nearest VOR Page displayed, press the MENU Key. 2) Highlight ‘Select VOR Window’, and press the ENT Key. 3) Press the ENT Key or turn either FMS Knob to select an identifier in the Nearest VOR Box. 4) Press the FMS Knob to remove the flashing cursor. The Nearest VOR Page can be used to quickly find a VOR station close to the aircraft. Also, a NAV frequency from a selected VOR station can be loaded from the Nearest VOR Page. In addition to displaying a map of the surrounding area, the Nearest VOR Page displays information for up to 25 nearest VOR stations in three boxes labeled ‘NEAREST VOR’, ‘INFORMATION’, and ‘FREQUENCY’. The list only includes waypoints that are within 200 nm. A white arrow before the VOR identifier indicates the selected VOR. Up to sixteen VORs are visible at a time. If there are more than can be shown, each list can be scrolled. If there are no VORs in the list, text indicating that there are no nearest VORs is displayed. If there are no nearest VORs in the list, the information is dashed. VOR Identifier/Symbol - Bearing/Distance to VOR from aircraft position Navigation Map Showing Nearest VOR VOR Information - Facility Name/City - Class/Magnetic Variation - Lat/Long Nearest VOR VOR Frequency Figure 5-44 Nearest VOR Page 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 221 FLIGHT MANAGEMENT USER WAYPOINTS The system can create and store up to 1,000 user-defined waypoints. User waypoints can be created from any map page (except PFD Inset Map, AUX-Trip Planning Page, or Procedure Pages) by selecting a position on the map using the Joystick, or from the User Waypoint Information Page by referencing a bearing/distance from an existing waypoint, bearings from two existing waypoints, or entering a latitude/longitude. Once a waypoint has been created, it can be renamed, deleted, or moved. Temporary user waypoints are erased upon system power down. User Waypoint Info - Identifier - Temporary/Normal - Waypoint Type User Wpt Comment Navigation Map Showing Selected User Waypoint Reference Wpt/Info Selected User Waypoint User Waypoint List - Identifier/Rad/Dist or - Identifiers/Radials or - Region/Lat/Long - Identifier - Comment # User Wpts Used Displayed if User Wpt was created on map page Softkeys Figure 5-45 User Waypoint Information Page Selecting a User Waypoint: 1) With the User Waypoint Information Page displayed, enter the name of the User Waypoint, or scroll to the desired waypoint in the User Waypoint List using the large FMS Knob. 2) Press the ENT Key. 3) Press the FMS Knob to remove the flashing cursor. Or: 1) With the Nearest User Waypoints Page displayed, press the FMS Knob. 2) Press the ENT Key or turn either FMS Knob to select an identifier in the Nearest USR Box. 3) Press the FMS Knob to remove the flashing cursor. 222 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Nearest User Wpt List - Identifier - Bearing/Distance from aircraft position Navigation Map Showing Selected User Waypoint User Waypoint Info Selected User Waypoint - Comment - Lat/Long Reference Wpt Info - Identifier - Radial/Distance Figure 5-46 Nearest User Waypoint Page CREATING USER WAYPOINTS User waypoints can be created from the User Waypoint Information Page in the following ways: Creating user waypoints from the User Waypoint Information Page: 1) Press the NEW Softkey, or press the MENU Key and select ‘Create New User Waypoint’. 2) Enter a user waypoint name (up to six characters). 3) Press the ENT Key. The current aircraft position is the default location of the new waypoint. 4) If desired, define the type and location of the waypoint in one of the following ways: a) Select “RAD/RAD” using the small FMS Knob, press the ENT Key, and enter the two reference waypoint identifiers and radials into the REFERENCE WAYPOINTS window using the FMS Knobs. Or: b) Select “RAD/DIS” using the small FMS Knob, press the ENT Key, and enter the reference waypoint identifier, the radial, and the distance into the REFERENCE WAYPOINTS window using the FMS Knobs. Or: c) Select “LAT/LON” using the small FMS Knob, press the ENT Key, and enter the latitude and longitude into the INFORMATION window using the FMS Knobs. 5) Press the ENT Key to accept the new waypoint. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 223 FLIGHT MANAGEMENT 6) If desired, change the storage method of the waypoint to “TEMPORARY” or “NORMAL” by moving the cursor to “TEMPORARY” and selecting the ENT Key to check or uncheck the box. 7) Press the FMS Knob to remove the flashing cursor. Or: 1) Press the FMS Knob to activate the cursor. 2) Enter a user waypoint name (up to six characters). 3) Press the ENT Key. The message ‘Are you sure you want to create the new User Waypoint AAAAAA?’ is displayed. 4) With ‘YES’ highlighted, press the ENT Key. 5) If desired, define the type and location of the waypoint in one of the following ways: a) Select “RAD/RAD” using the small FMS Knob, press the ENT Key, and enter the two reference waypoint identifiers and radials into the REFERENCE WAYPOINTS window using the FMS Knobs. Or: b) Select “RAD/DIS” using the small FMS Knob, press the ENT Key, and enter the reference waypoint identifier, the radial, and the distance into the REFERENCE WAYPOINTS window using the FMS Knobs. Or: c) Select “LAT/LON” using the small FMS Knob, press the ENT Key, and enter the latitude and longitude into the INFORMATION window using the FMS Knobs. 6) Press the ENT Key to accept the new waypoint. 7) If desired, change the storage method of the waypoint to “TEMPORARY” or “NORMAL” by moving the cursor to “TEMPORARY” and selecting the ENT Key to check or uncheck the box. 8) Press the FMS Knob to remove the flashing cursor. Figure 5-47 User Waypoint Information Page Menu 224 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Creating user waypoints from map pages: 1) Press the Joystick to activate the panning function and pan to the map location of the desired user waypoint. 2) Press the ENT Key. The User Waypoint Information Page is displayed with the captured position. NOTE: If the pointer has highlighted a map database feature, one of three things happens upon pressing the ENT Key: 1) information about the selected feature is displayed instead of initiating a new waypoint, 2) a menu pops up allowing a choice between ‘Review Airspaces’ or ‘Create User Waypoint’, or 3) a new waypoint is initiated with the default name being the selected map item. 3) Enter a user waypoint name (up to six characters). 4) Press the ENT Key to accept the selected name. 5) If desired, define the type and location of the waypoint in one of the following ways: a) Select “RAD/RAD” using the small FMS Knob, press the ENT Key, and enter the two reference waypoint identifiers and radials into the REFERENCE WAYPOINTS window using the FMS Knobs. Or: b) Select “RAD/DIS” using the small FMS Knob, press the ENT Key, and enter the reference waypoint identifier, the radial, and the distance into the REFERENCE WAYPOINTS window using the FMS Knobs. Or: c) Select “LAT/LON” using the small FMS Knob, press the ENT Key, and enter the latitude and longitude into the INFORMATION window using the FMS Knobs. 6) Press the ENT Key to accept the new waypoint. 7) If desired, change the storage method of the waypoint to “TEMPORARY” or “NORMAL” by moving the cursor to “TEMPORARY” and selecting the ENT Key to check or uncheck the box. 8) Press the FMS Knob to remove the flashing cursor. 9) Press the GO BACK Softkey to return to the map page. EDITING USER WAYPOINTS Editing a user waypoint comment or location: 1) With the User Waypoint Information Page displayed, press the FMS Knob to activate the cursor. 2) Select a user waypoint in the User Waypoint List, if required, and press the ENT Key. 3) Move the cursor to the desired field. 4) Turn the small FMS Knob to make any changes. 5) Press the ENT Key to accept the changes. 6) Press the FMS Knob to remove the flashing cursor. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 225 FLIGHT MANAGEMENT Renaming user waypoints: 1) Highlight a user waypoint in the User Waypoint List. Select the RENAME Softkey, or press the MENU Key and select ‘Rename User Waypoint’. 2) Enter a new name. 3) Press the ENT Key. The message ‘Do you want to rename the user waypoint AAAAAA to BBBBBB?’ is displayed. 4) With ‘YES’ highlighted, press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor. Changing the location of an existing waypoint to the aircraft present position: 1) Enter a waypoint name or select the waypoint in the User Waypoint List, then press the ENT Key. 2) Press the MENU Key. 3) Select ‘Use Present Position’. 4) Press the ENT Key twice. The new waypoint’s location is saved. 5) Press the FMS Knob to remove the flashing cursor. A system generated comment for a user waypoint incorporates the reference waypoint identifier, bearing, and distance. If a system generated comment has been edited, a new comment can be generated. Resetting the comment field to the system generated comment: 1) Enter a waypoint name or select the waypoint in the User Waypoint List, then press the ENT Key. 2) Press the MENU Key. 3) Select ‘Auto Comment’. 4) Press the ENT Key. The generated comment is based on the reference point used to define the waypoint. The default type of user waypoint (normal or temporary) can be changed using the user waypoint information page menu. Temporary user waypoints are automatically deleted upon the next power cycle. Changing the user waypoint storage duration default setting: 1) With the User Waypoint Information Page displayed, press the MENU Key. 2) Move the cursor to select ‘Waypoint Setup’, and press the ENT Key. 3) Select ‘NORMAL’ or ‘TEMPORARY’ as desired, and press the ENT Key. 4) Press the FMS Knob to remove the flashing cursor and return to the User Waypoint Information Page. 226 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT DELETING USER WAYPOINTS Deleting a single user waypoint: 1) Highlight a User Waypoint in the User Waypoint List, or enter a waypoint in the User Waypoint field. 2) Press the DELETE Softkey or press the CLR Key. ‘Yes’ is highlighted in the confirmation window. 3) Press the ENT Key. 4) Press the FMS Knob to remove the flashing cursor. Or: 1) Highlight a User Waypoint in the User Waypoint List, or enter a waypoint in the User Waypoint field. 2) Press the MENU Key. 3) Select ‘Delete User Waypoint’. 4) Press the ENT Key twice to confirm the selection. 5) Press the FMS Knob to remove the flashing cursor. NOTE: The option to ‘Delete All User Waypoints’ is not available while the aircraft is in flight. Deleting all user waypoints: 1) Highlight a User Waypoint in the User Waypoint List. 2) Press the MENU Key. 3) Select ‘Delete All User Waypoints’. 4) Press the ENT Key twice to confirm the selection. 5) Press the FMS Knob to remove the flashing cursor. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 227 FLIGHT MANAGEMENT 5.4 AIRSPACES The system can display the following types of airspaces: Class B/TMA, Class C/TCA, Class D, Restricted, MOA (Military), Other Airspace, Air Defense Identification Zone (ADIZ), and Temporary Flight Restriction (TFR). Class D Airspace MOA (Military) Class B Airspace Restricted Area Alert Area Class C Airspace ADIZ Warning Area Figure 5-48 Airspaces The Nearest Airspaces Page, Airspace Alerts Window, and Airspace Alerts on the PFD provide additional information about airspaces and the location of the aircraft in relationship to them. 228 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT The Airspace Alerts Box allows the pilot to turn the controlled/special-use airspace message alerts on or off. This does not affect the alerts listed on the Nearest Airspaces Page or the airspace boundaries depicted on the Navigation Map Page. It simply turns on/off the warning provided when the aircraft is approaching or near an airspace. An altitude buffer is also provided which “expands” the vertical range above or below an airspace. For example, if the buffer is set at 500 feet, and the aircraft is more than 500 feet above/below an airspace, an alert message is not generated, but if the aircraft is less than 500 feet above/below an airspace and projected to enter it, the pilot is notified with an alert message. The default setting for the altitude buffer is 200 feet. Changing the altitude buffer distance setting: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the altitude buffer field in the Airspace Alerts Box. 4) Use the FMS Knob to enter an altitude buffer value and press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor. Turning an airspace alert on or off: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the desired field in the Airspace Alerts Box. 4) Turn the small FMS Knob clockwise to turn the airspace alert ON or counterclockwise to turn the alert OFF. 5) Press the FMS Knob to remove the flashing cursor. Airspace Alerts Box - Airspace Altitude Buffer - Alert On/Off (Default Settings Shown) DFLTS Softkey Figure 5-49 System Setup Page - Airspace Alerts 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 229 FLIGHT MANAGEMENT Map ranges for the airspace boundaries are selected from the Aviation Group in the Map Setup Menu. See Table 5-2 for the default and maximum ranges for each type of airspace and the symbol used to define the airspace area. The Nearest Airspaces Page can be used to quickly find airspaces close to the flight path. In addition, a selected frequency associated with the airspace can be loaded from the Nearest Airspaces Page. In addition to displaying a map of airspace boundaries and surrounding area, the Nearest Airspaces Page displays airspace information in four boxes labeled ‘AIRSPACE ALERTS’, ‘AIRSPACE, AGENCY’, ‘VERTICAL LIMITS’, and ‘FREQUENCIES’. Airspace Alerts Info - Name - Proximity (Ahead, Inside, Ahead < 2nm, Within 2nm) - Time till Intercept (only if Ahead or Ahead < 2nm) Airspace/Agency Info - Airspace Type - Controlling Agency Airspace Vertical Limits Airspace 1 - Ceiling - Floor Associated Frequencies - Type - Availability/Info - Frequency Softkeys Figure 5-50 Nearest Airspaces Page Airspace alerts and associated frequencies are shown in scrollable lists on the Nearest Airspaces Page. The ALERTS and FREQ softkeys place the cursor in the respective list. The FREQ Softkey is enabled only if one or more frequencies exist for a selected airspace. Selecting and viewing an airspace alert with its associated information: 1) Select the Nearest Airspaces Page. 2) Select the ALERTS Softkey; or press the FMS Knob; or press the MENU Key, highlight ‘Select Alerts Window’, and press the ENT Key. The cursor is placed in the ‘AIRSPACE ALERTS’ Box. 3) Select the desired airspace. 4) Press the FMS Knob to remove the flashing cursor. 230 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Pressing the PFD MSG Softkey displays the message window on the PFD. The following airspace alerts are displayed in the message window: Message INSIDE ARSPC – Inside airspace. ARSPC AHEAD – Airspace ahead – less than 10 minutes. ARSPC NEAR – Airspace near and ahead. ARSPC NEAR – Airspace near – less than 2 nm. Comments The aircraft is inside the airspace. Special use airspace is ahead of aircraft. The aircraft penetrates the airspace within 10 minutes. Special use airspace is near and ahead of the aircraft position. Special use airspace is within 2 nm of the aircraft position. Table 5-6 PFD Airspace Alert Messages 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 231 FLIGHT MANAGEMENT 5.5 DIRECT-TO-NAVIGATION The Direct-to method of navigation, initiated by pressing the Direct-to Key on either the MFD or PFD, is quicker to use than a flight plan when the desire is to navigate to a single point such as a nearby airport. Once a direct-to is activated, the system establishes a point-to-point course line from the present position to the selected direct-to destination. Course guidance is provided until the direct-to is replaced with a new direct-to or flight plan, or cancelled. A vertical navigation (VNV) direct-to creates a descent path (and provides guidance to stay on the path) from the current altitude to a selected altitude at the direct-to waypoint. Vertical navigation is based on barometric altitudes, not on GPS altitude, and is used for cruise and descent phases of flight. The Direct-to Window allows selection and activation of direct-to navigation. The Direct-to Window displays selected direct-to waypoint data on the PFD and the MFD. Direct-to Point Info - Identifier/Symbol/Region - Facility Name - City VNV Constraints - Altitude at Arrival - Along Track Offset Map of Selected Point Location of Destination Desired Course - Bearing/Distance Figure 5-51 Direct-to Window - MFD 232 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Direct-to Point Info - Identifier/Symbol/City - Facility Name VNV Constraints - Altitude at Arrival - Along Track Offset Direct-to Point Info - Bearing/Distance - Desired Course Activation Command Figure 5-52 Direct-to Window - PFD Any waypoint can be entered as a direct-to destination from the Direct-to Window. Entering a waypoint identifier, facility name, or city as a direct-to destination: 1) Press the Direct-to Key. The Direct-to Window is displayed (with the active flight plan waypoint as the default selection or a blank waypoint field if no flight plan is active). 2) Turn the small FMS Knob clockwise to begin entering a waypoint identifier (turning it counter-clockwise brings up the waypoint selection submenu - press the CLR Key to remove it), or turn the large FMS Knob to select the facility name, or city field and turn the small FMS Knob to begin entering a facility name or city. If duplicate entries exist for the entered facility or city name, additional entries can be viewed by turning the small FMS Knob during the selection process. 3) Press the ENT Key. The ‘Activate?’ field is highlighted. 4) Press the ENT Key to activate the direct-to. Any waypoint contained in the active flight plan can be selected as a direct-to waypoint from the Direct-to Window, the Active Flight Plan Page, or the Active Flight Plan Window. Waypoint Submenu - Flight Plan Waypoints - Nearest Airports - Recent Waypoints - User Waypoints - Airway Waypoints (only available when active leg is part of an airway) Figure 5-53 Waypoint Submenu 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 233 FLIGHT MANAGEMENT Selecting an active flight plan waypoint as a direct-to destination: 1) While navigating an active flight plan, press the Direct-to Key. The Direct-to Window is displayed with the active flight plan waypoint as the default selection. 2) Turn the small FMS Knob counter-clockwise to display a list of flight plan waypoints (the FPL list is populated only when navigating a flight plan). 3) Select the desired waypoint. 4) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 5) Press the ENT Key again to activate the direct-to. Or: 1) Select the Active Flight Plan Page on the MFD, or the Active Flight Plan Window on the PFD. 2) Select the desired waypoint. 3) Press the Direct-to Key. 4) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 5) Press the ENT Key again to activate the direct-to. Any NRST, RECENT, USER, or AIRWAY waypoint can be selected as a direct-to destination in the Direct-to Window. Selecting a NRST, RECENT, USER, or AIRWAY waypoint as a direct-to destination: 1) Press the Direct-to Key. The Direct-to Window is displayed (with the active flight plan destination as the default selection or a blank destination if no flight plan is active). 2) Turn the small FMS Knob counter-clockwise to display a list of flight plan waypoints (the FPL list is populated only when navigating a flight plan). 3) Turn the small FMS Knob clockwise to display the NRST, RECENT, USER, or AIRWAY waypoints. 4) Turn the large FMS Knob clockwise to select the desired waypoint. 5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 6) Press the ENT Key again to activate the direct-to. The Direct-to Window can be displayed from any page and allows selection and activation of direct-to navigation. If the direct-to is initiated from any page except the WPT pages, the default waypoint is the active flight plan waypoint (if a flight plan is active) or a blank waypoint field. Direct-to requests on any WPT page defaults to the displayed waypoint. Selecting any waypoint as a direct-to destination: 1) Select the page or window containing the desired waypoint type and select the desired waypoint. 2) Press the Direct-to Key to display the Direct-to Window with the selected waypoint as the direct-to destination. 3) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 4) Press the ENT Key again to activate the direct-to. 234 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Selecting a nearby airport as a direct-to destination: 1) Press the NRST Softkey on the PFD; or turn the FMS Knob to display the Nearest Airports Page and press the FMS Knob. 2) Select the desired airport (the nearest one is already selected). 3) Press the Direct-to Key. 4) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 5) Press the ENT Key again to activate the direct-to. Direct-to destinations may also be selected by using the pointer on the navigation map pages. If no airport, NAVAID, or user waypoint exists at the desired location, a temporary waypoint named ‘MAPWPT’ is automatically created at the location of the map arrow. Selecting a waypoint as a direct-to destination using the pointer: 1) From a navigation map page, press the Joystick to display the pointer. 2) Move the Joystick to place the pointer at the desired destination location. 3) If the pointer is placed on an existing airport, NAVAID, or user waypoint, the waypoint name is highlighted. 4) Press the Direct-to Key to display the Direct-to Window with the selected point entered as the direct-to destination. 5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 6) Press the ENT Key again to activate the direct-to. Cancelling a Direct-to: 1) Press the Direct-to Key to display the Direct-to Window. 2) Press the MENU Key. 3) With ‘Cancel Direct-To NAV’ highlighted, press the ENT Key. If a flight plan is still active, the system resumes navigating the flight plan along the closest leg. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 235 FLIGHT MANAGEMENT Page Menu - Cancel Direct-To Navigation Figure 5-54 Direct-to Window - Cancelling Direct-to Navigation When navigating a direct-to, the system sets a direct great circle course to the selected destination. The course to a destination can also be manually selected using the course field (‘COURSE’) on the Direct-to Window. Selecting a manual direct-to course: 1) Press the Direct-to Key. The Direct-to Window is displayed with the destination field highlighted. 2) Highlight the course field. 3) Enter the desired course. 4) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 5) Press the ENT Key again to activate the direct-to. Reselecting the direct course from the current position: 1) Press the Direct-to Key. The Direct-to Window is displayed with the destination field highlighted. 2) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 3) Press the ENT Key again to activate the direct-to. A direct-to with altitude constraints creates a descent path (and provides guidance to stay on the path) from the aircraft’s current altitude to the altitude of the direct-to waypoint. The altitude is reached at the waypoint, or at the specified distance along the flight path if an offset distance has been entered. All VNV altitudes prior to the direct-to destination are removed from the active flight plan upon successful activation of the direct-to. All VNV altitudes following the direct-to waypoint are retained. See the section on Vertical Navigation for more information regarding the use and purpose of VNV altitudes and offset distances. 236 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Entering a VNV altitude and along-track offset for the waypoint: 1) Press the Direct-to Key to display the Direct-to Window. 2) Turn the large FMS Knob to place the cursor over the ‘VNV’ altitude field. 3) Enter the desired altitude. 4) Press the ENT Key. The option to select MSL or AGL is now displayed. 5) Turn the small FMS Knob to select ‘MSL’ or ‘AGL’. 6) Press the ENT Key. The cursor is now flashing in the VNV offset distance field. 7) Enter the desired along-track distance before the waypoint. 8) Press the ENT Key. The ‘Activate?’ field is highlighted. 9) Press the ENT Key to activate. Removing a VNV altitude constraint: 1) Press the Direct-to Key to display the Direct-to Window. 2) Press the MENU Key. 3) With ‘Clear Vertical Constraints’ highlighted, press the ENT Key. Page Menu - Clear Vertical Navigation Constraints Figure 5-55 Direct-to Window - Clearing Vertical Constraints 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 237 FLIGHT MANAGEMENT 5.6 FLIGHT PLANNING Flight planning consists of building a flight plan by entering waypoints one at a time, adding waypoints along airways, and inserting departures, airways, arrivals, or approaches as needed. The system allows flight planning information to be entered from either the MFD or PFD. The flight plan is displayed on maps using different line widths, colors, and types, based on the type of leg and the segment of the flight plan currently being flown (departure, enroute, arrival, approach, or missed approach). Flight Plan Leg Type Symbol Active Course Leg Active Heading Leg Course Leg in the current flight segment Course Leg not in the current flight segment Heading Leg Turn Anticipation Arc Table 5-7 Flight Plan Leg Symbols Up to 99 flight plans with up to 99 waypoints each can be created and stored in memory. One flight plan can be activated at a time and becomes the active flight plan. The active flight plan is erased when the system is turned off and overwritten when another flight plan is activated. When storing flight plans with an approach, departure, or arrival, the system uses the waypoint information from the current database to define the waypoints. If the database is changed or updated, the system automatically updates the information if the procedure has not been modified. If an approach, departure, or arrival procedure is no longer available, the procedure is deleted from the affected stored flight plan(s), and an alert is displayed (see Miscellaneous Messages in Appendix A) advising that one or more stored flight plans need to be edited. Whenever an approach, departure, or arrival procedure is loaded into the active flight plan, a set of approach, departure, or arrival waypoints is inserted into the flight plan along with a header line describing the instrument procedure the pilot selected. The original enroute portion of the flight plan remains active (unless an instrument procedure is activated) when the procedure is loaded. 238 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT When the database is updated, the airways need to be reloaded also. Each airway segment is reloaded from the database given the entry waypoint, the airway identifier and the exit waypoint. This reloads the sequence of waypoints between the entry and exit waypoints (the sequence may change when the database is updated). The update of an airway can fail during this process. If that happens, the airway waypoints are changed to regular (non-airway) flight plan waypoints, and an alert is displayed (see Miscellaneous Messages in Appendix A). The following could cause the airway update to fail: • Airway identifier, entry waypoint or exit waypoint not found in the new database. • Airway entry/exit waypoint is not an acceptable waypoint for the airway – either the waypoint is no longer on the airway, or there is a new directional restriction that prevents it being used. • Loading the new airway sequence would exceed the capacity of the flight plan. FLIGHT PLAN CREATION There are three methods to create or modify a flight plan: • Active Flight Plan Page on the MFD (create/modify the active flight plan) • Active Flight Plan Window on the PFD (create/modify the active flight plan) • Flight Plan Catalog Page on the MFD (create/modify a stored flight plan) Active FPL Waypoint List - Comment - Procedure Header - Waypoint Identifier - Airway Identifier - Desired Track to Waypoint - Distance to Waypoint - Waypoint Altitude Constraint Active Flight Plan Leg Vertical Navigation Profile - Active Vertical WPT Alt/ID - Vertical Speed Target - Flight Path Angle - Vertical Speed Target - Time to Top of Descent - Vertical Deviation Turn Anticipation Arc Non-Active, Flight Plan Leg Figure 5-56 Active Flight Plan Page 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 239 FLIGHT MANAGEMENT Active Flight Plan Comment Active Flight Plan Leg Active Flight Plan Waypoint List - Waypoint ID - Desired Track to Waypoint - Distance to Waypoint - Airway Identifier Figure 5-57 Active Flight Plan Window on PFD Catalog Contents - # Used - # Empty Flight Plan List - Comment Selected Flight Plan Map Selected FPL Info - Departure Waypoint - Destination Waypoint - Total Flight Plan Distance - Enroute Safe Altitude Softkeys Figure 5-58 Flight Plan Catalog Page 240 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT The active flight plan is listed on the active Flight Plan Page on the MFD, and in the Active Flight Plan Window on the PFD. It is the flight plan to which the system is currently providing guidance, and is shown on the navigation maps. Stored flight plans are listed on the Flight Plan Catalog Page, and are available for activation (becomes the active flight plan). NOTE: The system supports AFCS lateral guidance for all leg types (using NAV or FMS APPR mode). The system does not support course deviation for any heading leg types (VA, VD, VI, VM, or VR). Creating an active flight plan: 1) Press the FPL Key. 2) Press the FMS Knob to activate the cursor (only on MFD). 3) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway waypoints). 4) Enter the identifier, facility, or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key. The active flight plan is modified as each waypoint is entered. 5) Repeat step numbers 3 and 4 to enter each additional flight plan waypoint. 6) When all waypoints have been entered, press the FMS Knob to remove the cursor. Creating a stored flight plan: 1) Press the FPL Key. 2) Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page. 3) Select the NEW Softkey; or press the MENU Key, highlight ‘Create New Flight Plan’, and press the ENT Key to display a blank flight plan for the first empty storage location. 4) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway waypoints). 5) Enter the identifier, facility, or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key. 6) Repeat step numbers 4 and 5 to enter each additional flight plan waypoint. 7) When all waypoints have been entered, press the FMS Knob to return to the Flight Plan Catalog Page. The new flight plan is now in the list. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 241 FLIGHT MANAGEMENT Flight plans can be imported from an SD Card or exported to an SD Card from the Stored Flight Plan Page. Importing a Flight Plan from an SD Card 1) Insert the SD card containing the flight plan in the top card slot on the MFD. 2) Press the FPL Key to display the Active Flight Plan Page on the MFD. 3) Turn the small FMS Knob to select the Flight Plan Catalog Page. 4) Press the FMS Knob to activate the cursor. 5) Turn either FMS Knob to highlight an empty or existing flight plan. 6) Press the IMPORT Softkey; or press the MENU Key, select “Import Flight Plan”, and press the ENT Key. If an empty slot is selected, a list of the available flight plans on the SD card will be displayed. Or: If an existing flight plan is selected, an “Overwrite existing flight plan? OK or CANCEL” prompt is displayed. Press the ENT Key to choose to overwrite the selected flight plan and see the list of available flight plans on the SD card. If overwriting the existing flight plan is not desired, select “CANCEL” using the FMS Knob, press the ENT Key, select another flight plan slot, and press the IMPORT Softkey again. 7) Turn the small FMS Knob to highlight the desired flight plan for importing. 8) Press the ENT Key to initiate the import. 9) Press the ENT Key again to confirm the import. Import/Export Softkeys List of Flight Plans to Import & Details for the Selected File Import Successful Figure 5-59 Flight Plan Import 242 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT NOTE: If the imported flight plan contains a waypoint with a name that duplicates the name of a waypoint already stored on the system, the system compares the coordinates of the imported waypoint with those of the existing waypoint. If the coordinates are different, the imported waypoint is automatically renamed by adding characters to the end of the name. Exporting a Flight Plan to an SD Card 1) Insert the SD card into the top card slot on the MFD. 2) Press the FPL Key to display the Active Flight Plan Page on the MFD. 3) Turn the small FMS Knob to select the Flight Plan Catalog Page. 4) Press the FMS Knob to activate the cursor. 5) Turn the large FMS Knob to highlight the flight plan to be exported. 6) Press the EXPORT Softkey; or press the MENU Key, select “Export Flight Plan”. 7) If desired, change the name for the exported file by turning the large FMS Knob to the left to highlight the name, then use the small and large FMS knobs to enter the new name, and press the ENT Key. 8) Press the ENT Key to initiate the export. 9) Press the ENT Key to confirm the export. NOTE: The exported flight plan will not contain any procedures or airways. Import/Export Softkeys Stored Flight Plan to be Exported & Exported Flight Plan Name Export Successful Figure 5-60 Flight Plan Export 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 243 FLIGHT MANAGEMENT ADDING WAYPOINTS TO AN EXISTING FLIGHT PLAN Waypoints can be added to the active flight plan or any stored flight plan. Choose the flight plan, select the desired point of insertion, enter the waypoint, and it is added in front of the selected waypoint. Flight plans are limited to 99 waypoints (including waypoints within airways and procedures). If the number of waypoints in the flight plan exceeds 99, the message “Flight plan is full. Remove unnecessary waypoints.” appears and the new waypoint(s) are not added to the flight plan. Stored Flight Plan Selected - Memory Slot - Comment - Procedure Identifier - Waypoint Identifier - Airway Identifier - Desired Track to Waypoint - Distance to Waypoint - Waypoint Altitude Constraint Softkeys Figure 5-61 Stored Flight Plan Page Flight Plan Full Message Figure 5-62 Active Flight Plan Page - FPL Full 244 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Adding a waypoint to a stored flight plan: 1) On the Flight Plan Catalog Page, press the FMS Knob to activate the cursor. 2) Highlight the desired flight plan. 3) Select the EDIT Softkey; or press the ENT Key, turn the large FMS Knob clockwise to select “EDIT” and press the ENT Key. The Stored Flight Plan Page is displayed. 4) Select the point in the flight plan to add the new waypoint. The new waypoint is placed directly in front of the highlighted waypoint. 5) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway waypoints). 6) Enter the identifier, facility, or city name of the waypoint; or select a waypoint from the submenu of waypoints and press the ENT Key. The new waypoint now exists in the flight plan. NOTE: If the identifier entered in the Waypoint Information Window has duplicates, a Duplicate Waypoint Window is displayed. Use the FMS Knob to select the correct waypoint. Figure 5-63 Duplicate Waypoints Window Adding a waypoint to the active flight plan: 1) Press the FPL Key. 2) Press the FMS Knob to activate the cursor (not required on the PFD). 3) Select the point in the flight plan before which to add the new waypoint. The new waypoint is placed directly in front of the highlighted waypoint. 4) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway waypoints). 5) Enter the identifier, facility, or city name of the waypoint or select a waypoint from the submenu of waypoints and press the ENT Key. The active flight plan is modified as each waypoint is entered. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 245 FLIGHT MANAGEMENT Creating and adding user waypoints to the active flight plan: 1) Press the Joystick to activate the panning function on the Active Flight Plan Page and pan to the map location of the desired user waypoint. 2) Select the LD WPT Softkey; or press the MENU Key, select ‘Load Waypoint’, and press the ENT Key. The user waypoint is created with a name of USRxxx (using the next available in sequence) and is added to the end of the active flight plan. ADDING AIRWAYS TO A FLIGHT PLAN Airways can be added to the active flight plan or any stored flight plan. Choose a flight plan (add the desired airway entry point if not already in the flight plan), select the waypoint after the desired airway entry point, select the airway, and it is added in front of the selected waypoint. An airway can only be loaded if there is a waypoint in the flight plan that is part of the desired airway and is not part of an arrival or approach procedure. The system also anticipates the desired airway and exit point based on loaded flight plan waypoints. Airway Entry Waypoint Selected Airway Airways Available at TOP Airway Waypoint Sequence Preview of Selected Airway Figure 5-64 Select Airway Page - Selecting Airway Adding an airway to a flight plan: 1) Press the FPL Key. 2) Press the FMS Knob to activate the cursor (not required on the PFD). 3) Turn the large FMS Knob to highlight the waypoint after the desired airway entry point. If this waypoint is not a valid airway entry point, a valid entry point should be entered at this time. 246 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT 4) Turn the small FMS Knob one click clockwise and select the LD AIRWY Softkey, or press the MENU Key and select “Load Airway”. The Select Airway Page is displayed. The LD AIRWY Softkey or the “Load Airway” menu item is available only when a valid airway entry waypoint has been chosen (the waypoint ahead of the cursor position). 5) Turn the FMS Knob to select the desired airway from the list, and press the ENT Key. Low altitude airways are shown first in the list, followed by “all” altitude airways, and then high altitude airways. 6) Turn the FMS Knob to select the desired airway exit point from the list, and press the ENT Key. ‘LOAD?’ is highlighted. 7) Press the ENT Key. The system returns to editing the flight plan with the new airway inserted. Airway Entry Waypoint Selected Airway Selected Exit Point Preview of Selected Airway Selected Airway Exit Point Airway Exit Points Available Figure 5-65 Select Airway Page - Selecting Exit Point 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 247 FLIGHT MANAGEMENT Inserted Airway Header - Airway Identifier: [airway identifier].[exit waypoint identifier] (e.g., V4.SLN) Figure 5-66 Active Flight Plan Page - Airway Inserted RESTRICTIONS ON ADDING AIRWAYS Some airways have directional restrictions on all or part of the route. Airway “A2” in Europe has a directional restriction over the whole route such that it can be flown only in the direction MTD-ABB-BNE-DEVAL. Airway “UR975” in North Africa has more complicated directional restrictions within the list of airway waypoints AMANO, VAKOR, LIBRO, NELDA, DIRKA, GZO, KOSET, and SARKI: • Starting from AMANO, the airway can be flown only to LIBRO. • Starting from SARKI, the airway can be flown only to LIBRO. • Between NELDA and GZO, the airway can be flown in either direction. In the US, airways that are “one-way” for specified hours of operation are not uncommon. These airways are always bidirectional in the database. The system only allows correct airway sequences to be inserted. If the pilot subsequently inverts the flight plan, the system inverts the airway waypoint sequence and removes the airway header. 248 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT ADDING PROCEDURES TO A STORED FLIGHT PLAN The system allows the pilot to insert pre-defined instrument procedures from the navigation database into a flight plan. The procedures are designed to facilitate routing of traffic leaving an airport (departure), arriving at an airport (arrival), and landing at an airport (approach). See the procedures section for more details. Flight Plan Name Flight Plan Waypoint List Softkeys Load Departure Load Arrival Load Approach Activate Flight Plan Figure 5-67 Stored Flight Plan Page 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 249 FLIGHT MANAGEMENT DEPARTURE (DP) A Departure Procedure (DP) is loaded at the departure airport in the flight plan. Only one departure can be loaded at a time in a flight plan. The route is defined by selection of a departure, the transition waypoints, and a runway. Departure Airport Selected Departure Departures Available at KMKC Preview of Selected Departure Departure Waypoint Sequence Figure 5-68 Departure Loading Page - Selecting the Departure Loading a departure procedure into a stored flight plan: 1) Select a stored flight plan from the Flight Plan Catalog Page. 2) Select the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’, and press the ENT Key. The Stored Flight Plan Page is displayed. 3) Select the LD DP Softkey; or press the MENU Key, select “Load Departure”, and press the ENT Key. The Departure Loading Page is displayed. 4) Select a departure. Press the ENT Key. 5) Select a runway served by the selected departure, if required. Press the ENT Key. 6) Select a transition for the selected departure. Press the ENT Key. 7) Press the ENT Key to load the selected departure procedure. 250 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Departure Airport Selected Departure Selected Runway Selected Departure End Point Selected Transition Departure Transition Points Available Preview of Selected Departure Figure 5-69 Departure Loading Page - Selecting Transition Inserted Departure Header - Departure Identifier: [departure airport]-[departure runway]. [departure transition]. [departure end point] (e.g., KMKC-ALL.TIFTO2.TIFTO) Figure 5-70 Stored Flight Plan Page - Departure Inserted 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 251 FLIGHT MANAGEMENT ARRIVAL (STAR) A Standard Terminal Arrival (STAR) is loaded at the destination airport in the flight plan. Only one arrival can be loaded at a time in a flight plan. The route is defined by selection of an arrival, the transition waypoints, and a runway. Destination Airport Selected Arrival Arrivals Available at KCOS Selected Runway Arrival Waypoint Sequence Preview of Selected Arrival Figure 5-71 Arrival Loading Page - Selecting the Arrival Loading an arrival procedure into a stored flight plan: 1) Select a stored flight plan from the Flight Plan Catalog Page. 2) Select the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’, and press the ENT Key. The Stored Flight Plan Page is displayed. 3) Select the LD STAR Softkey; or press the MENU Key, select “Load Arrival”, and press the ENT Key. The Arrival Loading Page is displayed. 4) Select an arrival. Press the ENT Key. 5) Select a transition for the selected arrival. Press the ENT Key. 6) Select a runway served by the selected arrival, if required. Press the ENT Key. 7) Press the ENT Key to load the selected arrival procedure. 252 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Destination Airport Selected Arrival Selected Transition Transitions Available with DBRY1 Arrival Waypoint Sequence Preview of Selected Arrival Figure 5-72 Arrival Loading Page - Selecting the Transition Inserted Arrival Header - Arrival Identifier: [arrival airport]-[arrival transition]. [arrival].[arrival runway] (e.g., KCOS-TBE.DBRY1.ALL) Figure 5-73 Stored Flight Plan Page - Arrival Inserted 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 253 FLIGHT MANAGEMENT APPROACH (APPR) An Approach Procedure (APPR) can be loaded at any airport that has an approach available. Only one approach can be loaded at a time in a flight plan. The route for a selected approach is defined by designating transition waypoints. Destination Airport Selected Approach Approaches Available at KCOS Preview of Selected Approach Approach Waypoint Sequence Figure 5-74 Approach Loading Page - Selecting the Approach Loading an approach procedure into a stored flight plan: 1) Select a stored flight plan from the Flight Plan Catalog Page. 2) Select the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’, and press the ENT Key. The Stored Flight Plan Page is displayed. 3) Select the LD APR Softkey; or press the MENU Key, select “Load Approach”, and press the ENT Key. The Approach Loading Page is displayed. 4) Select the airport and approach: a) Use the FMS Knob to select an airport and press the ENT Key. b) Select an approach from the list and press the ENT Key. Or: a) If necessary, push the FMS Knob to exit the approach list, and use the large FMS Knob to move the cursor to the APPROACH CHANNEL field. b) Use the FMS Knob to enter the approach channel number, and press the ENT Key to accept the approach channel number. The airport and approach are selected. 254 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT 5) Select a transition for the selected approach. Press the ENT Key. 6) Press the ENT Key to load the selected approach procedure. Destination Airport Selected Approach Selected Transition Transitions Available with Selected Approach Barometric Minimum Approach Waypoint Sequence Preview of Selected Approach Load Approach? Figure 5-75 Approach Loading Page - Selecting the Transition Inserted Approach Header - Approach Identifier: [approach airport].[runway and approach type] Figure 5-76 Stored Flight Plan Page - Approach Inserted 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 255 FLIGHT MANAGEMENT FLIGHT PLAN STORAGE The system can store up to 99 flight plans, numbered 1 through 99. The active flight plan is erased when the system is powered off or when another flight plan is activated. Details about each stored flight plan can be viewed on the Flight Plan Catalog Page and on the Stored Flight Plan Page. Viewing information about a stored flight plan: 1) Press the FPL Key on the MFD to display the Active Flight Plan Page. 2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the desired flight plan. 4) The Flight Plan Information is displayed showing departure, destination, total distance, and enroute safe altitude information for the selected Flight Plan. 5) Select the EDIT Softkey to open the Stored Flight Plan Page and view the waypoints in the flight plan. 6) Press the FMS Knob to exit the Stored Flight Plan Page. Flight Plan Name (Comment) Selected Flight Plan Preview of Selected Flight Plan Stored Flight Plan Info - Departure Airport - Destination Airport - Total Flight Plan Distance - Enroute Safe Altitude Stored FPL Editing Softkeys Figure 5-77 Stored Flight Plan Information Storing an active flight plan from the Active Flight Plan Page or the Active Flight Plan Window: 1) Press the MENU Key. 2) Highlight ‘Store Flight Plan’. 3) Press the ENT Key. 4) With ‘OK’ highlighted, press the ENT Key. The flight plan is stored in the next available position in the flight plan list on the Flight Plan Catalog Page. 256 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT ACTIVATE A FLIGHT PLAN Activating a stored flight plan erases the active flight plan and replaces it with the flight plan being activated. Inverting a stored flight plan reverses the waypoint order, erases the active flight plan, and replaces it with the flight plan being activated (the stored flight plan is not changed). Activating a stored flight plan on the MFD: 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan. 3) Select the ACTIVE Softkey; or press the ENT Key twice; or press the MENU Key, highlight ‘Activate Flight Plan’, and press the ENT Key. The ‘Activate Stored Flight Plan?’ window is displayed. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. Inverting and activating a stored flight plan on the MFD: 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan. 3) Select the INVERT Softkey; or press the MENU Key, highlight ‘Invert & Activate FPL?’, and press the ENT Key. The ‘Invert and activate stored flight plan?’ window is displayed. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. COPY A FLIGHT PLAN The system allows copying a flight plan into a new flight plan memory slot, allowing editing, etc., without affecting the original flight plan. This can be used to duplicate an existing stored flight plan for use in creating a modified version of the original stored flight plan. Copying a stored flight plan on the MFD: 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan. 3) Select the COPY Softkey; or press the MENU Key, highlight ‘Copy Flight Plan’, and press the ENT Key. The ‘Copy to Flight Plan XX?’ window is displayed. 4) With ‘OK’ highlighted, press the ENT Key to copy the flight plan. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. DELETE A STORED FLIGHT PLAN Individual or all stored flight plans can be deleted from memory. Deleting a stored flight plan: 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 257 FLIGHT MANAGEMENT 3) Select the DELETE Softkey; press the CLR Key; or press the MENU Key, highlight ‘Delete Flight Plan’, and press the ENT Key. The ‘Delete Flight Plan XX?’ window is displayed. 4) With ‘OK’ highlighted, press the ENT Key to delete the flight plan. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. NOTE: The option to delete all stored flight plans is not available while the aircraft is in flight. Deleting all stored flight plans: 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the MENU Key. 3) Highlight ‘Delete All’ and press the ENT Key. A ‘Delete all flight plans?’ confirmation window is displayed. 4) With ‘OK’ highlighted, press the ENT Key to delete all flight plans. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. FLIGHT PLAN EDITING The active flight plan or any stored flight plan can be edited. The edits made to the active flight plan affect navigation as soon as they are entered. DELETING THE ACTIVE FLIGHT PLAN The system allows deleting an active flight plan. Deleting the active flight plan suspends navigation by the system. Deleting the active flight plan: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, highlight ‘Delete Flight Plan’, and press the ENT Key. The ‘Delete all waypoints in flight plan?’ window is displayed. 3) With ‘OK’ highlighted, press the ENT Key to delete the active flight plan. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. DELETING FLIGHT PLAN ITEMS Individual waypoints, entire airways, and entire procedures can be deleted from a flight plan. Some waypoints in the final approach segment (such as the FAF or MAP) can not be deleted individually. Attempting to delete a waypoint that is not allowed results in a window displaying ‘Invalid flight plan modification.’ Deleting an individual waypoint from the active flight plan: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the waypoint to be deleted. 3) Press the CLR Key. The ‘Remove XXXXX?’ window is displayed. 258 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT 4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor. Deleting an entire airway from the active flight plan: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the white header of the airway to be deleted. 3) Press the CLR Key. The ‘Remove?’ window is displayed. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor. Deleting an entire procedure from the active flight plan: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the white header of the procedure to be deleted. 3) Press the CLR Key. The ‘Remove from flight plan?’ window is displayed. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor. Or: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key to display the Page Menu and turn the FMS Knob to highlight ‘Remove ’. 3) Press the ENT Key. The ‘Remove from flight plan?’ window is displayed. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. Deleting an individual waypoint from a stored flight plan: 1) Press the FPL Key to display the Active Flight Plan Page. 2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the flight plan to be edited. 4) Select the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored Flight Plan Page is displayed. 5) Turn the large FMS Knob to highlight the waypoint to be deleted. 6) Press the CLR Key. The ‘Remove XXXXX?’ window is displayed. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 259 FLIGHT MANAGEMENT 7) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. 8) Press the FMS Knob to remove the flashing cursor. Deleting an entire airway from a stored flight plan: 1) Press the FPL Key to display the Active Flight Plan Page. 2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the flight plan to be edited. 4) Select the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored Flight Plan Page is displayed. 5) Turn the large FMS Knob to highlight the white header of the airway to be deleted. 6) Press the CLR Key. The ‘Remove ?’ window is displayed. 7) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. 8) Press the FMS Knob to remove the flashing cursor. Deleting an entire procedure from a stored flight plan: 1) Press the FPL Key to display the Active Flight Plan Page. 2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the flight plan to be edited. 4) Select the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored Flight Plan Page is displayed. 5) Turn the large FMS Knob to highlight the white header of the procedure to be deleted. 6) Press the CLR Key. The ‘Remove from flight plan?’ window is displayed. 7) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. 8) Press the FMS Knob to remove the flashing cursor. Or: 1) Press the FPL Key to display the Active Flight Plan Page. 2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the flight plan to be edited. 4) Select the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored Flight Plan Page is displayed. 5) Press the MENU Key to display the Page Menu and turn the FMS Knob to highlight ‘Remove ’. 6) Press the ENT Key. The ‘Remove from flight plan?’ window is displayed. 260 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT 7) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. 8) Press the FMS Knob to remove the flashing cursor. CHANGING FLIGHT PLAN COMMENTS (NAMES) The comment field (or name) of each flight plan can be changed to something that is useful for identification. Changing the active flight plan comment: 1) Press the FPL Key to display the Active Flight Plan Page. 2) Press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the comment field. 3) Use the FMS Knobs to edit the comment. 4) Press the ENT Key to accept the changes. 5) Press the FMS Knob to remove the flashing cursor. Changing a stored flight plan comment: 1) Press the FPL Key to display the Active Flight Plan Page. 2) Turn the small FMS Knob clockwise one click to display the Flight Plan Catalog Page. 3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the flight plan to be edited. 4) Select the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored Flight Plan Page is displayed. 5) Turn the large FMS Knob to highlight the comment field. 6) Use the FMS Knobs to edit the comment. 7) Press the ENT Key to accept the changes. 8) Press the FMS Knob to remove the flashing cursor. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 261 FLIGHT MANAGEMENT ALONG TRACK OFFSETS A waypoint having an “along track offset” distance from an existing waypoint can be entered into a flight plan. Along track offset waypoints lie along the path of the existing flight plan, and can be used to make the system reach a specified altitude before or after reaching the specified flight plan waypoint. Offset distances can be entered from 1 to 999 nm in increments of 1 nm. Entering a negative offset distance results in an along track offset waypoint inserted before the selected waypoint, whereas entering a positive offset distance results in an along track offset waypoint inserted after the selected waypoint. Multiple offset waypoints are allowed. A waypoint must be adjacent to its parent waypoint in the flight plan, so the system limits the along-track distance to less than the length of the leg before or after the selected waypoint. If the selected waypoint is the active waypoint, the distance is limited to less than the distance to go to the active waypoint. Assigning an along track offset to a leg with indeterminate length is not permitted. An along track offset is not allowed at or after the final approach fix of an approach. An along track offset distance cannot be modified once entered. If the along track offset distance must be changed, the existing along track offset waypoint must be deleted and a new one created with the new offset distance. Along Track Offset Waypoint and Distance from Flight Plan Waypoint Along Track Offset Waypoint and Distance Figure 5-78 Along Track Offset Entering an along track offset distance: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the waypoint for the along track offset. 3) Select the ATK OFST Softkey (MFD only); or press the MENU Key, highlight ‘Create ATK Offset Waypoint’, and press the ENT Key. 262 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT 4) Enter a positive or negative offset distance in the range of +/- 1 to 999 nm (limited by leg distance). 5) Press the ENT Key to create the offset waypoint. 6) Press the FMS Knob to remove the flashing cursor. PARALLEL TRACK The Parallel Track (PTK) feature allows creation of a parallel course offset of 1 to 50 nm left or right of the current flight plan. When Parallel Track is activated, the course line drawn on the map pages shows the parallel course, and waypoint names have a lower case “p” placed after the identifier. Using direct-to, loading an approach, a holding pattern, or editing and activating the flight plan automatically cancels Parallel Track. Parallel Track is also cancelled if a course change occurs greater than 120° or the parallel tracks overlap as a result of the course change. NOTE: Vertical navigation is unavailable while the Parallel Track feature is active. Active Flight Plan prior to Parallel Track Selecting Parallel Track Figure 5-79 Active Flight Plan Window - Selecting Parallel Track Activating parallel track: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, highlight ‘Parallel Track’, and press the ENT Key. The Parallel Track Window is displayed with the direction field highlighted. 3) Turn the small FMS Knob to select ‘Left’ or ‘Right’ and press the ENT Key. The ‘DISTANCE’ field is highlighted. 4) Turn the small FMS Knob to enter a distance from 1-99 nm and press the ENT Key. ‘ACTIVATE PARALLEL TRACK’ is highlighted. 5) Press the ENT Key to activate parallel track. Press the FMS Knob or the CLR Key to cancel the parallel track activation. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 263 FLIGHT MANAGEMENT Offset Direction Offset Distance Activation Prompt Figure 5-80 Parallel Track Window Parallel Track Waypoints - TIFTO-p - TOP-p - ULNAZ-p - ... - LAA-p Activating Parallel Track affects the active flight plan from the current position on (will not affect an approach) Original Track Parallel Track Figure 5-81 Parallel Track Active If the parallel track proposed by the offset direction and distance is not allowed by the system, the activation prompt is displayed, but disabled. Parallel Track cannot be activated if a course is set using direct-to or if the active leg is the first leg of the departure procedure. Attempting to activate parallel track with these conditions results in the message ‘Parallel Track Unavailable Invalid Route Geometry’. If an approach leg is active the status indicates that the system is unable to activate the parallel track with the message ‘Parallel Track Unavailable Approach Leg Active’. If the offset direction and distance results in an unreasonable route geometry the status indicates that the system is unable to activate the parallel track because of invalid geometry. 264 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Subdued Prompt (Unavailable) Unavailable Status Invalid Geometry Approach Active Figure 5-82 Parallel Track Unavailable If the active leg is not a track between two fixes (TF) or a course to a fix (DF) leg, the status indicates that the system is unable to activate the parallel track because parallel track is not available for the active leg type. Offset Direction & Distance Subdued (Unavailable) Cancel Prompt Active Status Figure 5-83 Cancelling Parallel Track Cancelling parallel track: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, highlight ‘Parallel Track’, and press the ENT Key. The Parallel Track Window is displayed with ‘CANCEL PARALLEL TRACK?’ highlighted. 3) Press the ENT Key. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 265 FLIGHT MANAGEMENT ACTIVATING A FLIGHT PLAN LEG The system allows selection of a highlighted leg as the “active leg” (the flight plan leg which is currently used for navigation guidance). Activating a flight plan leg: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the destination waypoint for the desired leg. 3) Select the ACT LEG Softkey (MFD only); or press the MENU Key, highlight ‘Activate Leg’, and press the ENT Key. A confirmation window is displayed with ‘ACTIVATE’ highlighted. 4) Press the ENT Key to activate the flight plan leg. To cancel, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor. Current Active Leg Selected Destination Waypoint Activate Leg Softkey Figure 5-84 Active Flight Plan Page - Selecting the Leg Destination Waypoint 266 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT New Active Flight Plan Leg Confirmation Window Figure 5-85 Active Flight Plan Page - New Active Leg INVERTING A FLIGHT PLAN Any flight plan may be inverted (reversed) for navigation back to the original departure point. Inverting the active flight plan: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, highlight ‘Invert Flight Plan’, and press the ENT Key. An ‘Invert Active Flight Plan?’ confirmation window is displayed. 3) Select ‘OK’. 4) Press the ENT Key to invert and activate the active flight plan. To cancel, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. Inverting and activating a stored flight plan: 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan. 3) Select the INVERT Softkey; or press the MENU Key, highlight ‘Invert & Activate FPL?’, and press the ENT Key. The ‘Invert and activate stored flight plan?’ window is displayed. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 267 FLIGHT MANAGEMENT FLIGHT PLAN VIEWS Information about flight plans can be viewed in more than one way. The active flight plan can be configured to show cumulative distance over the length of the flight plan or the distance for each leg of the flight plan; and the active flight plan can be viewed in a narrow or wide view. In the wide view, additional information is displayed: Fuel Remaining (FUEL REM), Estimated Time Enroute (ETE), Estimated Time of Arrival (ETA), and Bearing to the waypoint (BRG). Switching between leg-to-leg waypoint distance and cumulative waypoint distance: 1) Press the FPL Key on the MFD to display the Active Flight Plan Page. 2) Select the VIEW Softkey to display the CUM and LEG-LEG Softkeys. 3) Select the CUM Softkey to view cumulative waypoint distance, or select the LEG-LEG Softkey to view leg-to-leg waypoint distance. 4) Select the BACK Softkey to return to the top level active flight plan softkeys. Active Flight Plan Leg to Leg Distance Active Flight Plan Cumulative Distance WIDE Softkey, NARROW Softkey, LEG-LEG Softkey, CUM Softkey Figure 5-86 Active Flight Plan - Leg to Leg vs. Cumulative Distance Switching between wide and narrow view: 1) Press the FPL Key on the MFD to display the Active Flight Plan Page. 2) Select the VIEW Softkey to display the WIDE and NARROW Softkeys. 3) Select the WIDE Softkey to display the wide view, or select the NARROW Softkey to display the narrow view. 4) Select the BACK Softkey to return to the top level active flight plan softkeys. 268 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Active Flight Plan Narrow View Active Flight Plan Wide View WIDE Softkey, NARROW Softkey, LEG-LEG Softkey, CUM Softkey Figure 5-87 Active Flight Plan - Wide vs. Narrow View COLLAPSING AIRWAYS The system allows airways on the active flight plan to be collapsed or expanded from the Active Flight Plan Page/Window. When airways have been collapsed, it is indicated on the airway heading. When airways are collapsed, leg-to-leg computed values such as DIS or ETE shown for the exit waypoint reflect the total of all the legs on the airway that have been hidden in the collapsed display. The DTK value is inhibited because it is not usable in this context. The Active Flight Plan Page always keeps the following three waypoints visible: “From” waypoint, “To” waypoint, and “Next” waypoint. To prevent one or more of these waypoints from being hidden in a collapsed airway segment, the airway segment that contains either the “To” or the “Next” waypoint is automatically expanded. When an airway is loaded, airways are automatically expanded to facilitate flight plan review. Q3.FEPOT Airway Collapsed View Expanded View Figure 5-88 Expanded/Collapsed Airways 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 269 FLIGHT MANAGEMENT Collapsing/expanding the airways in the active flight plan: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, highlight ‘Collapse Airways’ or ‘Expand Airways’, and press the ENT Key. The airways are collapsed/expanded. CLOSEST POINT OF FPL ‘Closest Point of FPL’ calculates the bearing and closest distance at which a flight plan passes a reference waypoint, and creates a new user waypoint along the flight plan at the location closest to a chosen reference waypoint. Determining the closest point along the active flight plan to a selected waypoint: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, highlight ‘Closest Point Of FPL’’, and press the ENT Key. A window appears with the reference waypoint field highlighted. 3) Enter the identifier of the reference waypoint and press the ENT Key. The system displays the bearing (BRG) and distance (DIS) to the closest point along the flight plan to the selected reference waypoint and creates a user waypoint at this location. The name for the new user waypoint is derived from the identifier of the reference waypoint. USER-DEFINED HOLDING PATTERNS A holding pattern can be defined at any active flight plan waypoint, or at the aircraft present position. Creating a user-defined hold at an active flight plan waypoint: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the waypoint for the hold. 3) Press the MENU Key, highlight ‘Hold At Waypoint’, and press the ENT Key. The HOLD AT window appears with the course field highlighted. 4) Use the FMS Knobs to edit the entry course, and press the ENT Key. 5) Use the small FMS Knob to select ‘INBOUND’ or ‘OUTBOUND’ course direction, and press the ENT Key. 6) Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press the ENT Key. 7) Use the FMS Knobs to edit the length, and press the ENT Key. 8) Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and press the ENT Key. 9) Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME), and press the ENT Key. 10) Press the ENT Key while ‘LOAD?’ is highlighted to add the hold into the flight plan. 270 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Waypoint Selected Hold At Waypoint Menu Selection Location of Hold Hold Entry Course Course Direction (INBOUND or OUTBOUND) Leg Length Mode Button (TIME or DIST)) Leg Length (Time in nm or Distance in minutes) Turn Direction (RIGHT or LEFT) Map of Hold Location Expect Further Clearance Time Load Hold in Active Flight Plan Figure 5-89 Creating a User Defined Holding Pattern at an Active Flight Plan Waypoint 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 271 FLIGHT MANAGEMENT Removing a user-defined hold (created at an active flight plan waypoint): 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the HOLD waypoint. 3) Press the CLR Key. A ‘Remove Holding Pattern?’ confirmation window is displayed. 4) Select ‘OK’ and press the ENT Key. The holding pattern is removed from the active flight plan. Select ‘CANCEL’ and press the ENT Key to cancel the removal of the holding pattern. Creating a user-defined hold at the aircraft present position: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, highlight ‘Hold At Present Position’, and press the ENT Key. The HOLD AT window appears with the course field highlighted. 3) Use the FMS Knobs to edit the entry course, and press the ENT Key. 4) Use the small FMS Knob to select ‘INBOUND’ or ‘OUTBOUND’ course direction, and press the ENT Key. 5) Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press the ENT Key. 6) Use the FMS Knobs to edit the length, and press the ENT Key. 7) Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and press the ENT Key. 8) Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME), and press the ENT Key. 9) Press the ENT Key while ‘ACTIVATE?’ is highlighted to create an Offroute Direct-to hold waypoint at the aircraft present position and activate the hold. Creating a user-defined hold at a Direct To waypoint: 1) Press a Direct-to Key and set up the Direct To waypoint as desired, but select ‘HOLD?’ instead of ‘ACTIVATE?’ when finished (MFD or PFD). 2) Use the FMS Knobs to edit the entry course, and press the ENT Key. 3) Use the small FMS Knob to select ‘INBOUND’ or ‘OUTBOUND’ course direction, and press the ENT Key. 4) Use the small FMS Knob to select ‘TIME’ or ‘DIST’ length mode, and press the ENT Key. 5) Use the FMS Knobs to edit the length, and press the ENT Key. 6) Use the small FMS Knob to select ‘RIGHT’ or ‘LEFT’ turn direction, and press the ENT Key. 7) Use the FMS Knobs to edit the Expect Further Clearance Time (EFC TIME), and press the ENT Key. 8) Press the ENT Key while ‘ACTIVATE?’ is highlighted to activate the Direct To with the user-defined hold defined at the Direct To waypoint. Removing a user-defined hold (created at the aircraft present position or at a Direct-To waypoint): 1) Press the Direct To Key to display the DIRECT TO Window (PFD or MFD). 2) Press the MENU Key to display the PAGE MENU with the cursor on the ‘Cancel Direct To NAV’ selection. 3) Press the ENT Key. The holding pattern is removed. 272 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Hold At Present Position Menu Selection Location of Hold Hold Entry Course Course Direction (INBOUND or OUTBOUND) Leg Length Mode Button (TIME or DIST)) Leg Length (Time in nm or Distance in minutes) Turn Direction (RIGHT or LEFT) Map of Hold Location Expect Further Clearance Time Activate Hold Figure 5-90 Creating a User Defined Holding Pattern at the Aircraft Present Position 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 273 FLIGHT MANAGEMENT Waypoint Selected Hold Entry Course Location of Hold Course Direction (INBOUND or OUTBOUND) Leg Length (Time in nm or Distance in minutes) Turn Direction (RIGHT or LEFT) Leg Length Mode Button (TIME or DIST)) Map of Hold Location Expect Further Clearance Time Hold At Direct To Waypoint selection Load Hold and Activate Direct To Figure 5-91 Creating a User Defined Holding Pattern at a Direct To Waypoint 274 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT 5.7 VERTICAL NAVIGATION NOTE: The system supports vertical path guidance and altitude constraints for the following leg types: AF, CD, CF, CI, CR, DF, FC, FD, PI, RF, and TF. Altitude constraints are not retained in stored flight plans. The G1000 system Vertical Navigation (VNV) feature provides vertical profile guidance during the enroute and terminal phases of flight. Guidance based on specified altitudes at waypoints in the active flight plan or to a direct-to waypoint is provided. It includes vertical path guidance to a descending path, which is provided as a linear deviation from the desired path. The desired path is defined by a line joining two waypoints with specified altitudes or as a vertical angle from a specified waypoint/altitude. The vertical waypoints are integrated into the active flight plan. Both manual and autopilot-coupled guidance are supported. Current Vertical Navigation Profile Disabled (fields dashed) ENBL VNV Softkey Current Vertical Navigation Profile Enabled (valid data) CNCL VNV Softkey Figure 5-92 Enabling/Disabling Vertical Navigation Enabling VNV guidance: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Select the ENBL VNV Softkey; or press the MENU Key, highlight ‘Enable VNV’, and press the ENT Key. Vertical navigation is enabled, and vertical guidance begins with the waypoint shown in the CURRENT VNV PROFILE box (defaults first waypoint in the active flight plan with an altitude enabled for vertical navigation (e.g., HABUK)). Disabling VNV guidance: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Select the CNCL VNV Softkey; or press the MENU Key, highlight ‘Cancel VNV’, and press the ENT Key. Vertical navigation is disabled. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 275 FLIGHT MANAGEMENT Canceling vertical navigation results in vertical deviation (V DEV), vertical speed required (VS REQ), and time to top of descent/bottom of descent (TIME TO TOD/BOD) going invalid. The Vertical Deviation Indicator (VDI) and Required Vertical Speed Indicator (RVSI) on the PFD are removed, and the V DEV, VS REQ, and TIME TO TOD items displayed in the CURRENT VNV PROFILE box are dashed. VNV remains disabled until manually enabled. Vertical guidance in reversionary mode can only be enabled for a direct-to waypoint. The system allows a vertical navigation direct-to to any waypoint in the active flight plan with an altitude constraint “designated” for vertical guidance. Selecting the VNV Direct-to Softkey on the Active Flight Plan Page allows the flight plan to be flown, while vertical guidance based on the altitude constraint at the VNV direct-to waypoint is provided. The altitude change begins immediately and is spread along the flight plan from current position to the vertical direct-to waypoint, not just along the leg for the direct-to waypoint. A direct-to with altitude constraint activated by pressing the Direct-to Key also provides vertical guidance, but would bypass flight plan waypoints between the current position in the flight plan and the direct-to waypoint. A top of descent (TOD) point is computed based on the default flight path angle; descent begins once the TOD is reached. Current Vertical Navigation Profile Prior to VNV Direct-to VNV Direct-To Softkey Current Vertical Navigation Profile After VNV Direct-to VNV PROF Softkey Figure 5-93 Vertical Navigation Direct-To Activating a vertical navigation direct-to: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the desired waypoint. NOTE: The selected waypoint must have a designated altitude constraint (cyan number) to be used. If not, the first waypoint in the flight plan with a designated altitude constraint is selected. 276 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT 3) Select the VNV Direct-To Softkey; or press the MENU Key, highlight ‘VNV Direct-To’, and press the ENT Key. An ‘Activate vertical Direct-to to: NNNNNFT at XXXXXX?’ confirmation window is displayed. 4) Press the ENT Key. Vertical guidance begins to the altitude constraint for the selected waypoint. 5) Press the FMS Knob to remove the flashing cursor. The vertical navigation profile can be modified by directly entering a vertical speed target (VS TGT) and/or flight path angle (FPA) in the CURRENT VNV PROFILE box. Modifying the VS TGT and FPA: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Select the VNV PROF Softkey; or press the MENU Key, highlight ‘Select VNV Profile Window’, and press the ENT Key. The cursor is now located in the CURRENT VNV PROFILE box. 3) Turn the FMS Knobs as needed to edit the values. 4) Press the FMS Knob to remove the flashing cursor. ALTITUDE CONSTRAINTS The system can use altitude constraints associated with lateral waypoints to give guidance for vertical navigation. These altitudes are, depending on the specific instance, manually entered or retrieved from the published altitudes in the navigation database. The navigation database only contains altitudes for procedures that call for “Cross at” altitudes. If the procedure states “Expect to cross at,” then the altitude is not in the database. In this case the altitude may be entered manually. Displayed Text Examples Cross AT or ABOVE 5,000 ft Large White Text Large Cyan Text Cross AT 2,300 ft Small Cyan Text Cross AT or BELOW 3,000 ft Small Cyan Subdued Text Altitude Constraint Examples Small White Text with Altitude Restriction Bar Figure 5-94 Waypoint Altitude Constraints 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 277 FLIGHT MANAGEMENT White Text Cyan Text Cyan Subdued Text Large Altitude calculated by the system Text estimating the altitude of the aircraft as it passes over the navigation point. This altitude is provided as a reference and is not designated to be used in determining vertical speed and deviation guidance. Altitude has been entered manually. Altitude is designated for use in giving vertical speed and deviation guidance. Altitude does not match the published altitude in navigation database or no published altitude exists. The system cannot use this altitude in determining vertical speed and deviation guidance because of an invalid constraint condition. Small Text Altitude is designated for use in giving vertical speed and deviation guidance. Altitude has been retrieved from the navigation database or has been entered manually and matches a published altitude in the navigation database. The system cannot use this altitude in determining vertical speed and deviation guidance because of an invalid constraint condition. Altitude is not designated to be used in determining vertical speed and deviation guidance. Altitude has been retrieved from the navigation database and is provided as a reference. Table 5-8 Altitude Constraint Size and Color Coding Altitudes associated with arrival and approach procedures are “auto-designated”. This means the system automatically uses the altitudes loaded with the arrival or approach for giving vertical speed and deviation guidance. Note that these altitudes are displayed as blue text up to, but not including, the FAF. The FAF is always a “reference only” altitude and cannot be designated, unless the selected approach does not provide vertical guidance. In this case, the FAF altitude can be designated. Altitudes that have been designated for use in vertical guidance can be “un-designated” using the CLR Key. The altitude is now displayed only as a reference. It is not used to give vertical guidance. Other displayed altitudes may change due to re-calculations or be rendered invalid as a result of manually changing an altitude to a non-designated altitude. Designating a waypoint altitude to be used for vertical guidance: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude. 3) Turn the small FMS Knob to enter editing mode. 4) Press the ENT Key. The altitude is now shown in blue, indicating it is usable for vertical guidance. Designating a procedure waypoint altitude to be used for vertical guidance: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude. 3) Press the ENT Key. The altitude is now shown in blue, indicating it is usable for vertical guidance. Altitude constraints are displayed and entered in feet mean sea level (MSL) values to the nearest hundred. An altitude constraint in feet above ground level (AGL) format is supported for airports. When a database altitude restriction is displayed, the system allows entry of a different altitude when creating a waypoint, effectively overriding the database restriction (only before the FAF). When a database altitude restriction of type “AT or ABOVE” or “AT or BELOW” is activated, the system uses the “AT” portion of the restriction to define the vertical profile. 278 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT An altitude constraint is invalid if: • Meeting the constraint requires the aircraft to climb • Meeting the constraint requires the maximum flight path angle (6° down) or maximum vertical speed (-6000 fpm) to be exceeded • The altitude constraint results in a TOD behind the aircraft present position • The constraint is within a leg type for which altitude constraints are not supported • The altitude constraint is added to the FAF of an approach that provides vertical guidance (i.e., ILS or GPS SBAS approach) • The altitude constraint is added to a waypoint past the FAF. Entering/modifiying an altitude constraint: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. 3) Enter an altitude constraint value using the FMS Knobs. To enter altitudes as a flight level, turn the small FMS Knob counter-clockwise past zero or clockwise past 9 on the first character, and the system automatically changes to show units of Flight Level. Turn the large FMS Knob clockwise to highlight the first zero and enter the three digit flight level. 4) Press the ENT Key to accept the altitude constraint; if the selected waypoint is an airport, an additional choice is displayed. Turn the small FMS Knob to choose ‘MSL’ or ‘AGL’, and press the ENT Key to accept the altitude. Altitude constraints can be modified or deleted after having been added to the flight plan. In the event an altitude constraint is deleted and the navigation database contains an altitude restriction for the lateral waypoint, the system displays the altitude restriction from the database provided no predicted altitude can be provided. The system also provides a way to reinstate a published altitude constraint that has been edited. Deleting an altitude constraint provided by the navigation database: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. 3) Press the CLR Key. A ‘Remove VNV altitude constraint?’ confirmation window is displayed. 4) Select ‘OK’ and press the ENT Key. Deleting an altitude constraint that has been manually entered: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. 3) Press the CLR Key. A ‘Remove or Revert to published VNV altitude of nnnnnFT?’ confirmation window is displayed. 4) Select ‘REMOVE’ and press the ENT Key. The manually entered altitude is deleted (it is replaced by a system calculated altitude, if available). 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 279 FLIGHT MANAGEMENT Reverting a manually entered altitude constraint back to the navigation database value: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. 3) Press the CLR Key. A ‘Remove or Revert to published VNV altitude of nnnnnFT?’ confirmation window is displayed. 4) Select ‘REVERT’ and press the ENT Key. The altitude is changed to the navigation database value. 5) Press the FMS Knob to remove the flashing cursor. Modifying a system calculated altitude constraint: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. 3) Press the CLR Key. An ‘Edit or Revert to published VNV altitude of nnnnnFT?’ confirmation window is displayed. 4) Select ‘EDIT’ and press the ENT Key. 5) Edit the value using the FMS Knobs, and press the ENT Key. 6) Press the FMS Knob to remove the flashing cursor. 280 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT 5.8 PROCEDURES The system can access the whole range of instrument procedures available. Departures (DPs), arrivals (STARs), and non-precision and precision approaches (APPRs) are stored within the database and can be loaded using the Procedures (PROC) Key. The selected procedure for the departure or arrival airport is added to the active flight plan. No waypoints are required to be in the active flight plan to load procedures; however, if the departure and arrival airport are already loaded, the procedure loading window defaults to the appropriate airport, saving some time selecting the correct airport on the Procedure Loading Page. Whenever an approach is selected, the choice to either “load” or “activate” is given. “Loading” adds the approach to the end of the flight plan without immediately using it for navigation guidance. This allows continued navigation via the intermediate waypoints in the original flight plan, but keeps the procedure available on the Active Flight Plan Page for quick activation when needed. “Activating” also adds the procedure to the end of the flight plan but immediately begins to provide guidance to the first waypoint in the approach. The system adds terminal procedures to the flight plan based on leg types coded within that procedure in the navigation database. If the terminal procedure in the flight plan contains an identifier like ‘6368ft’, that indicates a leg that terminates when the specified altitude (6368 feet) has been exceeded. A heading leg in the flight plan displays ‘hdg’ preceding the DTK (e.g. ‘hdg 008°’). A flight plan leg requiring the pilot to manually intitiate sequencing to the next leg displays ‘MANSEQ’ as the identifier. Heading Leg Terminating at the Specified Altitude Manually Sequenced Heading Leg Figure 5-95 Procedure Leg Identifiers 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 281 FLIGHT MANAGEMENT DEPARTURES A Departure Procedure (DP) is loaded at the departure airport in the flight plan. Only one departure can be loaded at a time in a flight plan. If a departure is loaded when another departure is already in the active flight plan, the new departure replaces the previous departure. The route is defined by selection of a departure, the transition waypoints, and a runway. LOADING A DEPARTURE INTO THE ACTIVE FLIGHT PLAN Loading a departure into the active flight plan using the PROC Key: 1) Press the PROC Key. The Procedures Window is displayed. 2) Highlight ‘SELECT DEPARTURE’. 3) Press the ENT Key. The Departure Loading Page is displayed. 4) Use the FMS Knob to select an airport and press the ENT Key. 5) Select a departure from the list and press the ENT Key. 6) Select a runway (if required) and press the ENT Key. 7) Select a transition (if required) and press the ENT Key. ‘LOAD?’ is highlighted. 8) Press the ENT Key to load the departure procedure. Departure Airport Available Procedure Actions Loaded Procedures Departure Preview Departure Choices Figure 5-96 Departure Selection 282 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Selected Departure Loaded Departure Procedure Loading Page Selection Softkeys Figure 5-97 Departure Loading Viewing available departures at an airport: 1) From the Airport Information Page (first page in the WPT group), select the DP Softkey. The Departure Information Page is displayed, defaulting to the airport displayed on the Airport information Page. 2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and press the ENT Key. 3) Turn the large FMS Knob to highlight the Departure. The departure is previewed on the map. 4) Turn the small FMS Knob to view the available departures. Press the ENT Key to select the departure. The cursor moves to the Runway box. The departure is previewed on the map. 5) Turn the small FMS Knob to view the available runways. Press the ENT Key to select the runway. The cursor moves to the Transition box (only if there are available transitions). The departure is previewed on the map. 6) Turn the small FMS Knob to view the available transitions. Press the ENT Key to select the transition. The cursor moves to the Sequence box. The departure is previewed on the map. 7) Select the INFO-1 Softkey or the INFO-2 Softkey to return to the Airport Information Page. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 283 FLIGHT MANAGEMENT Loading a departure into the active flight plan from the Departure Information Page: 1) From the Airport Information Page (first page in the WPT group), select the DP Softkey. The Departure Information Page is displayed, defaulting to the airport displayed on the Airport information Page. 2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and press the ENT Key. 3) Select a different departure, if desired. a) Turn the large FMS Knob to highlight the Departure. The departure is previewed on the map. b) Turn the small FMS Knob to view the available departures. Press the ENT Key to select the departure. The cursor moves to the Runway box. The departure is previewed on the map. c) Turn the small FMS Knob to view the available runways. Press the ENT Key to select the runway. The cursor moves to the Transition box (only if there are available transitions). The departure is previewed on the map. d) Turn the small FMS Knob to view the available transitions. Press the ENT Key to select the transition. The cursor moves to the Sequence box. The departure is previewed on the map. 4) Press the MENU Key to display the Departure Information Page Menu. 5) Turn the FMS Knob to highlight ‘Load Departure’. 6) Press the ENT Key to load the departure procedure into the active flight plan. REMOVING A DEPARTURE FROM THE ACTIVE FLIGHT PLAN When plans change while flying IFR, departures can be easily removed from the Active Flight Plan. Removing a departure procedure from the active flight plan: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, and highlight ‘Remove Departure’. 3) Press the ENT Key. A confirmation window is displayed listing the departure procedure. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT Key. Or: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the FMS Knob, and turn to highlight the departure header in the active flight plan. 3) Press the CLR Key. A confirmation window is displayed listing the departure procedure. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor. 284 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT ARRIVALS A Standard Terminal Arrival (STAR) can be loaded at any airport that has one available. Only one arrival can be loaded at a time in a flight plan. If an arrival is loaded when another arrival is already in the active flight plan, the new arrival replaces the previous arrival. The route is defined by selection of an arrival, the transition waypoints, and a runway. LOADING AN ARRIVAL INTO THE ACTIVE FLIGHT PLAN Loading an arrival into the active flight plan using the PROC Key: 1) Press the PROC Key. The Procedures Window is displayed. 2) Highlight ‘SELECT ARRIVAL’. 3) Press the ENT Key. The Arrival Loading Page is displayed. 4) Use the FMS Knob to select an airport and press the ENT Key. 5) Select an arrival from the list and press the ENT Key. 6) Select a transition (if required) and press the ENT Key. 7) Select a runway (if required) and press the ENT Key. ‘LOAD?’ is highlighted. 8) Press the ENT Key to load the arrival procedure. Available Procedure Actions Loaded Procedures Destination Airport Arrival Preview Arrival Choices Figure 5-98 Arrival Selection 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 285 FLIGHT MANAGEMENT Selected Arrival Loaded Arrival Procedure Loading Page Selection Softkeys Figure 5-99 Arrival Loading Viewing available arrivals at an airport: 1) From the Airport Information Page (first page in the WPT group), select the STAR Softkey. The Arrival Information Page is displayed, defaulting to the airport displayed on the Airport Information Page. 2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and press the ENT Key. 3) Turn the large FMS Knob to highlight the Arrival. The arrival is previewed on the map. 4) Turn the small FMS Knob to view the available arrivals. Press the ENT Key to select the arrival. The cursor moves to the Transition box. The arrival is previewed on the map. 5) Turn the small FMS Knob to view the available transitions. Press the ENT Key to select the transition. The cursor moves to the Runway box. The arrival is previewed on the map. 6) Turn the small FMS Knob to view the available runways. Press the ENT Key to select the runway. The cursor moves to the Sequence box. The arrival is previewed on the map. 7) Select the INFO-1 Softkey or the INFO-2 Softkey to return to the Airport Information Page. 286 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Loading an arrival into the active flight plan from the Arrival Information Page: 1) From the Airport Information Page (first page in the WPT group), select the STAR Softkey. The Arrival Information Page is displayed, defaulting to the airport displayed on the Airport information Page. 2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and press the ENT Key. 3) Select a different arrival, if desired. a) Turn the large FMS Knob to highlight the arrival. The arrival is previewed on the map. b) Turn the small FMS Knob to view the available arrivals. Press the ENT Key to select the arrival. The cursor moves to the Transition box (only if there are available transitions). The arrival is previewed on the map. c) Turn the small FMS Knob to view the available transitions. Press the ENT Key to select the transition. The cursor moves to the Runway box. The arrival is previewed on the map. d) Turn the small FMS Knob to view the available runways. Press the ENT Key to select the runway. The cursor moves to the Sequence box. The arrival is previewed on the map. 4) Press the MENU Key to display the Arrival Information Page Menu. 5) Turn the FMS Knob to highlight ‘Load Arrival’. 6) Press the ENT Key to load the arrival procedure into the active flight plan. REMOVING AN ARRIVAL FROM THE ACTIVE FLIGHT PLAN When plans change while flying IFR, arrivals can be easily removed from the Active Flight Plan. Removing an arrival from the active flight plan: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, and highlight ‘Remove Arrival’. 3) Press the ENT Key. A confirmation window is displayed listing the arrival procedure. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT Key. Or: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the FMS Knob, and turn to highlight the arrival header in the active flight plan. 3) Press the CLR Key. A confirmation window is displayed listing the arrival procedure. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 287 FLIGHT MANAGEMENT APPROACHES NOTE: If certain GPS parameters (SBAS, RAIM, etc.) are not available, some published approach procedures for the desired airport may not be displayed in the list of available approaches. An Approach Procedure (APPR) can be loaded at any airport that has one available, and provides guidance for non-precision and precision approaches to airports with published instrument approach procedures. Only one approach can be loaded at a time in a flight plan. If an approach is loaded when another approach is already in the active flight plan, the new approach replaces the previous approach. The route is defined by selection of an approach and the transition waypoints. Whenever an approach is selected, the choice to either “load” or “activate” is given. “Loading” adds the approach to the end of the flight plan without immediately using it for navigation guidance. This allows continued navigation via the intermediate waypoints in the original flight plan, but keeps the procedure available on the Active Flight Plan Page for quick activation when needed. “Activating” also adds the procedure to the end of the flight plan but immediately begins to provide guidance to the first waypoint in the approach. When selecting an approach, a “GPS” designation to the right of the procedure name indicates the procedure can be flown using the GPS receiver. Some procedures do not have this designation, meaning the GPS receiver can be used for supplemental navigation guidance only. If the GPS receiver cannot be used for primary guidance, the appropriate navigation receiver must be used for the selected approach (e.g., VOR or ILS). The final course segment of ILS approaches, for example, must be flown by tuning the NAV receiver to the proper frequency and selecting that NAV receiver on the CDI. The G1000 SBAS GPS allows for flying LNAV, LNAV+V, LNAV/VNAV, LP, LP+V, LPV, and RNP approach service levels according to the published chart. The ‘+V’ designation adds advisory vertical guidance for assistance in maintaining a constant vertical glidepath similar to an ILS glideslope on approach. This guidance is displayed on the system PFD in the same location as the ILS glideslope using a magenta diamond. The active approach service level is annunciated on the HSI as shown in the following table: HSI Annunciation Description LNAV GPS approach using published LNAV minima LNAV+V GPS approach using published LNAV minima. Advisory vertical guidance is provided L/VNAV GPS approach using published LNAV/VNAV (available only if minima (downgrades to LNAV if SBAS SBAS available) unavailable) LP GPS approach using published LP minima (available only if (downgrades to LNAV if SBAS unavailable) SBAS available) LP+V RNAV GPS approach using published LP minima (available only if Advisory vertical guidance is provided SBAS available) (downgrades to LNAV if SBAS unavailable) LPV GPS approach using published LPV minima (available only if (downgrades to LNAV if SBAS unavailable) SBAS available) Example on HSI Approach Service Level - LNAV, LNAV+V, L/VNAV, LP, LP+V, LPV Table 5-9 Approach Types 288 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT LOADING AN APPROACH INTO THE ACTIVE FLIGHT PLAN Loading an approach into the active flight plan using the PROC Key: 1) Press the PROC Key. The Procedures Window is displayed. 2) Highlight ‘SELECT APPROACH’, and press the ENT Key. The Approach Loading Page is displayed. 3) Select the airport and approach: a) Use the FMS Knob to select an airport and press the ENT Key. b) Select an approach from the list and press the ENT Key. Or: a) If necessary, push the FMS Knob to exit the approach list, and use the large FMS Knob to move the cursor to the APPROACH CHANNEL field. b) Use the FMS Knob to enter the approach channel number, and press the ENT Key to accept the approach channel number. The airport and approach are selected. 4) Select a transition (if required) and press the ENT Key. 5) Minimums a) To set ‘MINIMUMS’, turn the small FMS Knob to select ‘BARO’, ‘TEMP COMP’ or ‘RAD ALT’, and press the ENT Key. Turn the small FMS Knob to select the altitude, and press the ENT Key. b) If ‘TEMP COMP’ was selected, the cursor moves to the temperature field. Turn the small FMS Knob to select the temperature, and press the ENT Key. Or: a) To skip setting minimums, press the ENT Key. 6) Press the ENT Key with ‘LOAD?’ highlighted to load the approach procedure; or turn the large FMS Knob to highlight ‘ACTIVATE’ and press the ENT Key to load and activate the approach procedure. NOTE: When GPS is not approved for the selected final approach course, the message ‘NOT APPROVED FOR GPS’ is displayed. GPS provides guidance to the approach, but the HSI must to be switched to a NAV receiver to fly the final course of the approach. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 289 FLIGHT MANAGEMENT Available Procedure Actions Loaded Procedures Destination Airport Approach Preview Approach Choices Figure 5-100 Approach Selection Selected Approach Procedure Loading Page Selection Softkeys Loaded Approach LOAD or ACTIVATE? Annunciation Figure 5-101 Approach Loading 290 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Viewing available approaches at an airport: 1) From the Airport Information Page (first page in the WPT group), select the APR Softkey. The Approach Information Page is displayed, defaulting to the airport displayed on the Airport information Page. 2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and press the ENT Key. 3) Press the FMS Knob, then turn the large FMS Knob to highlight the Approach. The approach is previewed on the map. 4) Turn the small FMS Knob to view the available approaches. Press the ENT Key to select the approach. The cursor moves to the Transition box. The approach is previewed on the map. 5) Turn the small FMS Knob to view the available transitions. Press the ENT Key to select the transition. The cursor moves to the Minimums box. The approach is previewed on the map. 6) Select the INFO-1 Softkey or the INFO-2 Softkey to return to the Airport Information Page. Loading an approach into the active flight plan from the Nearest Airport Page: 1) Select the Nearest Airports Page. 2) Press the FMS Knob, then turn the large FMS Knob to highlight the desired nearest airport. The airport is previewed on the map. 3) Select the APR Softkey; or press the MENU Key, highlight ‘Select Approach Window’, and press the ENT Key. 4) Turn the FMS Knob to highlight the desired approach. 5) Select the LD APR Softkey; or press the MENU Key, highlight ‘Load Approach’, and press the ENT Key. The Approach Loading Page is displayed with the transitions field highlighted. 6) Turn the FMS Knob to highlight the desired transition, and press the ENT Key. 7) Minimums a) To set ‘MINIMUMS’, turn the small FMS Knob to select ‘BARO’, ‘TEMP COMP’ or ‘RAD ALT’, and press the ENT Key. Turn the small FMS Knob to select the altitude, and press the ENT Key. b) If ‘TEMP COMP’ was selected, the cursor moves to the temperature field. Turn the small FMS Knob to select the temperature, and press the ENT Key. Or: a) To skip setting minimums, press the ENT Key. 8) Press the ENT Key with ‘LOAD?’ highlighted to load the approach procedure; or turn the large FMS Knob to highlight ‘ACTIVATE’ and press the ENT Key to load and activate the approach procedure. The system continues navigating the current flight plan until the approach is activated. When GPS is not approved for the selected final approach course, the message ‘NOT APPROVED FOR GPS’ is displayed. GPS provides guidance to the approach, but the HSI must to be switched to a NAV receiver to fly the final course of the approach. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 291 FLIGHT MANAGEMENT ACTIVATING AN APPROACH A previously loaded approach can be activated from the Procedures Window. Activating a previously loaded approach: 1) Press the PROC Key. The Procedures Window is displayed with ‘Activate Approach’ highlighted. 2) Press the ENT Key to activate the approach. In many cases, it may be easiest to “load” the full approach while still some distance away, enroute to the destination airport. Later, if vectored to final, use the steps above to select ‘Activate Vector-To-Final’ — which makes the inbound course to the FAF waypoint active. Activating a previously loaded approach with vectors to final: 1) Press the PROC Key to display the Procedures Window. 2) Highlight ‘ACTIVATE VECTOR-TO-FINAL’ and press the ENT Key. Loading and activating an approach using the MENU Key: 1) From the Approach Loading Page, press the MENU Key. The page menu is displayed with ‘Load & Activate Approach’ highlighted. 2) Press the ENT Key. When GPS is not approved for the selected final approach course, the message ‘NOT APPROVED FOR GPS’ is displayed. GPS provides guidance to the approach, but the HSI must to be switched to a NAV receiver to fly the final course of the approach. REMOVING AN APPROACH FROM THE ACTIVE FLIGHT PLAN When plans change while flying IFR, approaches can be easily removed from the Active Flight Plan. Removing an approach from the active flight plan: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, and highlight ‘Remove Approach’. 3) Press the ENT Key. A confirmation window is displayed listing the approach procedure. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal, highlight ‘CANCEL’ and press the ENT Key. Or: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the FMS Knob, and turn to highlight the approach header in the active flight plan. 3) Press the CLR Key. A confirmation window is displayed listing the approach procedure. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal, highlight ‘CANCEL’ and press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor. 292 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT MISSED APPROACH Activating a missed approach in the active flight plan: 1) Press the PROC Key. 2) Turn the FMS Knob to highlight ‘ACTIVATE MISSED APPROACH’. 3) Press the ENT Key. The aircraft automatically sequences to the MAHP. Or: Press the Go-Around Button. In this missed approach procedure, the altitude immediately following the MAP (in this case ‘6368ft’) is not part of the published procedure. It is simply a Course to Altitude (CA) leg which guides the aircraft along the runway centerline until the altitude required to safely make the first turn toward the MAHP is exceeded. This altitude is provided by the navigation database, and may be below, equal to, or above the published minimums for this approach. In this case, if the aircraft altitude is below the specified altitude (6,368 feet) after crossing the MAP, a direct-to is established to provide a course on runway heading until an altitude of 6,368 feet is reached. After reaching 6,368 feet, a direct-to is established to the published MAHP (in this case MOGAL). If the aircraft altitude is above the specified altitude after crossing the MAP, a direct-to is established to the published fix (MOGAL) to begin the missed approach procedure. Course to Alttitude Leg Figure 5-102 Course to Altitude In some missed approach procedures this Course to Altitude leg may be part of the published procedure. For example, a procedure may dictate a climb to 5,500 feet, then turn left and proceed to the Missed Approach Hold Point (MAHP). In this case, the altitude would appear in the list of waypoints as ‘5500ft’. Again, if the aircraft altitude is lower than the prescribed altitude, a direct-to is established on a Course to Altitude leg when the missed approach procedure is activated. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 293 FLIGHT MANAGEMENT TEMPERATURE COMPENSATED ALTITUDE If desired, the system can compensate the loaded approach altitudes based on a pilot-supplied temperature at the destination. For example, if the pilot enters a destination temperature of -40º C, the system increases the approach altitudes accordingly. A temperature compensated altitude is displayed in slanted text. Enabling temperature compensated altitude: 1) From the Active Flight Plan Page, press the MENU Key. The Page Menu is displayed. 2) Turn the FMS Knob to highlight ‘Temperature Compensation’. 3) Press the ENT Key. The TEMPERATURE COMPENSATION Window is displayed. 4) Use the small FMS Knob to select the temperature at the . The compensated altitude is computed as the temperature is selected. NOTE: The temperature at the destination can be entered in the TEMPERATURE COMPENSATION Window on the MFD, or in the REFERENCES Window on the PFD. There is only one compensation temperature for the system, therefore, changing the temperature will affect both the loaded approach altitudes and the minimums. Refer to the Flight Instruments section for information about applying temperature compensation to the MDA/DH. 5) Press the ENT Key. ‘ACTIVATE COMPENSATION?’ is highlighted. 6) Press the ENT Key. The compensated altitudes for the approach are shown in the flight plan. Selected Temperature FAF Altitude Compensated Altitude Temperature Compensation Selected Figure 5-103 Temperature Compensation 294 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT ACTIVATE COMPENSATION? Highlighted CANCEL COMPENSATION? Highlighted Figure 5-104 Activating/Cancelling Temperature Compensation Compensated Altitudes Uncompensated Altitudes Figure 5-105 Temperature Compensation in the Active Flight Plan Disabling temperature compensated altitude: 1) From the Active Flight Plan Page, press the MENU Key. The Page Menu is displayed. 2) Turn the FMS Knob to highlight ‘Temperature Compensation’. 3) Press the ENT Key. The TEMPERATURE COMPENSATION Window is displayed. 4) Press the ENT Key. ‘CANCEL COMPENSATION?’ is highlighted. 5) Press the ENT Key. The temperature compensated altitude at the FAF is cancelled. NOTE: Activating/cancelling temperature compensation for the loaded approach altitudes does not select/ deselect temperature compensated minimums (MDA/DH), nor does selecting/deselecting temperature compensated minimums activate/cancel temperature compensated approach altitudes. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 295 FLIGHT MANAGEMENT 5.9 TRIP PLANNING The system allows the pilot to view trip planning information, fuel information, and other information for a specified flight plan or flight plan leg based on automatic data, or based on manually entered data. Weight planning is also available, based on fuel sensor data and the active flight plan (to estimate remaining fuel). TRIP PLANNING All of the input of data needed for calculation and viewing of the statistics is done on the Trip Planning Page located in the AUX Page Group. Selected Flight Plan Segment - FPL Number/Cumulative Legs (CUM or REM) or Leg Number (NN) - Waypoints Defining Selected Flight Plan/Flight Plan Leg Trip Planning Page Mode - Automatic/Manual Trip Input Data (sensor/pilot) Preview of Selected Flight Plan/ Flight Plan Leg - Departure Time (local) - Ground Speed - Fuel Flow - Fuel On Board Aircraft - Calibrated Airspeed - Indicated Altitude - Barometric Pressure - Total Air Temperature Trip Statistics Desired Track Distance Est. Time Enroute Est. Time of Arrival Enroute Safe Altitude Sunrise Time (local) Sunset Time (local) - Other Statistics - Density Altitude - True Airspeed (TAS) Fuel Statistics Efficiency Total Endurance Remaining Fuel Remaining Endurance Fuel Required Total Range - Softkeys - Automatic/Manual Page Mode - Flight Plan/Waypoint Mode Figure 5-106 Trip Planning Page The trip planning inputs are based on sensor inputs (automatic page mode) or on pilot inputs (manual page mode). Some additional explanation of the sources for some of the inputs is as follows: • Departure time (DEP TIME) - This defaults to the current time in automatic page mode. The computations are from the aircraft present position, so the aircraft is always just departing. • Calibrated airspeed (CALIBRATED AS) - The primary source is from the air data system, and the secondary source of information is GPS ground speed. • Indicated altitude (IND ALTITUDE) - The primary source is the barometric altitude, and the secondary source of information is GPS altitude. 296 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT TRIP STATISTICS The trip statistics are calculated based on the selected starting and ending waypoints and the trip planning inputs. In flight plan mode (FPL) with a stored flight plan selected (NN), and the entire flight plan (CUM) selected, the waypoints are the starting and ending waypoints of the selected flight plan. In flight plan mode (FPL) with a stored flight plan selected (NN), and a specific leg (NN) selected, the waypoints are the endpoints of the selected leg. In flight plan mode (FPL) with the active flight plan selected (00), and the remaining flight plan (REM) selected, the ‘from’ waypoint is the present position of the aircraft and the ‘to’ waypoint is the endpoint of the active flight plan. In flight plan mode (FPL) with the active flight plan selected (00), and a specific leg (NN) selected, the ‘from’ waypoint is the current aircraft position and the ‘to’ waypoint is the endpoint of the selected leg. In waypoint (WPTS) mode these are manually selected waypoints (if there is an active flight plan, these default to the endpoints of the active leg). Some of the calculated trip statistics are dashed when the selected leg of the active flight plan has already been flown. • Desired Track (DTK) - DTK is shown as nnn° and is the desired track between the selected waypoints. It is dashed unless only a single leg is selected. • Distance (DIS) - The distance is shown in tenths of units up to 99.9, and in whole units up to 9999. • Estimated time enroute (ETE) - ETE is shown as hours:minutes until less than an hour, then it is shown as minutes:seconds. • Estimated time of arrival (ETA) - ETA is shown as hours:minutes and is the local time at the destination. - If in waypoint mode then the ETA is the ETE added to the departure time. - If a flight plan other than the active flight plan is selected it shows the ETA by adding to the departure time all of the ETEs of the legs up to the selected leg. If the entire flight plan is selected, then the ETA is calculated as if the last leg of the flight plan was selected. - If the active flight plan is selected the ETA reflects the current position of the aircraft and the current leg being flown. The ETA is calculated by adding to the current time the ETEs of the current leg up to and including the selected leg. If the entire flight plan is selected, then the ETA is calculated as if the last leg of the flight plan was selected. • Enroute safe altitude (ESA) - The ESA is shown as nnnnnFT • Destination sunrise and sunset times (SUNRISE, SUNSET) - These times are shown as hours:minutes and are the local time at the destination. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 297 FLIGHT MANAGEMENT FUEL STATISTICS The fuel statistics are calculated based on the selected starting and ending waypoints and the trip planning inputs. Some of the calculated trip statistics are dashed when the selected leg of the active flight plan has already been flown. • Fuel efficiency (EFFICIENCY) - This value is calculated by dividing the current ground speed by the current fuel flow. • Time of fuel endurance (TOTAL ENDUR) - This time is shown as hours:minutes. This value is obtained by dividing the amount of fuel on board by the current fuel flow. • Fuel on board upon reaching end of selected leg (REM FUEL) - This value is calculated by taking the amount of fuel onboard and subtracting the fuel required to reach the end of the selected leg. • Fuel endurance remaining at end of selected leg (REM ENDUR) - This value is calculated by taking the time of fuel endurance and subtracting the estimated time enroute to the end of the selected leg. • Fuel required for trip (FUEL REQ) - This value is calculated by multiplying the time to go by the fuel flow. • Total range at entered fuel flow (TOTAL RANGE) - This value is calculated by multiplying the time of fuel endurance by the ground speed. OTHER STATISTICS These statistics are calculated based on the system sensor inputs or the manual trip planning inputs. • Density altitude (DENSITY ALT) • True airspeed (TRUE AIRSPEED) The pilot may select automatic (AUTO) or manual (MANUAL) page mode, and flight plan (FPL) or waypoint (WPTS) mode. In automatic page mode, only the FPL, LEG, or waypoint IDs are editable (based on FPL/WPTS selection). Selected Flight Plan NN - Selected Leg(s) 00 is Active FPL 01-99 are Stored FPLs Starting and Ending Waypoint of Selected Flight Plan Segment Stored Flight Plan - CUM: Beginning to End of FPL - NN: Beginning to End of Selected Leg Active Flight Plan - REM: Pres. Pos. to End of FPL - NN: Pres. Pos. to End of Selected Leg Figure 5-107 Trip Planning Page - Flight Plan Mode Selected Flight Plan Not Available Selected Leg(s) Not Available Selected Starting and Ending Waypoints Figure 5-108 Trip Planning Page - Waypoint Mode 298 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Selecting automatic or manual page mode: Select the AUTO Softkey or the MANUAL Softkey; or press the MENU Key, highlight ‘Auto Mode’ or ‘Manual Mode’, and press the ENT Key. Selecting flight plan or waypoint mode: Select the FPL Softkey or the WPTS Softkey; or press the MENU Key, highlight ‘Flight Plan Mode’ or ‘Waypoints Mode’, and press the ENT Key. Selecting a flight plan and leg for trip statistics: 1) Press the FMS Knob to activate the cursor in the flight plan number field. 2) Turn the small FMS Knob to select the desired flight plan number. 3) Turn the large FMS Knob to highlight ‘CUM’ or ‘REM’. The statistics for each leg can be viewed by turning the small FMS Knob to select the desired leg. The Inset Map also displays the selected data. Selecting waypoints for waypoint mode: 1) Select the WPTS Softkey; or press the MENU Key, highlight ‘Waypoints Mode’, and press the ENT Key. The cursor is positioned in the waypoint field directly below the FPL field. 2) Turn the FMS knobs to select the desired waypoint (or select from the Page Menu ‘Set WPT to Present Position’ if that is what is desired), and press the ENT Key. The cursor moves to the second waypoint field. 3) Turn the FMS knobs to select the desired waypoint, and press the ENT Key. The statistics for the selected leg are displayed. In manual page mode, the other eight trip input data fields must be entered by the pilot, in addition to flight plan and leg selection. Entering manual data for trip statistics calculations: 1) Select the MANUAL Softkey or select ‘Manual Mode’ from the Page Menu, and press the ENT Key. The cursor may now be positioned in any field in the top right two boxes. 2) Turn the FMS Knobs to move the cursor onto the DEP TIME field and enter the desired value. Press the ENT Key. The statistics are calculated using the new value and the cursor moves to the next entry field. Repeat until all desired values have been entered. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 299 FLIGHT MANAGEMENT WEIGHT PLANNING NOTE: All weight planning page data fields displays data rounded to the nearest 10 pounds or 5 kilograms. A/C Payload Calculator Fuel Weight Calculator Empty Weight Softkey Fuel On Board Sync Softkey (sets FOB to sensor actual) - Zero Fuel Weight Calculation - Fuel on Board Entry (or sync) - Aircraft Weight Calculation - Estimated Landing Weight Calculation - Estimated Landing Fuel Calculation - Fuel Reserve Entry - Excess Fuel Calculation Basic Empty Weight Entry Pilot and Stores Weight Entry Basic Operating Weight Calculation Passenger(s) Weight Entry Cargo Weight Entry Zero Fuel Weight Calculation - (selects Basic Empty Weight) Figure 5-109 Weight Planning Page Entering basic empty weight: 1) Select the EMPTY WT Softkey; or press the MENU Key, highlight ‘Set Basic Empty Weight’, and press the ENT Key to select the ‘BASIC EMPTY WEIGHT’ field. 2) Turn the small FMS Knob to enter the basic empty weight. 3) Press the ENT Key to confirm the entry. 4) Press the FMS Knob to remove the flashing cursor. Entering a pilot and stores weight: 1) Press the FMS Knob to activate the cursor and highlight the ‘PILOT AND STORES’ field. 2) Turn the small FMS Knob to enter the pilot and stores weight. 3) Press the ENT Key to confirm the entry. 4) Press the FMS Knob to remove the flashing cursor. The basic operating weight is calculated by adding the basic empty weight and the pilot and stores weight. Entering the number of passengers: 1) Press the FMS Knob to activate the cursor and highlight the ‘PASSENGERS #’ field. 2) Turn the small FMS Knob to enter the number of passengers. 3) Press the ENT Key to confirm the entry. 4) Press the FMS Knob to remove the flashing cursor. 300 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Entering the average passenger weight: 1) Press the FMS Knob to activate the cursor and highlight the passenger weight field. 2) Turn the small FMS Knob to enter the average passenger weight. 3) Press the ENT Key to confirm the entry. 4) Press the FMS Knob to remove the flashing cursor The total weight of passengers is calculated by multiplying the number of passengers by the average passenger weight. Entering the cargo weight: 1) Press the FMS Knob to activate the cursor and highlight the ‘CARGO’ field. 2) Turn the small FMS Knob to enter the cargo weight. 3) Press the ENT Key to confirm the entry. 4) Press the FMS Knob to remove the flashing cursor The ‘ZERO FUEL WEIGHT’ is calculated by adding the basic empty, pilot and stores, passenger, and cargo weights. Entering a fuel on board weight: 1) Press the FMS Knob to activate the cursor and highlight the ‘FUEL ON BOARD’ field. 2) Turn the small FMS Knob to enter the fuel on board. 3) Press the ENT Key to confirm the entry. 4) Press the FMS Knob to remove the flashing cursor Entering fuel reserve: 1) Press the FMS Knob to activate the cursor and highlight the ‘FUEL RESERVES’ field. 2) Turn the small FMS Knob to enter the fuel reserves amount. 3) Press the ENT Key to confirm the entry. 4) Press the FMS Knob to remove the flashing cursor Synchronizing the fuel on board with the actual measured fuel on board: 190-00728-06 Rev. A Select the FOB SYNC Softkey; or select the MENU Key, highlight ‘Synchronize Fuel on Board’, and press the ENT Key. The actual measured fuel on board is displayed in the ‘FUEL ON BOARD’ field. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 301 FLIGHT MANAGEMENT When the aircraft is in the air and a destination waypoint has been entered, the fuel calculations can be completed. • Estimated landing weight = zero fuel weight + estimated landing fuel weight. • Estimated landing fuel weight = fuel on board weight - (fuel flow x ETE) • Excess fuel weight = estimated landing fuel weight - fuel reserves weight If the aircraft is on the ground or a destination waypoint has not been entered, the following fields display invalid values consisting of six dashes: • Estimated landing weight • Estimated landing fuel weight • Excess fuel weight WEIGHT CAUTION AND WARNING CONDITIONS If the estimated landing fuel weight is positive, but less than or equal to the fuel reserves weight, the following values are displayed in yellow: • Estimated fuel at landing weight • Excess fuel weight If the estimated landing fuel weight is zero or negative, then the following values are displayed in red: • Estimated fuel at landing weight • Excess fuel weight 302 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT 5.10 RAIM PREDICTION RAIM (Receiver Autonomous Integrity Monitoring) is a GPS receiver function that performs a consistency check on all tracked satellites. RAIM ensures that the available satellite geometry allows the receiver to calculate a position within a specified RAIM protection limit (2.0 nm for oceanic, 2.0 nm for enroute, 1.0 nm for terminal, and 0.3 nm for non-precision approaches). During oceanic, enroute, and terminal phases of flight, RAIM is available nearly 100% of the time. The RAIM prediction function also indicates whether RAIM is available at a specified date and time. RAIM computations predict satellite coverage within ±15 min of the specified arrival date and time. Because of the tighter protection limit on approaches, there may be times when RAIM is not available. RAIM prediction must be initiated manually if there is concern over SBAS coverage at the destination or some other reason that compromises navigation precision. If RAIM is not predicted to be available for the final approach course, the approach does not become active. If RAIM is not available when crossing the FAF, the missed approach procedure must be flown. RAIM PREDICTION Box - Prediction Waypoint - Arrival Time - Arrival Date - RAIM Status RAIM Softkey SBAS Softkey (displays SBAS Selection) (displays RAIM PREDICTION) Figure 5-110 RAIM Prediction Predicting RAIM availability at a selected waypoint: 1) Select the AUX-GPS Status Page. 2) Press the FMS Knob. The RAIM Prediction ‘WAYPOINT’ field is highlighted. 3) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway waypoints). 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 303 FLIGHT MANAGEMENT 4) Enter the identifier, facility, or city name of the departure waypoint; or select a waypoint from the submenu of waypoints and press the ENT Key to accept the waypoint entry. 5) Turn the FMS Knobs to enter an arrival time and press the ENT Key. 6) Turn the FMS Knobs to enter an arrival date and press the ENT Key. 7) Press the ENT Key with ‘COMPUTE RAIM?’ highlighted to begin the computation. Predicting RAIM availability at the aircraft present position: 1) Select the AUX-GPS Status Page. 2) Press the FMS Knob. The RAIM Prediction ‘WAYPOINT’ field is highlighted. 3) Press the MENU Key, highlight ‘Set WPT to Present Position’, and press the ENT Key. 4) Press the ENT Key to accept the waypoint entry. 5) Turn the FMS Knobs to enter an arrival time and press the ENT Key. 6) Turn the FMS Knobs to enter an arrival date and press the ENT Key. 7) Press the ENT Key with ‘COMPUTE RAIM?’ highlighted to begin the computation. Status of the RAIM computation for the selected waypoint, time, and date is displayed at the bottom of the RAIM PREDICTION Box as follows: • ‘COMPUTE RAIM?’ - RAIM has not been computed. • ‘COMPUTING AVAILABILITY’ - RAIM calculation is in progress. • ‘RAIM AVAILABLE’ - RAIM is predicted to be available. • ‘RAIM NOT AVAILABLE’ - RAIM is predicted to be unavailable. The Satellite Based Augmentation System (SBAS) provides increased navigation accuracy when available. SBAS can be enabled or disabled manually on the GPS Status Page. 304 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT SBAS Status SBAS SELECTION Box - EGNOS Enable/Disable - MSAS Enable/Disable - WAAS Enable/Disable RAIM Softkey SBAS Softkey (displays SBAS Selection) (displays RAIM PREDICTION) Figure 5-111 SBAS Display - Active Enabling/Disabling SBAS: 1) Select the AUX-GPS Status Page. 2) Select the SBAS Softkey. 3) Press the FMS Knob, and turn the large FMS Knob to highlight ‘EGNOS’, ‘MSAS’ or ‘WAAS’. 4) Press the ENT Key to disable SBAS. Press the ENT Key again to enable SBAS. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 305 FLIGHT MANAGEMENT SBAS Status SBAS SELECTION Box - EGNOS Enable/Disable - MSAS Enable/Disable - WAAS Enable/Disable RAIM Softkey SBAS Softkey (displays SBAS Selection) (displays RAIM PREDICTION) Figure 5-112 SBAS Display - Disabled 306 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT 5.11 NAVIGATING A FLIGHT PLAN The following discussion is an example of navigating a flight plan with the SBAS capable GPS system while the system provides vertical guidance through descents. A lateral flight plan (LNAV) would be navigated in much the same way, but would not include vertical guidance when the final approach course is active. NOTE: The following example flight plan is for instructional purposes only. All database information depicted should be considered not current. The example is a flight plan from KMKC to KCOS filed using the TIFTO2 departure, various Victor Airways, and the DBRY1 arrival with the transition at TBE. The flight plan includes an enroute altitude of 12,000 feet, an LPV (WAAS) approach selected for runway 35R, and a missed approach executed at the Missed Approach Point (MAP). A few enroute changes are demonstrated. 1) Prior to departure, the TIFTO2 departure, the airways, and the DBRY1 arrival at KCOS are loaded. See the Procedures section for loading departures and arrivals. Note the magenta arrow in Figure 5-113 indicating the active departure leg. After takeoff, ATC assigns a heading of 240º. 2) Figure 5-113 shows the aircraft on the assigned heading of 240º. ‘TERM’ (Terminal) is the current CDI flight phase displayed on the HSI indicating 1.0 nm CDI scaling. Figure 5-113 Assigned Heading of 240º 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 307 FLIGHT MANAGEMENT 3) ATC now assigns routing to join V4. A heading of 290º is assigned to intercept V4. The aircraft turns to heading 290° as seen in Figure 5-114. Figure 5-114 Assigned Heading of 290º 4) Enter V4 into the flight plan. a) Press the FMS Knob to activate the cursor. 308 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT b) The desired entry point for V4 (TOP) must be entered. Turn the large FMS Knob to highlight the desired flight plan insertion point (SLN) as shown in Figure 5-115. When the V4 entry point (TOP) is inserted, it is placed immediately above the highlighted waypoint (SLN). Figure 5-115 Begin Adding V4 to the Flight Plan c) Turn the small FMS Knob to display the Waypoint Information Window. Enter the desired entry point for V4, Topeka VOR (TOP), as shown in Figure 5-116. Figure 5-116 Entering V4 Entry Point 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 309 FLIGHT MANAGEMENT d) Press the ENT Key. TOP is inserted into the flight plan as in Figure 5-117. Figure 5-117 TOP Inserted into the Flight Plan e) With SLN still highlighted as in Figure 5-117, turn the small FMS Knob clockwise. The Waypoint Information Page is displayed and the LD AIRWY Softkey is now available. f) Select the LD AIRWY Softkey to display the list of available airways for TOP as seen in Figure 5-118. Figure 5-118 List of Available Airways for TOP g) Turn either FMS Knob to highlight V4 in the list as seen in Figure 5-118. 310 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT h) Press the ENT Key. The list of available exits for V4 is now displayed as in Figure 5-119. Figure 5-119 List of Available Exits for V4 i) If necessary, turn either FMS Knob to select the desired exit. In this case Salina VOR (SLN) is selected as in Figure 5-119. j) Press the ENT Key. The selected airway and exit are displayed, and the prompt “LOAD?” highlighted as in Figure 5-120. Figure 5-120 Ready to Load V4 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 311 FLIGHT MANAGEMENT k) Press the ENT Key. l) V4 is now loaded into the flight plan as shown in Figure 5-121. Figure 5-121 V4 is Loaded in the Flight Plan 5) Making V4 the active leg of the flight plan. a) Press the FMS Knob to activate the cursor. b) Turn the large FMS Knob to highlight ULNAZ. The TO waypoint of the leg is selected in order to activate the leg. c) Select the ACT LEG Softkey. The confirmation window is now displayed as in Figure 5-122. Note the TOP to ULNAZ leg is actually part of V4. Figure 5-122 Comfirm Active Leg 312 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT d) Verify the displayed leg is the desired leg and press the ENT Key. Note in Figure 5-123, the magenta arrow in the flight plan window and magenta line on the map indicating V4 is now the active flight plan leg. Note the phase of flight remained in Terminal (TERM) mode up to this point because a departure leg was active. Since a leg after the departure is now active, the current CDI flight phase is ENR (Enroute) and CDI scaling has changed to 2.0 nm. Figure 5-123 V4 Now Active Leg 6) The aircraft continues on heading 290º. When crosstrack distance is less than 2.0 nm, the XTK disappears from the HSI and the CDI is positioned on the last dot indicating a 2.0 nm distance from the centerline of the next course. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 313 FLIGHT MANAGEMENT 7) As the CDI approaches center, the aircraft turns onto the active leg as seen in Figure 5-124. Figure 5-124 Turn on to Active Leg 8) At SLN, Victor Airway 244 (V244) is intercepted. Turn prompts are displayed in the PFD Navigation Status Box as seen in Figure 5-125. Figure 5-125 Turn to Intercept V244 314 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT 9) As seen in Figure 5-126, V244 is now the active flight plan leg. Figure 5-126 V244 Now Active Leg 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 315 FLIGHT MANAGEMENT 10) At Lamar VOR (LAA) V263 is intercepted. See Figure 5-127. Figure 5-127 WIZGE to LAA Leg Active 11) ATC grants clearance to proceed direct to the OPSHN intersection to begin the arrival procedure. ATC advises to expect an altitude of 10,000 feet at OPSHN. a) Press the FMS Knob to activate the cursor. b) Turn the large FMS Knob to select OPSHN in the flight plan list. c) Press the Direct-to ( ) Key. The Direct-to Window is now displayed as shown in Figure 5-128. Figure 5-128 Direct To OPSHN 316 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT d) Turn the large FMS Knob to place the cursor in the VNV altitude field as shown in Figure 5-129. Figure 5-129 Enter VNV Altitude e) An altitude of 10,000 feet is entered as requested by ATC. f) Press the ENT Key. The cursor is now displayed in the VNV offset field as shown in Figure 5-130. Figure 5-130 Enter VNV Offset Distance g) Enter the offset, or distance from the waypoint at which to reach the selected altitude. In this case, three miles prior to OPSHN is entered. In other words, the system gives vertical guidance so the aircraft arrives at an altitude of 10,000 feet three miles prior to OPSHN. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 317 FLIGHT MANAGEMENT h) Press the ENT Key twice to activate the direct-to. Note, in Figure 5-131, the magenta arrow indicating the direct-to OPSHN after the offset waypoint for OPSHN. The preceding offset waypoint indicates the offset distance and altitude that were previously entered. The remaining waypoints in the loaded arrival procedure have no database specified altitudes, therefore, dashes are displayed. Keep the CDI centered and maintain a track along the magenta line to OPSHN. Note the Direct-to waypoint is within the loaded arrival procedure, therefore, phase of flight scaling for the CDI changes to Terminal Mode and is annunciated by displaying ‘TERM’ on the HSI. NOTE: If the loaded arrival procedure has waypoints with altitude constraints retrieved from the database that will be used as is, the altitude must be manually accepted by placing the cursor over the desired altitude, then pressing the ENT Key. The altitude is now displayed as cyan meaning it is now used by the system to determine vertical speed and deviation guidance. Figure 5-131 Direct-to Active 12) The aircraft is proceeding to OPSHN. The expected approach is the RNAV LPV approach to runway 35R, so it is selected. a) Press the PROC Key to display the Procedures Window. 318 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT b) ‘SELECT APPROACH’ should be highlighted as shown in Figure 5-132. Figure 5-132 Procedures Window c) Press the ENT Key. A list of available approaches for the destination airport is displayed as in Figure 5-133. Figure 5-133 List of Available Approaches d) Turn either FMS Knob to select the LPV approach for 35R as shown in Figure 5-133. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 319 FLIGHT MANAGEMENT e) Press the ENT Key. A list of available transitions for the selected approach is displayed as in Figure 5-134. Figure 5-134 List of Available Transitions f) Turn either FMS Knob to select the desired transition. In this case, the Initial Approach Fix (IAF) at HABUK is used. g) Press the ENT Key. h) Barometric Minimums To set ‘MINIMUMS’, turn the small FMS Knob to select ‘BARO’, and press the ENT Key. Turn the small FMS Knob to select the altitude, and press the ENT Key. Or: To skip setting minimums, press the ENT Key. 320 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT Figure 5-135 Barometric Minimums Set i) With ‘LOAD?’ highlighted, again press the ENT Key. The selected approach is added to the flight plan as seen in Figure 5-136. Figure 5-136 Loaded Approach 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 321 FLIGHT MANAGEMENT 13) Note the altitude constraints associated with each of the approach waypoints as seen in Figure 5-137. These altitudes are loaded from the database and are displayed as cyan text, indicating these values are “designated” for use in computing vertical deviation guidance. Note: To no longer use the displayed altitude for calculating vertical deviation guidance, perform the following: a) Press the FMS Knob to activate the cursor. b) Turn the small FMS Knob to highlight the desired altitude. c) Press the CLR Key. d) Press the FMS Knob to deactivate the cursor. After making the altitude “non-designated”, it is displayed as white text. Altitude constraint values associated with the Final Approach Fix (FAF) and waypoints beyond the FAF cannot be designated for vertical guidance. These altitude values are always displayed as white text, as in Figure 5-137. Vertical guidance from the FAF and on to the Missed Approach Point (MAP) is given using the WAAS GPS altitude source, therefore, the displayed altitude values are for reference only. Figure 5-137 Vertical Guidance is Active to the FAF 322 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT 14) As the aircraft approaches OPSHN, it may be desirable to adjust the speed, or steepness of the upcoming descent. The default Flight Path Angle (FPA) is -3.0 degrees and a required vertical speed is computed to maintain the -3.0 FPA. To change the vertical flight path, perform the following steps. a) Select the VNV PROF Softkey to place the cursor in the target vertical speed field (VS TGT) as shown in Figure 5-138. b) At this point, the descent vertical speed can be selected, or the FPA can be selected. Turn the large FMS Knob to select the desired selection field, then turn the small FMS Knob to enter the desired value. Note the information now displayed in the ‘CURRENT VNV PROFILE’ box. Also, note the offset waypoint (orange box) and gray circle are now displayed on the map. The gray circle marks the Top of Descent (TOD). In this example, vertical guidance is provided at the TOD that results in a -3.0 degree FPA descent to an altitude of 10,000 feet upon reaching the offset waypoint. Figure 5-138 Adjusting the Descent c) Press the ENT Key. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 323 FLIGHT MANAGEMENT 15) As seen in Figure 5-139, the aircraft is approaching TOD. Note the target vertical speed required to reached the selected altitude. The Vertical Deviation Indicator (VDI) and the Required Vertical Speed Indicator (RVSI) are now displayed on the PFD as shown in Figure 5-140. When the aircraft is within one minute of the TOD, it is annunciated as shown in Figure 5-140, and an aural alert ‘Vertical track’ will be heard. Figure 5-139 Approaching Top of Descent (TOD) Target Altitude Vertical Deviation Indicator (VDI) Required Vertical Speed Indicator (RVSI) Figure 5-140 VDI & RVSI When Approaching Top of Descent (TOD) 324 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT 16) Upon reaching TOD, a descent vertical speed is established by placing the VSI pointer in line with the RVSI as shown in Figure 5-141. Keep Vertical Deviation Indicator Centered Align Actual Vertical Speed with Required Vertical Speed Figure 5-141 VDI & RVSI Showing Correctly Established Descent 17) When the aircraft is one minute from the bottom of descent (BOD) it is annunciated as shown in Figure 5-142. Upon reaching the offset waypoint for OPSHN, the aircraft is at 10,000 feet. Figure 5-142 Approaching Bottom of Descent (BOD) at OPSHN Offset Waypoint 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 325 FLIGHT MANAGEMENT 18) The aircraft is approaching OPSHN. The upcoming turn and next heading are annunciated at the top left of the PFD as seen in Figure 5-143. Initiate the turn and maneuver the aircraft on a track through the turn radius to intercept the magenta line for the OPSHN to FSHER leg and center the CDI. Figure 5-143 Turn to intercept OPSHN to FSHER Leg 326 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT 19) After passing OPSHN, the next leg of the arrival turns magenta as shown in Figure 5-144. The magenta arrow in the flight plan list now indicates the OPSHN to FSHER leg of the arrival procedure is now active. Figure 5-144 Tracking the OPSHN to FSHER Leg 20) The flight continues through the arrival procedure to PYNON (see Figure 5-145). At a point 31 nm from the destination airport, the phase of flight scaling for the CDI changes to Terminal Mode and is annunciated by displaying ‘TERM’ on the HSI. A descent to HABUK is in the next leg. Note the TOD point on the map. Annunciations for the upcoming turn and descent, as well as the VDI and RVSI, appear on the PFD as the flight progresses. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 327 FLIGHT MANAGEMENT Figure 5-145 Approaching PYNON 328 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT 21) Upon passing PYNON the approach procedure automatically becomes active. The approach may be activated at any point to proceed directly to the IAF. In this example, the aircraft has progressed through the final waypoint of the arrival and the flight plan has automatically sequenced to the IAF as the active leg, activating the approach procedure (see Figure 5-146). Figure 5-146 Approach is Now Active Note: To manually activate the approach procedure, perform the following steps: a) Press the PROC Key. b) Turn the large FMS Knob to highlight ‘ACTIVATE APPROACH’ as shown in Figure 5-147. c) Press the ENT Key to activate the approach. Figure 5-147 Manually Activate Approach 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 329 FLIGHT MANAGEMENT 22) The IAF is the next waypoint. At the TOD, establish a descent vertical speed as previously discussed in Step 16. The aircraft altitude is 9,000 feet upon reaching HABUK. Figure 5-148 Descending Turn to the Initial Approach Fix (IAF) 330 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT 23) After crossing FALUR the next waypoint is the FAF. The flight phase changes to LPV on the HSI indicating the current phase of flight is in Approach Mode and the approach type is LPV. CDI scaling changes accordingly and is used much like a localizer when flying an ILS approach. The RVSI is no longer displayed and the VDI changes to the Glidepath Indicator (as shown in Figure 5-149) when the final approach course becomes active. Figure 5-149 Descending to the FAF The descent continues through the FAF (CEGIX) using the Glidepath Indicator, as one would use a glideslope indicator, to obtain an altitude “AT” 7,800 feet at the FAF. Note the altitude restriction lines over and under (At) the altitude in the ‘ALT’ field in Figure 5-149. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 331 FLIGHT MANAGEMENT 24) After crossing CEGIX, the aircraft continues following the glidepath to maintain the descent to “AT or ABOVE” 6,370 feet at the Missed Approach Point (MAP) (RW35R) as seen in Figure 5-150. Figure 5-150 Descending to the Missed Approach Point In this missed approach procedure, the altitude immediately following the MAP (in this case ‘6368ft’) is not part of the published procedure. It is simply a Course to Altitude (CA) leg which guides the aircraft along the runway centerline until the altitude required to safely make the first turn toward the MAHP is exceeded. This altitude is provided by the navigation database, and may be below, equal to, or above the published minimums for this approach. In this case, if the aircraft altitude is below the specified altitude (6,368 feet) after crossing the MAP, a direct-to is established to provide a course on runway heading until an altitude of 6,368 feet is reached. After reaching 6,368 feet, a direct-to is established to the published MAHP (in this case MOGAL). If the aircraft altitude is above the specified altitude after crossing the MAP, a direct-to is established to the published fix (MOGAL) to begin the missed approach procedure. In some missed approach procedures this Course to Altitude leg may be part of the published procedure. For example, a procedure may dictate a climb to 5,500 feet, then turn left and proceed to the Missed Approach Hold Point (MAHP). In this case, the altitude would appear in the list of waypoints as ‘5500ft’. Again, if the aircraft altitude is lower than the prescribed altitude, a direct-to is established on a Course to Altitude leg when the missed approach procedure is activated. 332 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT 25) Upon reaching the MAP, it is decided to execute a missed approach. Automatic waypoint sequencing is suspended past the MAP. Press the SUSP Softkey on the PFD to resume automatic waypoint sequencing through the missed approach procedure. A direct-to is initiated to MOGAL, which is the Missed Approach Hold Point (MAHP) as seen in Figure 5-151. The aircraft is climbing to 10,000 feet. The CDI flight phase now changes from LPV to MAPR as seen on the HSI. Figure 5-151 Missed Approach Active 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 333 FLIGHT MANAGEMENT 26) The aircraft continues climbing to “AT or ABOVE” 10,000 feet at MOGAL. A holding pattern is established at the MAHP (MOGAL) as shown in Figure 5-152. Figure 5-152 Establishing the Holding Pattern 27) The aircraft maintains 10,000 feet while following the magenta line through the hold as in Figure 5-153. Figure 5-153 Hold Established 334 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A FLIGHT MANAGEMENT 5.12 ABNORMAL OPERATION This section discusses the Dead Reckoning mode of operation and the subsequent indications. NOTE: Dead Reckoning Mode only functions in Enroute (ENR) or Oceanic (OCN) phase of flight. In all other phases, an invalid GPS solution produces a “NO GPS POSITION” annunciation on the map and the system stops using GPS. While in Enroute or Oceanic phase of flight, if the system detects an invalid GPS solution or is unable to calculate a GPS position, the system automatically reverts to Dead Reckoning (DR) Mode. In DR Mode, the system uses its last-known position combined with continuously updated airspeed and heading data (when available) to calculate and display the aircraft’s current estimated position. It is important to note that estimated navigation data supplied by the system in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation. If while in DR Mode airspeed and/or heading data is also lost or not available, the DR function may not be capable of accurately tracking estimated position and, consequently, the system may display a path that is different than the actual movement of the aircraft. Estimated position information displayed through DR while there is no heading and/or airspeed data available should not be used for navigation. DR Mode is inherently less accurate than the standard GPS/SBAS Mode due to the lack of satellite measurements needed to determine a position. Changes in wind speed and/or wind direction compound the relative inaccuracy of DR Mode. Because of this degraded accuracy, other navigation equipment must be relied upon for position awareness until GPS-derived position data is restored. DR Mode is indicated by the appearance of the letters ‘DR’ superimposed in yellow over the ‘own aircraft’ symbol as shown in Figure 5-154. In addition, ‘DR’ is prominently displayed in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in Figure 5-154. Also, the CDI deviation bar is removed from the display. Lastly, but at the same time, a ‘GPS NAV LOST’ alert message appears on the PFD. Normal navigation using GPS/SBAS source data resumes automatically once a valid GPS solution is restored. As a result of operating in DR Mode, all GPS-derived data is computed based upon an estimated position and is displayed as yellow text on the display to denote degraded navigation source information as shown in Figure 5-154. Also, while the system is in DR Mode, the autopilot does not couple to GPS, and TAWS is disabled. Additionally, the accuracy of all nearest information (airports, airspaces, and waypoints) is questionable. Finally, airspace alerts continue to function, but with degraded accuracy. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 335 FLIGHT MANAGEMENT Distance & Bearing Ground Speedr Dead Reckoning Annunciaion Wind Data GPS Navigation Lost Message Current Track Indicator Bearing Pointer/ Distance Navigation Data Bar Wind Data All data except Active Leg, TAS, and DTK are in yellow Dead Reckoning Annunciation Subdued Aircraft Symbol Figure 5-154 Dead Reckoning Mode - GPS Derived Data Shown in Yellow NOTE: The Inset Map is removed from the PFD any time aircraft pitch is greater than +30° or less than –20°, or when a 65° bank angle is reached. 336 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE SECTION 6 HAZARD AVOIDANCE Hazard avoidance features available for the Prodigy® Flight Deck 100 are designed to aid situational awareness and provide advisory information with regard to potential hazards to flight safety associated with weather, terrain, and air traffic. Weather • GDL 69A SiriusXM Weather (Subscription Optional) • GSR 56 Garmin Connext Weather (Subscription Optional) • GWX 68 Airborne Color Weather Radar (Optional) Terrain Avoidance • Terrain Awareness and Warning System - Class B (TAWS-B) • Terrain Awareness and Warning System - Class A (TAWS-A) (Optional) Traffic • Traffic Information Service (TIS) • Garmin GTS 850 Traffic Alert and Collision Avoidance System I (TCAS I) (Optional) • ACSS TCAS 3000SP™ Traffic Alert and Collision and Avoidance System II (TCAS II) (Optional) 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 337 HAZARD AVOIDANCE 6.1 SIRIUSXM WEATHER WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous weather. Information contained within data link weather products may not accurately depict current weather conditions. WARNING: Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather product. Due to time delays inherent in gathering and processing weather data for data link transmission, the weather information shown by the data link weather product may be significantly older than the indicated weather product age. The GDL 69A is a remote-mounted satellite data link receiver which provides SiriusXM Weather information. The system shows received graphical weather information and associated text on the Multi Function Display (MFD) and the Primary Flight Display (PFD) Inset Map. The GDL 69A can also receive SiriusXM Satellite Radio entertainment services. Both weather data and audio entertainment programming operate in the S-band frequency range to provide continuous reception capabilities at any altitude throughout North America. Both services are subscription-based. For more information on specific service packages, visit www.siriusxm. com. ACTIVATING SERVICES Before SiriusXM Weather can be used, the service must be activated. Service is activated by providing SiriusXM with coded IDs unique to the installed GDL 69A. SiriusXM Satellite Radio (audio) and SiriusXM Weather (data) services each have coded IDs. The Data and Audio Radio IDs must be provided to SiriusXM to activate the weather service and entertainment subscriptions, respectively. These IDs are located on: • The XM Information Page on the MFD (Figure 6-1) • The XM Satellite Radio Activation Instructions included with the GDL 69A. • The label on the back of the Data Link Receiver Contact the installer if the Audio and Data Radio IDs cannot be located. SiriusXM uses the coded IDs to send an activation signal that allows the system to provide weather data and/ or audio entertainment programming provided through the GDL 69A. Establishing an account for SiriusXM services: 1) Select the XM Page in the Auxiliary Page Group. 2) Select the INFO Softkey to display the AUX - XM Information Page. 3) Note the Data Radio ID (for SiriusXM Weather) and/or the Audio Radio ID (for SiriusXM Satellite Radio). 4) Contact SiriusXM customer service through the phone number listed on its website. 5) Provide SiriusXM customer service the Data Radio ID and/or Audio Radio ID, in addition to payment information, and desired weather product subscription package. 338 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Activating the SiriusXM Weather service: 1) Once a SiriusXM Weather account has been established, select the XM Page in the Auxiliary Page Group. 2) Select the INFO Softkey to display the XM Information Page. 3) Observe the list of Weather Products. A white empty box appears next to an unavailable weather product; a green filled box appears next to an available weather product. During activation, it may take several minutes for weather products in the chosen subscription package to become available. 4) When the available weather products displayed match the weather products offered in the chosen SiriusXM Weather product subscription package, press the LOCK Softkey. 5) Turn the large FMS Knob to highlight ‘YES’. 6) To complete activation, press the ENT Key. Data Radio ID (for SiriusXM Weather) Audio Radio ID (for SiriusXM Satellite Radio) Weather Products (Available Products for Service Class Indicated in Green) Select to Display XM Information page Figure 6-1 XM Information Page Select to Lock Subscription Information USING SIRIUSXM WEATHER PRODUCTS The principal map page for viewing SiriusXM Weather data is the Weather Data Link (XM) Page in the Map Page Group. This is the only map display capable of showing information for all available SiriusXM Weather products. Viewing the Weather Data Link (XM) Page: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Weather Data Link (XM or CNXT) Page. 3) If the page title contains ‘CNXT’, it will be necessary to change the data link weather source from Garmin Connext to SiriusXM Weather. Refer to the next procedure to change the source. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 339 HAZARD AVOIDANCE Changing the weather data link source (SiriusXM or Garmin Connext): 1) If necessary, turn the large FMS Knob to select the Map Page Group. 2) If necessary, turn the small FMS Knob to select the Weather Data Link (XM or CNXT) Page. 3) Press the MENU Key. 4) If necessary, turn the large FMS Knob to highlight ‘Display XM Weather’ or ‘Display Connext Weather’ and press the ENT Key. Weather Data Link Page title and softkeys change to correspond to selected data link weather source. NEXRAD Weather Product Symbol and Product Ages (U.S. and Canada) NEXRAD Weather Product Selected for Display Figure 6-2 Weather Data Link (XM) Page For each enabled SiriusXM Weather product, the system displays a weather product icon and product age. The product age is the elapsed time (in minutes) since the weather data provider compiled the weather product. The product age display does not indicate the age of the information contained within the weather product, which can be significantly older than the displayed weather product age. The SiriusXM Weather service broadcasts weather products at specific intervals (defined in the Broadcast Rate column in Table 6-1). If for any reason, a product is not broadcast within the Expiration Time intervals (see Table 6-1), the system removes the expired data from the display, and shows dashes instead of the product age. This ensures the displayed information is consistent with what is currently being transmitted by the SiriusXM Weather service. If more than half of the expiration time has elapsed, the color of the product age changes to yellow. If data for a weather product is not available, the system displays ‘N/A’ next to the weather product symbol instead of the product age. Table 6-1 shows the weather product symbols, the expiration times and the broadcast rates. The broadcast rate represents the interval at which the SiriusXM Weather service transmits new signals that may or may not contain updated weather products. It does not represent the rate at which the weather information is updated 340 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE or when the Data Link Receiver receives new data. SiriusXM and its weather data suppliers define and control the data update intervals, which are subject to change. SiriusXM Weather Product Product Symbol Next-generation Radar (NEXRAD) Expiration Time Broadcast Rate (Minutes) (Minutes) 5 (U.S.) 30 10 (Canada) Cloud Top (CLD TOP) 60 15 Echo Top (ECHO TOP) 30 7.5 SiriusXM Lightning (XM LTNG) 30 5 Cell Movement (CELL MOV) 30 12 SIGMETs/AIRMETs (SIG/AIR) 60 12 Meteorological Aerodrome Report (METARs) 90 12 City Forecast (CITY) 90 12 Surface Analysis (SFC) 60 12 Freezing Levels (FRZ LVL) 120 12 Winds Aloft (WIND) 90 12 County Warnings (COUNTY) 60 5 Cyclone Warnings (CYCLONE) 60 12 Icing Potential (CIP and SLD) (ICNG) 90 22 Pilot Weather Report (PIREPs) 90 12 Air Report (AIREPs) 90 12 Turbulence (TURB) 180 12 No Radar Coverage no product image 30 5 Temporary Flight Restrictions (TFRs) Terminal Aerodrome Reports (TAFs) no product image no product image 60 60 12 12 Table 6-1 SiriusXM Weather Product Symbols and Data Timing 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 341 HAZARD AVOIDANCE Navigation Map Page Weather Data Link (XM) Page AUX - Trip Planning Page SYS Page Group Nearest Page Group Flight Plan Pages NEXRAD + + + + + + + No Radar Coverage + + + + + + + SiriusXM Weather Product Cloud Top (CLD TOP) + Echo Top (ECHO TOP) + Weather Information Page PFD Inset Map Table 6-2 shows which SiriusXM Weather products can be displayed (indicated with a ‘+’ symbol) on specific maps. SiriusXM Lightning (XM LTNG) + + + + + + + Cell Movement (CELL MOV) + + + + + + + + + + + + + + + + + + + + SIGMETs/AIRMETs (SIG/AIR) METAR + + + + City Forecast (CITY) + Surface Analysis (SFC) + Freezing Levels (FRZ LVL) + Winds Aloft (WIND) +* + County Warnings (COUNTY) + Cyclone Warnings (CYCLONE) + Icing Potential (ICNG) + PIREPs + AIREPs + Turbulence (TURB) + TFRs TAFs + + * Winds Aloft data on the Navigation Map Page available inside the Profile View Window. Table 6-2 SiriusXM Weather Product Display Maps 342 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Softkeys control the display of weather information on most MFD pages and the PFD Inset Map (Figure 6-3 shows the weather product softkeys for the Weather Data Link (XM) Page). When a weather product is selected for display, the corresponding softkey label changes to gray to indicate the product is enabled. SYSTEM CPDLC NEXRAD ECHO TOP CLD TOP XM LTNG CELL MOV CYCLONE SFC OFF FRZ LVL SIG/AIR METAR LEGEND MORE WX CHKLIST WIND OFF ICNG OFF TURB OFF AIREPS PIREPS COUNTY BACK SFC Softkey label changes to reflect current selection. WIND/ICNG/TURB Softkey labels change to reflect current selection. CURRENT OFF 12 HR 24 HR 36 HR 48 HR Select the BACK Softkey to move up one level. LEGEND BACK PREV and NEXT Softkeys cycle through Winds Aloft, Icing, and Turbulence altitude selection softkeys. PREV OFF SFC 3000 6000 9000 12000 15000 NEXT LEGEND BACK PREV OFF 18000 21000 24000 27000 30000 33000 NEXT LEGEND BACK PREV OFF 36000 39000 42000 NEXT LEGEND BACK PREV OFF 1000 3000 6000 9000 12000 NEXT LEGEND BACK PREV OFF 18000 21000 24000 27000 30000 NEXT LEGEND BACK PREV OFF 21000 24000 27000 30000 33000 NEXT LEGEND BACK PREV OFF 39000 42000 45000 NEXT LEGEND BACK 15000 36000 Figure 6-3 Weather Data Link (XM) Page Weather Product Softkeys Displaying SiriusXM Weather products on the PFD Inset Map: 1) On the PFD, press the INSET Softkey (in non-TCAS II installations) or the TRFC/MAP Softkey (TCAS II installations). 2) If the PFD Inset Map is showing the traffic map, press the TFRC-2 Softkey to display the navigation map. 3) Press the desired weather product softkey(s) to enable/disable the display of SiriusXM Weather products on the Inset Map. 4) To display or remove the weather product icon and age box for displayed weather products on the inset map, press the WX LGND Softkey. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 343 HAZARD AVOIDANCE The setup menus for the Navigation Map Page and the Weather Data Link (XM) Page control the map range settings above which weather products data are decluttered from the display. If a map range larger than the weather product map range setting is selected, the weather product data is removed from the map. The menus also provide the ability to enable/disable the display of weather products, and provide the equivalent to using the softkeys. Setting up and customizing the Weather Data Link (XM) Page: 1) Select the Weather Data Link (XM) Page. 2) Press the MENU Key. 3) With ‘Weather Setup’ highlighted, press the ENT Key (Figure 6-4). 4) Turn the small FMS Knob to select ‘PRODUCT GROUP 1’ or ‘PRODUCT GROUP 2’, and press the ENT Key (Figure 6-5). 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections. 6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, maximum map range settings, etc.). 7) Press the ENT Key to select an option. 8) Press the FMS Knob or CLR Key to return to the Weather Data Link (XM) Page with the changed settings. Figure 6-4 Weather Data Link (XM) Page Menu Figure 6-5 Weather Data Link (XM) Page Setup Menu 344 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Restoring default Weather Data Link (XM) Page settings: 1) Select the Weather Data Link (XM) Page. 2) Press the MENU Key. 3) With ‘Weather Setup’ highlighted, press the ENT Key. 4) Press the MENU Key. 5) Highlight the desired default(s) to restore (all or for selection) and press ENT Key. Maps besides the Weather Data Link (XM) Page use settings based on those selected for the Navigation Map Page. Setting up and customizing weather data for the Navigation Map Page: 1) Select the Navigation Map Page. 2) Press the MENU Key. 3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-6). 4) Turn the small FMS Knob to select the ‘Weather’ Group and press the ENT Key (Figure 6-7). 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-8). 6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, maximum map range settings). 7) Press the ENT Key to select an option. 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. Figure 6-6 Navigation Map Page Menu Figure 6-7 Navigation Map Page Setup Menu 190-00728-06 Rev. A Figure 6-8 Navigation Map Page Setup Menu, Weather Group Embraer Prodigy® Flight Deck 100 Pilot’s Guide 345 HAZARD AVOIDANCE If multiple data link weather services are installed, surch as the optional GSR 56 Garmin Connext Weather service, customizing the display settings for the corresponding weather products shown in Table 6-3 will result in identical settings for a comparable weather product from another service provider. Garmin Connext Weather Product (CNXT) Precipitation Next-generation Radar (NEXRAD) (PRECIP) Cloud Top Infrared Satellite (CLD TOP) (IR SAT) SiriusXM Lightning Garmin Connext Data Link Lightning (DL LTNG) (XM LTNG) SIGMETs/AIRMETs SIGMETs/AIRMETs (SIG/AIR) (SIG/AIR) Meteorological Aerodrome Report Meteorological Aerodrome Report (METARs) (METARs) Winds Aloft Winds Aloft (WIND) (WIND) Pilot Weather Report Pilot Weather Report (PIREPs) (PIREPs) SiriusXM Weather Product Table 6-3 Corresponding Weather Data Link Product Settings Each active weather product has an associated legend which can be displayed on the Weather Data Link (XM) Page and on most MFD pages displaying a navigation map. Viewing legends for displayed weather products (on the Weather Data Link (XM) Page): 1) Select the Weather Data Link (XM) Page. 2) Select the LEGEND Softkey to display the legends for the displayed weather products. Or: a) Press the MENU Key. b) Select ‘Weather Legend’ and press the ENT Key. 3) Turn the FMS Knob to scroll through the legends if more are available than fit in the window. 4) To remove the XM Weather Legends Window, select the LEGEND Softkey, or press the ENT or the CLR Keys, or press the FMS Knob. Viewing legends for displayed weather products (on the Navigation Map Page): 1) Select the Navigation Map Page. 2) Select the MAP Softkey. 3) Select the LEGEND Softkey (available if one or more SiriusXM Weather products are enabled for display). 4) To remove the Legend Window, select the LEGEND Softkey, or press the ENT or the CLR Keys, or press the FMS Knob. 346 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Additional information about the following can be displayed by panning over the display on the map: • Echo Tops • METARs • Cloud Tops • County Warnings • Cell Movement • TFRs • SIGMETs • AIREPs • AIRMETs • PIREPs The map panning feature is enabled by pressing the Joystick. The map range is adjusted by turning the Joystick. If the map range is adjusted while panning is enabled, the map is re-centered on the Map Pointer. Additional Information on Weather Feature Selected with Map Pointer Flash Flood Warning Selected with Map Pointer Figure 6-9 Panning on the Weather Data Link (XM) Page NEXRAD NOTE: NEXRAD cannot be displayed simultaneously with terrain, echo tops, turbulence, or airborne weather radar data on the same map. The National Weather Service (NWS) operates the WSR-88D, or NEXRAD (NEXt-generation RADar) system, an extensive network of 156 high-resolution Doppler radar systems. The NEXRAD network provides centralized meteorological information for the continental United States and selected overseas locations. The maximum range of a single NEXRAD site is 250 nm. Individual NEXRAD sites supply the network with radar images, and the images from each radar site may arrive at the network at different rates and times. Periodically, the weather data provider compiles the available individual site images from the network to form a composite image, and assigns a single time to indicate when 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 347 HAZARD AVOIDANCE it created the image. This image becomes the NEXRAD weather product. Individual images--gathered from each NEXRAD site--differ in age, and are always older than the displayed NEXRAD weather product age. The data provider then sends the NEXRAD data to the SiriusXM Weather service, whose satellites transmit this information during the next designated refresh time for the NEXRAD weather product. Because of the time required to detect, assemble, and distribute the NEXRAD weather product, the displayed weather information contained within the product may be significantly older than the current radar synopsis and may not depict the current weather conditions. The NEXRAD weather product should never be used as a basis for maneuvering in, near, or around areas of hazardous weather regardless of the information it contains. Figure 6-10 NEXRAD Data on the Weather Data Link (XM) Page Displaying NEXRAD weather information: 1) Select the MAP Softkey. This step is not applicable on the Weather Data Link (XM) Page. 2) Select the NEXRAD Softkey. Composite data from all the NEXRAD radar sites in the United States is shown. This data is composed of the maximum reflectivity from the individual radar sweeps. The display of the information is color-coded to indicate the weather severity level. All weather product legends can be viewed on the Weather Data Link (XM) Page. For the NEXRAD legend (Figure 6-11), select the LEGEND Softkey when NEXRAD is selected for display. 348 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE No Radar Coverage Figure 6-11 NEXRAD Legend The display of no radar coverage is always active when either NEXRAD or Echo Tops is enabled. Areas where NEXRAD radar coverage and Echo Tops information are not currently available or are not being collected are indicated in gray shade of purple. Reflectivity Reflectivity is the amount of transmitted power returned to the radar receiver. Colors on the NEXRAD display are directly correlative to the level of detected reflectivity. Reflectivity as it relates to hazardous weather can be very complex. The role of radar is essentially to detect moisture in the atmosphere. Simply put, certain types of weather reflect radar better than others. The intensity of a radar reflection is not necessarily an indication of the weather hazard level. For instance, wet hail returns a strong radar reflection, while dry hail does not. Both wet and dry hail can be extremely hazardous. The different NEXRAD echo intensities are measured in decibels (dB) relative to reflectivity (Z). NEXRAD measures the radar reflectivity ratio, or the energy reflected back to the radar receiver (designated by the letter Z). The value of Z increases as the returned signal strength increases. NEXRAD Limitations NEXRAD radar images may have certain limitations: • NEXRAD base reflectivity does not provide sufficient information to determine cloud layers or precipitation characteristics (wet hail vs. rain). For example, it is not possible to distinguish between wet snow, wet hail, and rain. • NEXRAD base reflectivity is sampled at the minimum antenna elevation angle. An individual NEXRAD site cannot depict high altitude storms at close ranges. It has no information about storms directly over the site. • When zoomed in to a range of 30 nm, each square block on the display represents an area of four square kilometers. The intensity level reflected by each square represents the highest level of NEXRAD data sampled within the area (Figure 6-12). • Below 52ºN, if the type of precipitation is unavailable, the system displays the precipitation using the color codes associated with rain. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 349 HAZARD AVOIDANCE Block Area is 4 km2 Figure 6-12 NEXRAD Data - Zoomed The following may cause abnormalities in displayed NEXRAD radar images: • Ground clutter • Strobes and spurious radar data • Sun strobes (when the radar antenna points directly at the sun) • Interference from buildings or mountains, which may cause shadows • Metallic dust (chaff) from military aircraft, which can cause alterations in radar scans 350 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE NEXRAD Limitations (Canada) • Radar coverage extends to 55ºN. • Any precipitation displayed between 52ºN and 55ºN is displayed as mixed regardless of actual precipitation type. • Below 52ºN, if the type of precipitation is unavailable, the system displays the precipitation using the color codes associated with rain. No Coverage Above 55ºN Precipitation Above 52ºN Displays as Mixed Figure 6-13 NEXRAD Data - Canada 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 351 HAZARD AVOIDANCE ECHO TOPS NOTE: Echo Tops cannot be displayed at the same time as Cloud Tops or NEXRAD data on the Weather Data Link (XM) Page. The Echo Tops weather product (Figure 6-14) shows the location, elevation, and direction of the highest radar echo. The highest radar echo does not indicate the top of a storm or clouds; rather it indicates the highest altitude at which precipitation is detected. Information is derived from NEXRAD data. Figure 6-14 Echo Tops Weather Product Displaying Echo Tops information: 1) Select the Weather Data Link (XM) Page. 2) Select the ECHO TOP Softkey. To display the Echo Tops legend (Figure 6-15), select the LEGEND Softkey when Echo Tops is selected for display. Since Echo Tops and Cloud Tops use the same color scaling to represent altitude, display of these weather products is mutually exclusive. When Echo Tops is enabled on the Weather Data Link (XM) Page, the system disables the NEXRAD and Cloud Tops weather products. No Radar Coverage Figure 6-15 Echo Tops Legend 352 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE The display of No Radar Coverage is always active when either NEXRAD or Echo Tops is enabled. Areas where NEXRAD radar coverage and Echo Tops information is not currently available or is not being collected are indicated in gray shade of purple. CLOUD TOPS NOTE: Cloud Tops and Echo Tops cannot be displayed at the same time on the Weather Data Link (XM) Page. The Cloud Tops weather product (Figure 6-16) depicts cloud top altitudes as determined from satellite imagery. Figure 6-16 Cloud Tops Weather Product Displaying Cloud Tops information: 1) Select the Weather Data Link (XM) Page. 2) Select the CLD TOP Softkey. To display the Cloud Tops legend (Figure 6-17), select the LEGEND Softkey when Cloud Tops is selected for display. Since Cloud Tops and Echo Tops use the same color scaling to represent altitude, display of these weather products is mutually exclusive. When Cloud Tops is activated on the Weather Data Link (XM) Page, the system disables the Echo Tops weather product. Figure 6-17 Cloud Tops Legend 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 353 HAZARD AVOIDANCE SIRIUSXM LIGHTNING The SiriusXM Lightning weather product (Figure 6-18) shows the approximate location of cloud-to-ground lightning strikes. A strike icon represents a strike that has occurred within a two-kilometer region. The exact location of the lightning strike is not displayed. Lightning Strikes Figure 6-18 SiriusXM Lightning Weather Product Displaying SiriusXM Lightning information: 1) Select the MAP Softkey. This step is not necessary on the Weather Data Link (XM) Page. 2) Select the XM LTNG Softkey. To display the SiriusXM Lightning legend on the Weather Data Link (XM) Page (Figure 6-19), select the LEGEND Softkey when SiriusXM Lightning is selected for display. Figure 6-19 Lightning Legend 354 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE CELL MOVEMENT The Cell Movement weather product (Figure 6-20) shows the location and movement of storm cells as identified by the ground-based system. Cells are represented by yellow squares, with direction of movement indicated with short, orange arrows. Storm Cells Figure 6-20 Cell Movement Weather Product On most applicable maps, Cell Movement appears when the NEXRAD weather product is enabled. On the Weather Data Link (XM) Page, Cell Movement data can be selected independently from NEXRAD. Cell Movement data can be displayed on the following maps: • PFD Inset Map • AUX - Trip Planning Page • Navigation Map • Nearest Pages Displaying Cell Movement information: 1) Select the MAP Softkey. This step is not necessary on the Weather Data Link (XM) Page. 2) Select the NEXRAD Softkey (CEL MOV Softkey on the Weather Data Link (XM) Page). For Cell Movement to be displayed on maps other than the Weather Data Link (XM) Page, Cell Movement must be enabled in the Navigation Map Setup Menu (see the procedure ‘Setting up and customizing weather data for the Navigation Map Page’). To display the Cell Movement legend on the Weather Data Link (XM) Page, (Figure 6-21), select the LEGEND Softkey when Cell Movement is selected for display. Figure 6-21 Cell Movement Legend 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 355 HAZARD AVOIDANCE SIGMETS AND AIRMETS The National Weather Service (NWS) issues SIGMETs (SIGnificant METeorological Information) and AIRMETs (AIRmen’s METeorological Information) for potentially hazardous weather. The NWS issues Convective SIGMETs for hazardous convective weather such as severe or widespread thunderstorms. A localized SIGMET indicates a SIGMET affecting a small geographic area. AIRMET IFR AIRMET Turbulence Figure 6-22 SIGMET/AIRMET Data Displaying SIGMETs and AIRMETs: 1) Select the Weather Data Link (XM) Page. 2) Select the SIG/AIR Softkey. 3) To view the text of the SIGMET or AIRMET, press the Joystick and move the Map Pointer over the icon. 4) Press the ENT key. Figure 6-23 shows sample SIGMET text. To display the SIGMET and AIRMET legend (Figure 6-24), select the LEGEND Softkey when SIGMETs and AIRMETs are selected for display. Figure 6-23 Sample SIGMET Text 356 Figure 6-24 SIGMET/AIRMET Legend Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE METARS AND TAFS NOTE: Atmospheric pressure as reported for METARs is given in hectopascals (hPa), except for in the United States, where it is reported in inches of mercury (in Hg). Temperatures are reported in Celsius. NOTE: METAR information is only displayed within the installed navigation database service area. METARs (METeorological Aerodrome Reports) typically contain information about the temperature, dewpoint, wind, precipitation, cloud cover, cloud base heights, visibility, and barometric pressure at an airport or observation station. They can also contain information on precipitation amounts, lightning, and other critical data. METARs reflect hourly observations; non-routine updates include the code “SPECI” in the report. METARs are shown as colored flags at airports that provide them. Instructions for Viewing METAR and TAF Text Selected Airport Figure 6-25 METAR Flags on the Weather Data Link (XM) Page TAFs (Terminal Aerodrome Forecasts) are weather predictions for specific airports within a 24- hour period, and may span up to 36 hours. TAFs typically include forecast wind, visibility, weather phenomena, and sky conditions using METAR codes. METAR and TAF text are displayed on the Weather Information Page. METAR data is displayed first in a decoded fashion, followed by its original text. The original text may contain information not found in the decoded version. The system displays TAF information only in its original form, when a TAF is available. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 357 HAZARD AVOIDANCE Displaying METAR and TAF text: 1) On the Weather Data Link (XM) Page, select the METAR Softkey. 2) Press the Joystick and pan to the desired airport. 3) Press the ENT Key. The Weather Information Page is shown with METAR and TAF text. 4) Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text. METAR text must be completely scrolled through before scrolling through the TAF text. 5) Press the FMS Knob or the CLR Key to return to the Weather Data Link (XM) Page. Or: 1) Select the Weather Information Page. a) Turn the large FMS Knob to select the Waypoint Page Group. b) Select the WX Softkey to select the Weather Information Page. 2) Press the FMS Knob to display the cursor. 3) Use the FMS Knob to enter the desired airport and press the ENT Key. 4) Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text. Note that the METAR text must be completely scrolled through before scrolling through the TAF text. METAR Text for the Selected Airport METAR Symbol TAF Text for the Selected Airport Figure 6-26 METAR and TAF Text on the Weather Information Page 358 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Original METAR text is also accessible while panning the map cursor over a METAR flag on any map page on which a METAR is displayed. The METAR text is shown in a box near the METAR flag. In addition, METAR flags and their associated text are displayed on the Active Flight Plan Page on the MFD. METAR flags appears next to waypoints in the flight plan with an associated METAR. Displaying original METAR text on the Active Flight Plan Page: 1) Select the Active Flight Plan Page on the MFD. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the desired waypoint. The METAR text will appear in the ‘SELECTED WAYPOINT WEATHER’ window below. 4) When finished, press the FMS Knob to remove the cursor or press the FPL Key to exit the Active Flight Plan Page. To display the METAR legend on the Weather Data Link (XM) Page (Figure 6-27), select the LEGEND Softkey when METARs are enabled for display. Information in the METAR text determines the color of the METAR flag. A gray METAR flag appears for a reporting station when its METAR text does not contain adequate information to determine the METAR category (e.g. VFR, IFR). Figure 6-27 METAR Legend 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 359 HAZARD AVOIDANCE SURFACE ANALYSIS AND CITY FORECAST NOTE: Surface Analysis and City Forecast data are displayed only within the installed navigation database coverage area. Surface Analysis and City Forecast information is available for current and forecast weather conditions. Forecasts are available for intervals of 12, 24, 36, and 48 hours. Figure 6-28 12 Hour Surface Analysis and City Forecast Data Displaying Surface Analysis and City Forecast information: 1) Select the Weather Data Link (XM) Page. 2) Select the MORE WX Softkey. 3) Select the SFC Softkey. 4) Select the desired forecast time: CURRENT, 12 HR, 24 HR, 36 HR, or 48 HR. The SFC Softkey label changes to reflect the forecast time selected. To display the Surface Analysis and City Forecast legend (Figure 6-29), select the LEGEND Softkey when the Surface Analysis and City Forecast weather product is displayed. Figure 6-29 Surface Analysis Legend 360 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE FREEZING LEVELS The Freezing Level weather product shows the color-coded contour lines for the altitude and location at which the first isotherm is found (Figure 6-30). When no data is displayed for a given altitude, the data for that altitude has not been received, or is out of date and has been removed from the display. New data will appear when it becomes available. Figure 6-30 Freezing Level Data Displaying Freezing Level information: 1) Select the Weather Data Link (XM) Page. 2) Select the MORE WX Softkey. 3) Select the FRZ LVL Softkey. To display the Freezing Level legend (Figure 6-31), select the LEGEND Softkey when Freezing Level data is displayed. Figure 6-31 Freezing Level Legend 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 361 HAZARD AVOIDANCE WINDS ALOFT The Winds Aloft weather product (Figure 6-32) shows the predicted wind speed and direction at the surface and at selected altitudes. Altitude can be displayed in 3,000-foot increments from the surface up to 42,000 feet MSL. Displaying Winds Aloft data: 1) Select the Weather Data Link (XM) Page. 2) Select the MORE WX Softkey. 3) Select the WIND Softkey. 4) Select the desired altitude level: SFC (surface) up to 42,000 feet. Select the NEXT or PREV Softkey to cycle through the altitude softkeys. The WIND Softkey label changes to reflect the altitude selected. Figure 6-32 Winds Aloft Weather Product at 24,000 Feet To display the Winds Aloft legend (Figure 6-33), select the LEGEND Softkey when Winds Aloft is selected for display. Figure 6-33 Winds Aloft Data with Legend Headwind and tailwind components aloft are available inside the optional Profile View feature on the Navigation Map Page (Figure 6-34). The displayed wind components are relative to current aircraft altitude and track, but not to aircraft speed. 362 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Weather Product Age Wind Component Velocity and Direction Arrows Altitude Scale Figure 6-34 Winds Aloft Weather Product with Profile View (Navigation Map Page) Arrows pointing to the left indicate headwind components; tailwind component arrows point to the right, as shown in Table 6-4. Headwind Symbol Tailwind Symbol Headwind/Tailwind Component None None Less than 5 knots 5 knots 10 knots 50 knots Table 6-4 Profile View Headwind/Tailwind Component Symbols Showing/Hiding Profile View (containing winds aloft data) 1) Select the Navigation Map Page. 2) Select the PROFILE Softkey. Or: 1) Press the MENU Key. 2) Turn the large FMS Knob to highlight ‘Show Profile View’ or ‘Hide Profile View’ (choice dependent on current state) and press the ENT Key. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 363 HAZARD AVOIDANCE Winds Aloft data inside the Profile View is enabled by default when the Profile View is displayed on the Navigation Map Page. This behavior can be changed on the Navigation Map Page. Enabling/disabling winds aloft data display in Profile View: 1) Select the Navigation Map Page. 2) Press the MENU Key. 3) With Map Setup highlighted, press the ENT Key (Figure 6-35). 4) Turn the small FMS Knob to select the Profile Group and press the ENT Key (Figure 6-36). 5) Turn the large FMS Knob to select ‘Profile Winds’ (Figure 6-37). 6) Turn the small FMS Knob to select ‘On’ or ‘Off’. 7) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. Figure 6-35 Navigation Map Page Menu Figure 6-36 Navigation Map Page Setup Menu 364 Figure 6-37 Navigation Map Page Setup Menu, Weather Group Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE COUNTY WARNINGS The County Warnings weather product (Figure 6-38) provides specific public awareness and protection weather warnings from the National Weather Service (NWS). This can include information on tornadoes, severe thunderstorms, and flood conditions. Additional Information on Flood Warning Selected with Map Pointer Flood Warning Figure 6-38 County Flood Warning Displaying County Warning information: 1) Select the Weather Data Link (XM) Page. 2) Select the MORE WX Softkey. 3) Select the COUNTY Softkey. To display the County Warnings legend (Figure 6-39), select the LEGEND Softkey when County Warnings are selected to be displayed. Figure 6-39 County Warnings Legend 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 365 HAZARD AVOIDANCE CYCLONE The Cyclone weather product (Figure 6-40) shows the current location of cyclones (hurricanes), tropical storms, and their projected tracks. The system displays the projected track information in the form of DD/HH:MM. Cyclone Figure 6-40 Cyclone Weather Product Selected for Display Displaying cyclone (hurricane) track information: 1) Select the Weather Data Link (XM) Page. 2) Select the MORE WX Softkey. 3) Select the CYCLONE Softkey. To display the Cyclone legend (Figure 6-41), select the LEGEND Softkey when Cyclones are selected to be displayed. Figure 6-41 Cyclone Legend 366 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE ICING (CIP & SLD) Current Icing Product (CIP) data shows a graphical view of the icing environment (Figure 6-42). Icing severity is displayed in four categories: light, moderate, severe, and extreme (not specific to aircraft type). The CIP product is not a forecast, but a presentation of the conditions at the time of the analysis. Supercooled Large Droplet (SLD) icing conditions are characterized by the presence of relatively large, super cooled water droplets indicative of freezing drizzle and freezing rain aloft. SLD threat areas are depicted as magenta dots over the CIP colors. SLD conditions may be extremely hazardous to all aircraft. Displaying Icing data: 1) Select the Weather Data Link (XM) Page. 2) Select the MORE WX Softkey. 3) Select the ICNG Softkey. 4) Select the desired altitude level: 1,000 feet up to 30,000 feet. Press the NEXT or PREV Softkey to cycle through the altitude softkeys. The ICNG Softkey label changes to reflect the altitude selected. Icing Potential SLD Threat Figure 6-42 Icing Data at 21,000 Feet To display the Icing Potential legend (Figure 6-43), press the LEGEND Softkey when Icing is selected for display. Figure 6-43 Icing Potential Legend 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 367 HAZARD AVOIDANCE TURBULENCE The Turbulence weather product (Figure 6-44) identifies the potential for erratic movement of high-altitude air mass associated winds. Turbulence is classified as light, moderate, severe or extreme, at altitudes between 21,000 and 45,000 feet. Turbulence data is intended to supplement AIRMETs and SIGMETs. Displaying Turbulence data: 1) Select the Weather Data Link (XM) Page. 2) Select the MORE WX Softkey. 3) Select the TURB Softkey. 4) Select the desired altitude level: 21,000 feet up to 45,000 feet. Select the NEXT or PREV Softkey to cycle through the altitude softkeys. The TURB Softkey label changes to reflect the altitude selected. Severe Turbulence Moderate Turbulence Light Turbulence Figure 6-44 Turbulence Weather Product at 21,000 Feet To display the Turbulence legend (Figure 6-45), select the LEGEND Softkey when Turbulence is selected for display. Figure 6-45 Turbulence Legend 368 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE PIREPS AND AIREPS Pilot Weather Reports (PIREPs) describe in-flight weather conditions encountered by pilots. When significant weather conditions are reported or forecast, Air Traffic Control (ATC) facilities are required to solicit PIREPs. A PIREP may contain adverse weather conditions, such as low in-flight visibility, icing conditions, windshear, turbulence, and type of aircraft flown. PIREPs are issued as either Routine (UA) or Urgent (UUA). Another type of PIREP is an Air Report (AIREP). Commercial airlines typically generate AIREPs. Instructions for Viewing PIREP and AIREP Text Urgent PIREP Routine PIREP Selected AIREP Figure 6-46 AIREPs and PIREPs on the Weather Data Link (XM) Page Displaying PIREP and AIREP text: 1) Select the Weather Data Link (XM) Page. 2) Select the MORE WX Softkey. 3) Select the AIREPS or PIREPS Softkey. 4) Press the Joystick and pan to the desired weather report. A gray circle appears around the weather report when it is selected. 5) Press the ENT Key. The Weather Information Page is shown with PIREP or AIREP text. The data is first displayed in a decoded fashion, followed by the original text. Note the original text may contain additional information not present in the decoded version. 6) Use the FMS Knob or the ENT Key to scroll through the PIREP or AIREP text. 7) Press the FMS Knob or the CLR Key to return to the Weather Data Link (XM) Page. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 369 HAZARD AVOIDANCE Age of report in HH:MM Decoded PIREP Text Original PIREP Text Selected PIREP Figure 6-47 PIREP Text on the Weather Information Page To display the PIREP or AIREP legend (Figure 6-48), select the LEGEND Softkey when PIREPs or AIREPs are selected for display. The PIREP color is determined by the type (routine or urgent). Figure 6-48 AIREPs & PIREPs Legend 370 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE TFRS NOTE: Do not rely solely upon data link services to provide Temporary Flight Restriction (TFR) information. Always confirm TFR information through official sources such as Flight Service Stations or Air Traffic Control. In the United States, the Federal Aviation Administration (FAA) issues Temporary Flight Restrictions (TFRs) to designate areas where flight is restricted. TFRs are issued to restrict flight for a variety of reasons including national security, law enforcement, fire suppression, natural disasters., airshows, and large sporting events. TFRs may be issued at any time, and TFR data displayed is only intended to supplement official TFR information obtained from Flight Service Stations (FSS), and air traffic control. The age of TFR data is not shown; however, if TFR data is not available or has expired, the system displays ‘TFR N/A’ in the upper-left corner of maps on which TFRs can be displayed. TFR Summary Data TFR Selected with Map Pointer Figure 6-49 TFR Data on the Weather Data Link (XM) Page Displaying TFR Data: 1) Select the Weather Data Link (XM) Page or Navigation Map Page. 2) Press the Joystick and pan the map pointer to highlight a TFR border. The system displays TFR summary information for the highlighted TFR above the map. 3) Press the ENT Key. The system displays a pop-up menu. 4) If necessary, turn the FMS Knob to select ‘Review Airspaces’ and press the ENT Key. The system displays the TFR Information window. 5) Press the FMS Knob or the CLR Key to remove the TFR Information window. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 371 HAZARD AVOIDANCE Figure 6-50 Full Text for Selected TFR The setup menus for the Navigation Map Page control the map range settings above which TFR data is decluttered from the display. If a map range larger than the TFR product map range setting is selected, the TFR product data is removed from the map. Maps other than the Navigation Map Page use settings based on those selected for the Navigation Map Page. Setting up and customizing TFR data for maps on which TFR data can be displayed: 1) Select the Navigation Map Page. 2) Press the MENU Key. 3) With Map Setup highlighted, press the ENT Key (Figure 6-51). 4) Turn the small FMS Knob to select the Aviation Group and press the ENT Key (Figure 6-52). 5) Turn the large FMS Knob to scroll to the TFR product maximum map range setting (Figure 6-53). 6) Turn the small FMS Knob to scroll through options (range settings or ‘Off’ to disable display of TFRs). 7) Press the ENT Key to select an option. 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. Figure 6-51 Navigation Map Page Menu Figure 6-52 Navigation Map Page Setup Menu 372 Figure 6-53 Navigation Map Page Setup Menu, Weather Group Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE 6.2 GARMIN CONNEXT WEATHER WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous weather. Information contained within data link weather products may not accurately depict current weather conditions. WARNING: Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather product. Due to time delays inherent in gathering and processing weather data for data link transmission, the weather information shown by the data link weather product may be significantly older than the indicated weather product age. NOTE: The availability of specific Garmin Connext Weather products varies by region. For product coverage information, refer to https://fly.garmin.com/fly-garmin/connext/worldwide-weather/. The optional Garmin GSR 56 and GDL 59 provide the Garmin Connext data link weather service to the Prodigy system. The system displays graphical weather information and associated text on the Multi Function Display (MFD) and on the Primary Flight Display (PFD) Inset Map. The system provides Garmin Connext Weather information after the flight crew selects either a manual or automatic Connext Data Request on the Weather Data Link (CNXT) Page on the MFD. Before the Garmin Connext weather service can be used, an account must first be established. Refer to the Additional Features section for more information. REGISTERING THE SYSTEM FOR GARMIN CONNEXT WEATHER When an account is established, Garmin customer service provides an Access Code which must be entered on the system in order to complete the registration process. Registering the system to receive Garmin Connext Weather: 1) Ensure the aircraft is outside and has a clear view of the sky (if registering via an Iridium satellite telephone connection), or connected to a Wi-Fi network. Refer to the Additional Features section for more information on connecting to a Wi-Fi network. 2) Turn the large FMS Knob on the MFD to select the MAP page group. 3) Turn the small FMS Knob to select the MAP - WEATHER DATA LINK (CNXT or XM) Page. If ‘XM’ is displayed in the page title, it will be necessary to change the data link source to Garmin Connext (CNXT) before continuing. Refer to ‘Viewing the Weather Data Link Page’ procedure to change the data link source to Garmin Connext Weather prior to registration. 4) If the system displays the ‘Connext Registration’ window, proceed to step 7. Otherwise, press the MENU Key. The Page Menu appears as seen in Figure 6-54. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 373 HAZARD AVOIDANCE Figure 6-54 Select ‘Register With Connext’ 5) Turn the large FMS Knob to highlight ‘Register With Connext’ in the menu list. 6) Press the ENT Key. The Connext Registration Window is displayed as shown in Figure 6-55. Figure 6-55 Enter Access Code 7) Enter the access code provided by customer service in the ACCESS CODE field. 8) Press the ENT Key. ‘REGISTER’ is highlighted as in Figure 6-55. 9) Press the ENT Key. The system contacts the Garmin Connext service using the GDL 59 Wi-Fi connection (if available) or through the Iridium satellite network using the GSR 56. Registration is complete when the STATUS field displays ‘REGISTERED’. 374 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE ACCESSING GARMIN CONNEXT WEATHER PRODUCTS The principal map for viewing Garmin Connext Weather information is the Weather Data Link (CNXT) Page in the Map Page Group (Figure 6-56). This is the only map display capable of showing information for all available Garmin Connext weather products. No weather data appears until an initial Connext Data Request has been completed successfully. Viewing the Weather Data Link (CNXT) Page: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Weather Data Link (XM or CNXT) Page. 3) If the page title contains ‘XM’, it will be necessary to change the data link weather source from SiriusXM Weather to Garmin Connext Weather. Refer to the next procedure to change the source. Changing the weather data link source (Garmin Connext or SiriusXM): 1) If necessary, turn the large FMS Knob to select the Map Page Group. 2) If necessary, turn the small FMS Knob to select the Weather Data Link (XM or CNXT) Page. 3) Press the MENU Key. 4) If necessary, turn the large FMS Knob to highlight ‘Display Connext Weather’ or ‘Display XM Weather’ and press the ENT Key. Weather Data Link Page title and softkeys change to correspond to selected data link weather source. Precipitation Weather Product Symbol and Product Age in Minutes Precipitation Weather Product Selected for Display Figure 6-56 Weather Data Link (CNXT) Page When a weather product is selected for display on the Weather Data Link (CNXT) Page, a box containing a symbol or name for the product and its age (in minutes) are shown in the upper right (Figure 6-56) of the page. If weather data has not been requested, or is not available from the source, ‘N/A’ is shown next to the product 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 375 HAZARD AVOIDANCE symbol instead of the product age. The age of the weather product is based on the time difference between when the requested data was assembled on the ground and the current GPS time. The Garmin Connext Weather service updates its weather products continuously, or refreshes them at specific intervals, depending on the product (defined in the Refresh Rate column in Table 6-5). The product age display does not indicate the age of the information contained within the weather product, which can be significantly older than the displayed weather product age. If for any reason, a weather product is not refreshed within the defined Expiration Time intervals (see Table 6-4), the product is considered expired and is removed from the display. The age of the expired product is replaced by dashes. If more than half of the expiration time has elapsed, the color of the product age changes from white to yellow. Table 6-5 shows the Garmin Connext weather product symbols, the expiration times and the refresh rates. The refresh rate represents the interval at which the Garmin Connext ground-based servers make available the most current known weather data. It does not represent the rate at which new content is received from various weather sources around the world. NOTE: The availability of specific Garmin Connext Weather products varies by region. For product coverage information, refer to https://fly.garmin.com/fly-garmin/connext/worldwide-weather/. Garmin Connext Weather Product Symbol Radar Precipitation (PRECIP) Expiration Time (Minutes) 30 Infrared Satellite (IR SAT) Garmin Connext Data Link Lightning (DL LTNG) SIGMETs/AIRMETs (SIG/AIR) Meteorological Aerodrome Report (METARs) Winds Aloft (WIND) Pilot Weather Report (PIREPs) Temporary Flight Restrictions no product image (TFRs) Terminal Aerodrome Reports no product image (TAFs) Refresh Rate (Minutes) U.S.: 3* Canada: 3*† Europe: 15 Australia: 15ˆ 60 30 30 Continuous 60 Continuous 90 Continuous 90 Continuous 90 Continuous 60 Continuous 60 Continuous * The composite precipitation image is updated every 3 minutes, but individual radar sites may take between 3 and 10 minutes to provide new data. † Canadian radar precipitation data provided by Environment Canada. ˆ Australian radar precipitation data provided by the Australia Bureau of Meteorology Table 6-5 Garmin Connext Weather Product Symbols and Data Timing 376 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Infrared Satellite (IR SAT) Flight Plan Pages + Nearest Page Group + AUX - Trip Planning Page + Weather Information Page Weather Data Link (CNXT) Page Precipitation (PRECIP) Navigation Map Page Garmin Connext Weather Product PFD Inset Map Table 6-6 shows which Garmin Connext Weather products can be displayed (indicated with a ‘+’ symbol) on specific maps. + + + + + + + + + + + + + + Garmin Connext Data Link Lightning (DL LTNG) SIGMETs/AIRMETs (SIG/AIR) + METARs + + + + Winds Aloft (WIND) + + +* + PIREPs No Radar Coverage + + + + TFRs + + + + + + TAFs * Winds Aloft data on the Navigation Map Page available inside the Profile View Window. Table 6-6 Garmin Connext Weather Product Display Maps Softkeys control the display of weather information on most MFD pages and the PFD Inset Map (Figure 6-57 shows the weather product softkeys for the Weather Data Link (CNXT) Page). When a weather product is selected for display, the corresponding softkey label changes to gray to indicate the product display is enabled. SYSTEM CPDLC PRECIP IR SAT DL LTNG SIG/AIR WIND OFF METAR LEGEND MORE WX CHKLIST PIREPS BACK WIND Softkey label changes to reflect current selection. Press the BACK Softkey to move up one level. PREV and NEXT Softkeys cycle through Winds Aloft altitude selection softkeys. PREV OFF SFC 3000 6000 9000 12000 15000 NEXT LEGEND BACK PREV OFF 18000 21000 24000 27000 30000 33000 NEXT LEGEND BACK PREV OFF 36000 39000 42000 NEXT LEGEND BACK Figure 6-57 Weather Data Link (CNXT) Page Softkeys (MFD) 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 377 HAZARD AVOIDANCE The setup menus for the Navigation Map Page and the Weather Data Link (CNXT) Page control the map range settings above which weather products data are decluttered from the display. If a map range larger than the maximum weather product map range setting is selected, the system removes the weather product from the map. The menus also provide controls for enabling/disabling the display of weather products, in addition to using the softkeys. Setting up and customizing the Weather Data Link (CNXT) Page: 1) Select the Weather Data Link (CNXT) Page. 2) Press the MENU Key. 3) With ‘Weather Setup’ highlighted, press the ENT Key (Figure 6-58). 4) Turn the small FMS Knob to select ‘PRODUCT GROUP 1’ or ‘PRODUCT GROUP 2’, and press the ENT Key (Figure 6-59). 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections. 6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, maximum map range settings, etc.). 7) Press the ENT Key to select an option. 8) Press the FMS Knob or CLR Key to return to the Weather Data Link (CNXT) Page with the changed settings. Figure 6-58 Weather Data Link (CNXT) Page Menu Figure 6-59 Weather Data Link (CNXT) Page Setup Menu Restoring default Weather Data Link (CNXT) Page settings: 1) Select the Weather Data Link (CNXT) Page. 2) Press the MENU Key. 3) With ‘Weather Setup’ highlighted, press the ENT Key. 4) Turn the small FMS Knob to select ‘PRODUCT GROUP 1’ or ‘PRODUCT GROUP 2’, and press the ENT Key (Figure 6-59). 378 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE 5) Highlight the product group name (to restore default settings to the entire product group) or an individual weather product, then press the ENT Key. 6) Highlight ‘Restore All Defaults’ or ‘Restore Selection Default’, and press the ENT Key. If multiple data link weather services are installed, customizing the display settings for the corresponding weather products shown in Table 6-7 will result in identical settings for a comparable weather product from another service provider. Garmin Connext Weather Product (CNXT) Precipitation Next-generation Radar (NEXRAD) (PRECIP) Cloud Top Infrared Satellite (CLD TOP) (IR SAT) SiriusXM Lightning Garmin Connext Data Link Lightning (DL LTNG) (XM LTNG) SIGMETs/AIRMETs SIGMETs/AIRMETs (SIG/AIR) (SIG/AIR) Meteorological Aerodrome Report Meteorological Aerodrome Report (METARs) (METARs) Winds Aloft Winds Aloft (WIND) (WIND) Pilot Weather Report Pilot Weather Report (PIREPs) (PIREPs) SiriusXM Weather Product Table 6-7 Corresponding Weather Data Link Product Settings Maps besides the Weather Data Link (CNXT) Page use settings based on those selected for the Navigation Map Page. Setting up and customizing weather data for the Navigation Map Page: 1) Select the Navigation Map Page. 2) Press the MENU Key. 3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-60). 4) Turn the small FMS Knob to select the ‘Weather’ Group and press the ENT Key (Figure 6-61). 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-62). 6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, maximum map range settings). 7) Press the ENT Key to select an option. 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 379 HAZARD AVOIDANCE Figure 6-60 Navigation Map Page Menu Figure 6-61 Navigation Map Page Setup Menu Figure 6-62 Navigation Map Page Setup Menu, Weather Group Each active weather product has an associated legend which can be displayed on the Weather Data Link (CNXT) Page. If no weather product softkeys are selected, the LEGEND Softkey will be unavailable. Viewing legends for displayed weather products 1) Select the Weather Data Link (CNXT) Page. 2) Select the LEGEND Softkey to display the legends for the displayed weather products. Or: a) Press the MENU Key. b) Select ‘Weather Legend’ and press the ENT Key. 3) Turn the FMS Knob to scroll through the legends if more are available than fit in the window. 4) To remove the Legend Window, select the LEGEND Softkey, the ENT or the CLR Key, or press the FMS Knob. Viewing legends for displayed weather products (on the Navigation Map Page): 1) Select the Navigation Map Page. 2) Select the MAP Softkey. 3) Select the LEGEND Softkey (available if one or more SiriusXM Weather products are enabled for display). 4) To remove the Legend Window, select the LEGEND Softkey, or press the ENT or the CLR Key, or press the FMS Knob. 380 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Additional information about the following can be displayed by panning over the display on the map: • Infrared Satellite (IR SAT) • METARs • SIGMETs • TFRs • AIRMETs • PIREPs The map panning feature is enabled by pressing the Joystick. The map range is adjusted by turning the Joystick. If the map range is adjusted while panning is enabled, the map is re-centered on the Map Pointer. Additional information for selected PIREP PIREP selected with Map Pointer Figure 6-63 Panning on the Weather Data Link (CNXT) Page CONNEXT WEATHER DATA REQUESTS The Connext Data Request window provides the flight crew with the options to enable or disable the requested weather coverage area(s), choose automatic weather update intervals (if desired), and the ability to send or cancel weather data requests. The status of the Garmin Connext data request process is also displayed. Before a Garmin Connext data request can occur, a valid request coverage area must be defined from which all currently available Garmin Connext weather products will be retrieved. At a minimum, either the aircraft’s present position or a waypoint (as part of a flight plan or entered directly in the ‘WAYPOINT’ coverage field) must be part of the request coverage area, otherwise the request status window will indicate ‘INVALID COVERAGE AREA’ and the system will not allow a request to occur. It is not necessary for a destination (based on an active flight plan), a flight plan, or waypoint to be specified prior to enabling these coverage areas; however no weather data will be retrieved for these option(s) until a flight plan or waypoint is provided, respectively. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 381 HAZARD AVOIDANCE Requesting Garmin Connext weather data manually: 1) Select the Weather Data Link (CNXT) Page. 2) Press the MENU Key. 3) With ‘Connext Data Request’ highlighted, press the ENT Key (Figure 6-64). 4) Turn the large FMS Knob to highlight the desired coverage option(s) and press the ENT Key to add or remove a check from one of more of the following coverage selections (Figures 6-65, 6-66): • PRESENT POSITION – Requests data based on current location. • DESTINATION – Requests data based on the active flight plan destination (Direct-To destinations excluded). See the Flight Management section for more information about entering and activating flight plans. • FPL – Requests data along an active flight plan, if one exists. Turn the small FMS Knob to select the desired flight plan look-ahead distance option (or choose ‘REMAINING FPL’ to request the remainder of the flight plan), then press the ENT Key. • WAYPOINT – Requests data based on a waypoint (which may be off-route). Turn the large and small FMS Knobs to enter a waypoint, then press the ENT Key. 5) Turn the large FMS Knob highlight to the ‘DIAMETER / RTE WIDTH’ (diameter/route width) distance field and turn the small FMS Knob to select the desired diameter and route width of the request, then press the ENT Key. 6) Turn the large FMS Knob until the ‘SEND REQ’ button is highlighted. Press the ENT Key to initiate the request immediately or press the FMS Knob to return to the Weather Data Link (CNXT) Page without requesting weather data. Figure 6-64 Weather Data Link (CNXT) Page Menu Figure 6-65 Connext Data Request Window 382 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Present Position Selected, 200 nm Diameter Requested Next 80 nm of Flight Plan Selected, 200 nm Route Width Requested Destination Selected, 200 nm Diameter Requested Off-Route Waypoint Selected, 200 nm Diameter Requested Figure 6-66 Connext Weather Data Request Results with Precipitation Displayed During a Connext Data Request, the REQUEST STATUS window initially displays “Contacting Connext...”. Once a connection is established, the REQUEST STATUS window displays “Receiving Wx Data... Time Remaining:” with an estimated data transfer time (either in minutes or seconds). If desired, the Connext Data Request window may be closed while the data request is processing by pressing the FMS Knob; the data request will continue to process in the background. Connext Data Requests typically take between 1 to 4 minutes to complete depending on the size of the selected weather coverage area(s), the amount of weather activity present (such as precipitation), and the Iridium signal strength. The system retrieves all available Garmin Connext weather products within the selected coverage area(s) during an initial Connext Data Request. Enabling or disabling the display of the weather product does not affect which weather products are retrieved during a Connext Data Request. To reduce data usage during subsequent requests, the system retains previously retrieved textual weather products such as METARs and TAFs, so long as they have not expired. The system also retrieves any new textual weather products matching the current coverage area, and all graphical weather products during each data request. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 383 HAZARD AVOIDANCE If the Connext Data Request was successful, the REQUEST STATUS window (if shown) indicates ‘OK’. Refer to the Abnormal Operations discussion later in this section for more information on the messages received if the request is unsuccessful, with possible causes. Cancelling Connext Data Request in Progress: 1) Select the Weather Data Link (CNXT) Page. 2) Press the MENU Key. 3) With ‘Connext Data Request’ highlighted, press the ENT Key. 4) With the ‘CANCEL REQ’ option highlighted, press the ENT Key. The REQUEST STATUS window indicates ‘Request Canceled’. 5) Press the FMS Knob to return to the Weather Data Link (CNXT) Page. The flight crew can schedule Connext Data Requests to recur automatically. Auto requests remain enabled until the flight crew disables them, or the system power is cycled. When an automatic data request is enabled, the REQUEST STATUS Window displays the number of minutes or seconds until the automatic data request occurs. NOTE: If automatic Connext Data Requests were enabled prior to the system entering Reversionary Mode, the automatic weather data requests continue in Reversionary Mode, however the Connext Data Request window and its associated options will not be available. Enabling/disabling automatic Connext Data Requests: 1) Select the Weather Data Link (CNXT) Page. 2) Press the MENU Key. 3) With ‘Connext Data Request’ highlighted, press the ENT Key. 4) Choose the desired weather coverage options. 5) Turn the large FMS Knob to select the ‘UPDATE RATE’ setting. Then turn the small FMS Knob to highlight the desired automatic update frequency (Off, 5 Min, 10 Min, 15 Min, 20 Min, 30 Min, 45 Min, or 60 Min). 6) The ‘SEND REQ” button is highlighted and a countdown timer is displayed in the ‘REQUEST STATUS’ based on the currently selected update rate. Press the ENT Key to immediately send an immediate Connext Data Request. Or: 384 Press the FMS Knob to return to the Weather Data Link (CNXT) Page. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE GARMIN CONNEXT WEATHER PRODUCTS PRECIPITATION The Precipitation weather product provides radar precipitation information in selected radar coverage areas. This information comes from individual weather radar sites and weather data sources such as government agencies. Each radar site or source may provide weather data at differing rates and times. Periodically, the Garmin Connext service compiles the available information to form a composite image, and assigns a single time to indicate when it created the image. This image becomes the Precipitation weather product. Individual images--gathered from each radar site--differ in age, and are always older than the displayed Precipitation weather product age. Because of the time required to detect, assemble, and distribute the Precipitation weather product, the displayed weather information contained within the product may be significantly older than the current radar synopsis and may not depict the current weather conditions. The Precipitation weather product should never be used as a basis for maneuvering in, near, or around areas of hazardous weather regardless of the information it contains. Boundary of Connext Data Request area (shown for Precipitation weather product) No Radar Coverage within requested within request area Figure 6-67 Weather Data Link (CNXT) Page with Precipitation Displaying Precipitation weather information: 1) Select the MAP Softkey (for the PFD Inset Map, select the INSET Softkey). This step is not necessary on the Weather Data Link (CNXT) Page. 2) Select the PRECIP Softkey. Radar data shown represents lowest level, base reflectivity, of radar returns. The display of the information is color-coded to indicate the weather severity level. All weather product legends can be viewed on the 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 385 HAZARD AVOIDANCE Weather Data Link (CNXT) Page. For the Precipitation legend (Figure 6-68), select the LEGEND Softkey when Precipitation is selected for display. No Radar Coverage Boundary of Connext Data Request Figure 6-68 Precipitation Data Legend The display of no radar coverage is enabled when Precipitation is selected for display. Areas where precipitation radar coverage is not currently available or is not being collected are indicated in gray shade of purple. A white boundary line with white tick marks depicts the selected coverage area of the Connext Data Request. The boundary encloses the precipitation data when this weather product is displayed. Reflectivity Reflectivity is the amount of transmitted power returned to the radar receiver. Colors on the Precipitation display directly correlate to the level of detected reflectivity. Reflectivity as it relates to hazardous weather can be very complex. The role of radar is essentially to detect moisture in the atmosphere. Simply put, certain types of weather reflect radar better than others. The intensity of a radar reflection is not necessarily an indication of the weather hazard level. For instance, wet hail returns a strong radar reflection, while dry hail does not. Both wet and dry hail can be extremely hazardous. The different radar echo intensities are measured in decibels (dB) relative to reflectivity (Z). Weather radars measure the reflectivity ratio, or the energy reflected back to the radar receiver (designated by the letter Z). The value of Z increases as the returned signal strength increases. Precipitation Limitations Radar images may have certain limitations: • Radar base reflectivity does not provide sufficient information to determine cloud layers or precipitation characteristics (wet hail vs. rain). For example, it is not possible to distinguish between wet snow, wet hail, and rain. • Radar base reflectivity is sampled at the minimum antenna elevation angle. An individual radar site cannot depict high altitude storms at close ranges. It has no information about storms directly over the site. • When zoomed in to a range of 30 nm, each square block on the display represents an area of four square kilometers. 386 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE The following may cause abnormalities in displayed radar images: • Ground clutter • Strobes and spurious radar data • Sun strobes (when the radar antenna points directly at the sun) • Interference from buildings or mountains, which may cause shadows • Metallic dust (chaff) from military aircraft, which can cause alterations in radar scans INFRARED SATELLITE The Infrared Satellite (IR SAT) weather product (Figure 6-69) depicts cloud top temperatures from satellite imagery. Brighter cloud top colors indicate cooler temperatures occurring at higher altitudes. Temperature range of selected data Map Pointer on selected Infrared Satellite Information Figure 6-69 Infrared Satellite Data on the Weather Data Link (CNXT) Page Displaying Cloud Tops information: 1) Select the Weather Data Link (CNXT) Page. 2) Select the IR SAT Softkey. To display the Infrared Satellite legend (Figure 6-70), select the LEGEND Softkey when Infrared Satellite data is selected for display. Figure 6-70 Infrared Satellite Legend 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 387 HAZARD AVOIDANCE GARMIN CONNEXT DATA LINK LIGHTNING The Garmin Connext Data Link Lightning (DL LTNG) weather product (Figure 6-71) shows the approximate location of cloud-to-ground lightning strikes. A strike icon represents a strike that has occurred within a twokilometer region. Neither cloud-to-cloud nor the exact location of the lightning strike is displayed. Lightning Strikes Figure 6-71 Garmin Connext Data Link Lightning Displaying Lightning information: 1) Select the MAP Softkey (for the PFD Inset Map, select the INSET Softkey). This step is not necessary on the Weather Data Link (CNXT) Page. 2) Select the DL LTNG Softkey. To display the lightning legend on the Weather Data Link (CNXT) Page (Figure 6-72), select the LEGEND Softkey when the Garmin Connext Data Link Lightning weather product is enabled for display. Figure 6-72 Garmin Connext Data Link Lightning Legend 388 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE SIGMETS AND AIRMETS SIGMETs (SIGnificant METeorological Information) and AIRMETs (AIRmen’s METeorological Information) are issued for potentially hazardous weather. A Convective SIGMET is issued for hazardous convective weather such as severe or widespread thunderstorms. A localized SIGMET can be displayed when significant weather conditions are not widespread. The entire SIGMET or AIRMET is displayed as long as any portion of it is issued within the coverage area of the Connext Data Request. Additional information for selected SIGMET/ AIRMET AIRMET selected with Map Pointer Figure 6-73 SIGMET/AIRMET Data Displaying SIGMETs and AIRMETs: 1) Select the Weather Data Link (CNXT) Page. 2) Select the SIG/AIR Softkey. 3) To view the text of the SIGMET or AIRMET, press the Joystick and move the Map Pointer to highlight the border of the desired SIGMET/AIRMET. 4) Press the ENT key. Figure 6-74 shows sample SIGMET text. To display the SIGMET and AIRMET legend (Figure 6-75), select the LEGEND Softkey when SIGMETs and AIRMETs are selected for display. Figure 6-74 Sample SIGMET Text 190-00728-06 Rev. A Figure 6-75 SIGMET/AIRMET Legend Embraer Prodigy® Flight Deck 100 Pilot’s Guide 389 HAZARD AVOIDANCE METARS AND TAFS NOTE: METAR information is only displayed within the installed navigation database service area. METARs (METeorological Aerodrome Reports) typically contain information about the temperature, dewpoint, wind, precipitation, cloud cover, cloud base heights, visibility, and barometric pressure at an airport or observation station. They can also contain information on precipitation amounts, lightning, and other critical data. METARs reflect hourly observations; non-routine updates include the code “SPECI” in the report. METARs are shown as colored flags at airports that provide them. Instructions for Viewing METAR and TAF Text Selected Airport Figure 6-76 METAR Flags on the Weather Data Link (CNXT) Page TAFs (Terminal Aerodrome Forecasts) are weather predictions for specific airports within a 24- hour period, and may span up to 36 hours. TAFs typically include forecast wind, visibility, weather phenomena, and sky conditions using METAR codes. METAR and TAF text are displayed on the Weather Information Page. TAF information is displayed in its original form when a TAF is available. Displaying METAR and TAF text: 1) On the Weather Data Link (CNXT) Page, select the METAR Softkey. 2) Press the Joystick and pan to the desired airport. 3) Press the ENT Key. The Weather Information Page is shown with METAR and TAF text. 4) Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text. METAR text must be completely scrolled through before scrolling through the TAF text. 5) Press the FMS Knob or the CLR Key to return to the Weather Data Link (CNXT) Page. 390 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Or: 1) Select the Weather Information Page. a) Turn the large FMS Knob to select the Waypoint Page Group. b) Select the WX Softkey to select the Weather Information Page. 2) Press the FMS Knob to display the cursor. 3) Use the FMS Knob to enter the desired airport and press the ENT Key. 4) Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text. Note the METAR text must be completely scrolled through before scrolling through the TAF text. Decoded METAR Text Original METAR Text METAR Symbol TAF Available Figure 6-77 METAR Flags on the Weather Data Link (CNXT) Page Original METAR text is also accessible while panning the map cursor over a METAR flag on any map page on which a METAR is displayed. The METAR text is shown in a box near the METAR flag. In addition, METAR flags and their associated text are displayed on the Active Flight Plan Page on the MFD. METAR flags appears next to waypoints in the flight plan with an associated METAR. Displaying original METAR text on the Active Flight Plan Page: 1) Select the Active Flight Plan Page on the MFD. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the desired waypoint. The METAR text will appear in the ‘SELECTED WAYPOINT WEATHER’ window below. 4) When finished, press the FMS Knob to remove the cursor or press the FPL Key to exit the Active Flight Plan Page. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 391 HAZARD AVOIDANCE To display the METAR legend on the Weather Data Link (XM) Page (Figure 6-78), select the LEGEND Softkey when METARs are enabled for display. Information in the METAR text determines the color of the METAR flag. A gray METAR flag appears for a reporting station when its METAR text does not contain adequate information to determine the METAR category (e.g. VFR, IFR). Figure 6-78 METAR Legend WINDS ALOFT The Winds Aloft weather product (Figure 6-79) shows the predicted wind speed and direction at the surface and at selected altitudes. Altitude can be displayed in 3,000-foot increments from the surface up to 42,000 feet MSL. Displaying Winds Aloft data: 1) Select the Weather Data Link (CNXT) Page. 2) Press the MORE WX Softkey. 3) Press the WIND Softkey. 4) Select the desired altitude level: SFC (surface) up to 42,000 feet. Select the NEXT or PREV Softkey to cycle through the altitude softkeys. The WIND Softkey label changes to reflect the altitude selected. Figure 6-79 Winds Aloft Data at 33,000 Feet 392 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE To display the Winds Aloft legend (Figure 6-80), select the LEGEND Softkey when Winds Aloft is selected for display. Figure 6-80 Winds Aloft Data with Legend Headwind and tailwind components aloft are available inside the Profile View on the Navigation Map Page (Figure 6-81). The displayed components are relative to current aircraft altitude and track, but not to aircraft speed. Weather Product Age Wind Component Velocity and Direction Arrows Altitude Scale Figure 6-81 Winds Aloft Weather Product with Profile View (Navigation Map Page) Arrows pointing to the left indicate headwind components; tailwind component arrows point to the right, as shown in Table 6-8. Headwind Symbol Tailwind Symbol Headwind/Tailwind Component None None Less than 5 knots 5 knots 10 knots 50 knots Table 6-8 Profile View Headwind/Tailwind Component Symbols 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 393 HAZARD AVOIDANCE Showing/Hiding Profile View (containing winds aloft data) 1) Select the Navigation Map Page. 2) Select the PROFILE Softkey. Or: 1) Press the MENU Key. 2) Turn the large FMS Knob to highlight ‘Show Profile View’ or ‘Hide Profile View’ (choice dependent on current state) and press the ENT Key. Winds Aloft data inside the Profile View is enabled by default when the Profile View is displayed on the Navigation Map Page. This behavior can be changed on the Navigation Map Page. Enabling/disabling winds aloft data display in Profile View: 1) Select the Navigation Map Page. 2) Press the MENU Key. 3) With Map Setup highlighted, press the ENT Key (Figure 6-82). 4) Turn the small FMS Knob to select the Profile Group and press the ENT Key (Figure 6-83). 5) Turn the large FMS Knob to select ‘Profile Winds’ (Figure 6-84). 6) Turn the small FMS Knob to select ‘On’ or ‘Off’. 7) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. Figure 6-82 Navigation Map Page Menu Figure 6-83 Navigation Map Page Setup Menu 394 Figure 6-84 Navigation Map Page Setup Menu, Weather Group Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE PIREPS Pilot Weather Reports (PIREPs) describe in-flight weather encountered by pilots. A PIREP may contain adverse weather conditions, such as low in-flight visibility, icing conditions, wind shear, turbulence, and type of aircraft flown. PIREPs are issued as either Routine (UA) or Urgent (UUA). Instructions for Viewing PIREP Text Urgent PIREP Routine PIREP Selected Figure 6-85 PIREPs on the Weather Data Link (CNXT) Page Displaying PIREP text: 1) Select the Weather Data Link (CNXT) Page. 2) Press the MORE WX Softkey. 3) Press the PIREPS Softkey. 4) Press the Joystick and pan to the desired weather report. A gray circle will appear around the weather report when it is selected. 5) Press the ENT Key. The PIREP is first displayed in a decoded fashion, followed by the original text. Note the original text may contain additional information not found in the decoded version. 6) Use the FMS Knob or the ENT Key to scroll through the PIREP text. 7) Press the FMS Knob or the CLR Key to close the PIREP text window and return to the Weather Data Link (CNXT) Page. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 395 HAZARD AVOIDANCE Decoded PIREP Text Original PIREP Text Figure 6-86 PIREP Text on the Weather Data Link (CNXT) Page To display the PIREP legend (Figure 6-87), select the LEGEND Softkey when PIREPs are selected for display. The PIREP color is determined by the type (routine or urgent). Figure 6-87 AIREPs & PIREPs Legend 396 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE ABNORMAL OPERATIONS If the system cannot complete a Connext Data Request, one or more messages will appear in the request status window. Weather Request Status Message Auto requests inhibited Send manual request to reset. Description The system has disabled automatic weather data requests due to excessive errors. Automatic weather data requests have stopped. Send a manual weather data request to resume automatic updates. Auto update retry: ## Seconds The system will attempt another automatic weather data request after an error occurred during the previous request. Displays estimated time until next automatic request occurs. Connext Comm Error [2] A communications error has occurred with the GIA or GDL 59. Connext Comm Error [4] This occurs if multiple weather data requests have recently failed, or the GIA or GDL 59 is off-line. If this error persists, the system should be serviced. Connext Comm Error [5] The Iridium or Garmin Connext services are not accessible. Check Iridium signal strength. If this error persists, the system should be serviced. Connext Comm Error [6] A communications error has occurred. If this error persists, the system should be serviced. Connext Comm Error [7] The system halted the weather data request due to excessive delays while receiving weather data. Verify Iridium signal strength and re-try data request. Connext Comm Error [8] Connext Login Invalid A ground-based server error has occurred or invalid data received. There is a problem with the Garmin Connext registration. In the United States, contact Garmin at 1-866-739-5687. Outside the United States, call 913-397-8200, wait for the operator, and request extension 1135. The Garmin Connext weather data server is temporarily out of service, but is expected to return to service in less than 30 minutes. The Garmin Connext weather data server will be out of service for at least 30 minutes. The Connext Data Request does not sufficiently define a coverage area on which to retrieve weather data. Verify the selections in the Connext Weather Coverage Window, then issue another Connext Data Request. The system is not currently subscribed to the Garmin Connext Weather service, or the access code is incorrect. Verify the access code. In the United States, contact Garmin at 1-866-739-5687. Outside the United States, call 913-397-8200, wait for the operator, and request extension 1135. The weather data request area exceeds size limits. Reduce weather coverage area and re-send data request. The user has cancelled a weather data request. The ground-based server halted the weather data request due to excessive delays. Re-send data request. The Iridium voice telephone has interrupted the weather data request. Retry request when Iridium voice telephone is not in use. Connext Server Temporarily Inop Connext Server Inop Invalid Coverage Area No Connext Subscription Reduce Request Area Request Cancelled Request Failed - Try Again Transfer Preempted Table 6-9 Abnormal Weather Data Request Status Messages 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 397 HAZARD AVOIDANCE GARMIN CONNEXT WEATHER IN REVERSIONARY MODE When the system is operating in Reversionary Mode, only those weather products which can be displayed on the PFD Inset Map will be available for display (see Table 6-5 for a list of weather products and their associated map availability). If manual weather data requests were enabled prior to entering Reversionary Mode, no new Garmin Connext Weather data can be retrieved while operating in Reversionary Mode. If automatic weather data requests were enabled prior to Reversionary Mode operation, the system will continue the automatic data requests in Reversionary Mode (provided automatic requests have not been inhibited due to a system error). 398 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE 6.3 AIRBORNE COLOR WEATHER RADAR SYSTEM DESCRIPTION The Garmin GWX 68 Airborne Color Weather Radar is a 4-color digital pulsed radar with 6.5 kilowatts of output power. It combines excellent range and adjustable scanning profiles with a high-definition target display. The pulse width is four microseconds (µs) on all ranges except the 2.5 nm range. The GWX 68 uses a one µs pulse width at this range to reduce the targets smearing together on the display for better target definition at close range. The Embraer Phenom 100 uses a 12-inch phased array antenna that is fully stabilized to accommodate 30º of pitch and roll. To focus radar scanning on specific areas, Sector Scanning offers pilot-adjustable horizontal scan angles of 20º, 40º, 60º, or 90º. A vertical scanning function helps to analyze storm tops, gradients, and cell buildup activity at various altitudes. Radar features include: • Extended Sensitivity Time Constant (STC) logic that automatically correlates distance of the return echo with intensity, so cells do not suddenly appear to get larger as they get closer. • WATCH® (Weather ATtenuated Color Highlight) helps identify possible shadowing effects of short-range cell activity, identifying areas where radar return signals are weakened or attenuated by intense precipitation (or large areas of lesser precipitation) and may not fully reflect the weather behind a storm. • Weather Alert that looks ahead for intense cell activity in the 80-320 nm range, even if these ranges are not being displayed. PRINCIPLES OF PULSED AIRBORNE WEATHER RADAR The term RADAR is an acronym for RAdio Detecting And Ranging. Pulsed radar locates targets by transmitting a microwave pulse beam that, upon encountering a target, is reflected back to the radar receiver as a return echo. The microwave pulses are focused and radiated by the antenna, with the most intense energy in the center of the beam and decreasing intensity near the edge. The same antenna is used for both transmitting and receiving. The returned signal is then processed and displayed on the MFD. Radar detection is a two-way process that requires 12.36 µs for the transmitted microwave pulses to travel out and back for each nautical mile of target range. It takes 123.6 µs for a transmitted pulse to make the round trip if a target is ten nautical miles away. Airborne weather radar should be used to avoid severe weather, not for penetrating severe weather. The decision to fly into an area of radar targets depends on target intensity, spacing between the targets, aircraft capabilities, and pilot experience. Pulse type weather radar detects only precipitation, not clouds or turbulence. The display may indicate clear areas between intense returns, but this does not necessarily mean it is safe to fly between them. Only Doppler radar can detect turbulence. Airborne weather radar has other capabilities beyond weather detection. It also has the ability to detect and provide distance to cities, mountains, coastlines, rivers, lakes, and oceans. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 399 HAZARD AVOIDANCE NEXRAD AND AIRBORNE WEATHER RADAR Both Airborne Weather Radar and NEXRAD measure weather reflectivity in decibels (dB). A decibel is a logarithmic expression of the ratio of two quantities. Airborne Weather Radar measures the ratio of power against the gain of the antenna, while NEXRAD measures the energy reflected back to the radar, or the radar reflectivity ratio. Both systems use colors to identify the different echo intensities, but the colors are not interchangeable. Airborne color radar values used by Garmin Airborne Color Weather Radar should not be confused with NEXRAD radar values. ANTENNA BEAM ILLUMINATION The radar beam is much like the beam of a spotlight. The further the beam travels, the wider it becomes. The radar is only capable of seeing what is inside the boundaries of the beam. The figure below depicts a radar beam’s characteristics. The figure illustrates vertical dimensions of the radar beam, although the same holds true for the horizontal dimensions. In other words, the beam is as wide as it is tall. Note that it is possible to miss areas of precipitation on the radar display because of the antenna tilt setting. With the antenna tilt set to zero in this illustration, the beam overshoots the precipitation at 15 nautical miles. Altitude (x1000 ft.) 80 Antenna at Zero Tilt 18,000 ft. 8° 0 0 15 Half Power at s Beam Sidelobe Max Power at Beam Center 18,000 ft. 30 45 60 75 90 Range (nautical miles) Figure 6-88 Radar Beam from a 12 inch Antenna The curvature of the earth can also be a factor in missing areas of precipitation, especially at range settings of 150 nautical miles or more. Here the beam overshoots the precipitation at less than 320 nautical miles. 320 nm Figure 6-89 Radar Beam in Relation to the Curvature of the Earth 400 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE RADAR SIGNAL ATTENUATION The phenomenon of radar signal attenuation affects the operation of weather radar. When the radar signal is transmitted, it is progressively absorbed and scattered, making the signal weaker. This weakening, or attenuation, is caused by two primary sources, distance and precipitation. Attenuation because of distance is due to the fact that the radar energy leaving the antenna is inversely proportional to the square of the distance. The reflected radar energy from a target 40 miles away that fills the radar beam is one fourth the energy reflected from an equivalent target 20 miles away. This would appear to the operator that the storm is gaining intensity as the aircraft gets closer. Internal signal processing within the GWX 68 system compensates for much of this distance attenuation. Attenuation due to precipitation is not as predictable as distance attenuation. It is also more intense. As the radar signal passes through moisture, a portion of the radar energy is reflected back to the antenna. However, much of the energy is absorbed. If precipitation is very heavy, or covers a large area, the signal may not reach completely through the area of precipitation. The weather radar system cannot distinguish between an attenuated signal and an area of no precipitation. If the signal has been fully attenuated, the radar displays a radar shadow. This appears as an end to the precipitation when, in fact, the heavy rain may extend much further. A cell containing heavy precipitation may block another cell located behind the first, preventing it from being displayed on the radar. Never fly into these shadowed areas and never assume that all of the heavy precipitation is being displayed unless another cell or a ground target can be seen beyond the heavy cell. The WATCH® feature of the GWX 68 Weather Radar system can help in identifying these shadowed areas. Areas in question appear as shadowed or gray on the radar display. Proper use of the antenna tilt control can also help detect radar shadows. Attenuation can also be due to poor maintenance or degradation of the radome. Even the smallest amount of wear and scratching, pitting, and pinholes on the radome surface can cause damage and system inefficiency. RADAR SIGNAL REFLECTIVITY Precipitation Precipitation or objects more dense than water, such as the surface of the earth or solid structures, are detected by the weather radar. The weather radar does not detect clouds, thunderstorms, or turbulence directly. It detects precipitation associated with clouds, thunderstorms, and turbulence. The best radar signal reflectors are raindrops, wet snow, or wet hail. The larger the raindrop, the better the reflectivity. The size of the precipitation droplet is the most important factor in radar reflectivity. Because large drops in a small concentrated area are characteristic of a severe thunderstorm, the radar displays the storm as a strong return. Ice crystals, dry snow, and dry hail have low levels of reflectivity as shown in the illustration, and often not displayed by the radar. Additionally, a cloud that contains only small raindrops, such as fog or drizzle, does not reflect enough radar energy to produce a measurable target return. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 401 HAZARD AVOIDANCE Figure 6-90 Precipitation Type and Reflectivity Ground Returns The intensity of ground target returns depends upon the angle at which the radar beam strikes the ground target (Angle of Incidence) and the reflective properties of that target. The gain can be adjusted so shorelines, rivers, lakes, and cities are well defined. Increasing the gain too much causes the display to fill in between targets, thus obscuring some landmarks. Cities normally provide a strong return signal. While large buildings and structures provide good returns, small buildings can be shadowed from the radar beam by the taller buildings. As the aircraft approaches and shorter ranges are selected, details become more noticeable as the highly reflective regular lines and edges of the city become more defined. Bodies of water such as lakes, rivers, and oceans are not good reflectors and normally do not provide good returns. The energy is reflected in a forward scatter angle with inadequate energy being returned. They can appear as dark areas on the display. However, rough or choppy water is a better reflector and provides stronger returns from the downwind sides of the waves. Mountains also provide strong return signals to the antenna, but also block the areas behind. However, over mountainous terrain, the radar beam can be reflected back and forth in the mountain passes or off canyon walls, using up all or most of the radar energy. In this case, no return signal is received from this area, causing the display to show a dark spot which could indicate a pass where no pass exists. 402 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Angle of Incidence The angle at which the radar beam strikes the target is called the Angle of Incidence. The figure illustrates the incident angle (‘A’). This directly affects the detectable range, the area of illumination, and the intensity of the displayed target returns. A large incident angle gives the radar system a smaller detectable range and lower display intensity due to minimized reflection of the radar energy. Figure 6-91 Angle of Incidence A smaller incident angle gives the radar a larger detectable range of operation and the target display shows a higher intensity. Since more radar energy is reflected back to the antenna with a low incident angle, the resulting detectable range is increased for mountainous terrain. SAFE OPERATING DISTANCE The following information establishes a minimum safe distance from the antenna for personnel near operating weather radar. The minimum safe distance is based on the FCC’s exposure limit at 9.3 to 9.5 GHz for general population/uncontrolled environments, which is 1 mW/cm2. See Advisory Circular 20-68B for more information on safe distance determination. MAXIMUM PERMISSIBLE EXPOSURE LEVEL (MPEL) The zone in which the radiation level exceeds the US Government standard of 1 mW/cm2 is the semicircular area of at least 11 feet from the 12-inch antenna. All personnel must remain outside of this zone. With a scanning or rotating beam, the averaged power density at the MPEL boundary is significantly reduced. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 403 HAZARD AVOIDANCE MPEL Boundary 11’ for 12” antenna Figure 6-92 MPEL Boundary BASIC ANTENNA TILT SETUP The following discussion is a simple method for setting up the weather radar antenna tilt for most situations. It is not to be considered an all encompassing setup that works in all situations, but this method does provide good overall parameters for the monitoring of threats. Ultimately, it is desired to have the antenna tilted so that the bottom of the radar beam is four degrees below parallel with the ground. The following example explains one way of achieving this. With the aircraft flying level, adjust the antenna tilt so ground returns are displayed at a distance that equals the aircraft’s current altitude (AGL) divided by 1,000. For example, if the aircraft is at 14,000 feet, adjust the tilt so the front edge of ground returns are displayed at 14 nautical miles. Note this antenna tilt angle setting. Now, raise the antenna tilt 6 degrees above this setting. The bottom of the radar beam is now angled down 4º from parallel with the ground. 404 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE PRACTICAL APPLICATION USING THE BASIC TILT SETUP With the antenna tilt set as previously described, any displayed target return should be scrutinized when flying at altitudes between 2,000 and 30,000 feet AGL. If the displayed target advances on the screen to within five nautical miles of the aircraft, avoid it. This may be either weather or ground returns that are 2,000 feet or less below the aircraft. Raising the antenna tilt 4 degrees can help separate ground returns from weather returns in relatively flat terrain. This aligns the bottom of the radar beam parallel with the ground. Return the antenna tilt to the previous setting after a few sweeps. If the aircraft is above 29,000 feet, be cautious of any target return that gets to within 30 nautical miles. This is likely a thunderstorm that has a top high enough that the aircraft cannot fly over it safely. If the aircraft altitude is 15,000 feet or lower, setting the displayed range to 60 miles may be more helpful. Closely monitor anything that enters the display. 4000 Change in Antenna Tilt +4° +3° +2° +1° 0° -1° -2° -3° -4° 3000 2000 1000 0 1000 2000 3000 10 nm 4000 Vertical Change of Radar Beam (feet) Also, after setting up the antenna tilt angle as described previously, ground returns can be monitored for possible threats. The relationship between antenna tilt angle, altitude, and distance is one degree of tilt equals 100 feet of altitude for every one nautical mile. Figure 6-93 Vertical Change in Radar Beam per Nautical Mile Therefore, with the antenna tilt set so that the bottom of the beam is four degrees below parallel with the ground, a target return at 10 nm is approximately 4,000 feet below the aircraft; at 20 nm, 8,000 feet; at 50 nm, 20,000 feet. In other words, at this tilt setting, a ground return (such as a mountain peak) being displayed at 10 nm would have a maximum distance below the aircraft of 4,000 feet. A ground target return being displayed at 5 nm would have a maximum distance below the aircraft of 2,000 feet. This setup provides a good starting point for practical use of the GWX 68. There are many other factors to consider in order to become proficient at using weather radar in all situations. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 405 HAZARD AVOIDANCE WEATHER MAPPING AND INTERPRETATION WEATHER DISPLAY INTERPRETATION When evaluating various target returns on the weather radar display, the colors denote precipitation intensity and rates shown in the table. Weather Mode Color Intensity Black Green Yellow Red Magenta < 23 dBZ 23 dBZ to < 32 dBZ 32 dBZ to < 41 dBZ 41 dBZ to < 50 dBZ 50 dBZ and greater Approximate Precipitation Rate (in/hr.) < .01. .01 - 0.1. 0.1 - 0.5 0.5 - 2 >2 Table 6-10 Precipitation Intensity Levels Thunderstorms Updrafts and downdrafts in thunderstorms carry water through the cloud. The more severe the drafts, the greater the number and size of the precipitation droplets. With this in mind, the following interpretations can be made from what is displayed on the weather radar. Avoid these areas by an extra wide margin. • In areas where the displayed target intensity is red or magenta (indicating large amounts of precipitation), the turbulence is considered severe. • Areas that show steep color gradients (intense color changes) over thin bands or short distances suggest irregular rainfall rate and strong turbulence. • Areas that show red or magenta are associated with hail or turbulence, as well as heavy precipitation. Vertical scanning and antenna tilt management may be necessary to identify areas of maximum intensity. 406 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Along squall lines (multiple cells or clusters of cells in a line) individual cells may be in different stages of development. Areas between closely spaced, intense targets may contain developing clouds not having enough moisture to produce a return. However, these areas could have strong updrafts or downdrafts. Targets showing wide areas of green are generally precipitation without severe turbulence. Irregularities in the target return may also indicate turbulence, appearing as hooks, fingers, or scalloped edges. These irregularities may be present in green areas with no yellow, red, or magenta areas and should be treated as highly dangerous areas. Avoid these areas as if they are red or magenta. Squall Line Steep Gradient Hook or Finger Scalloped Edge Figure 6-94 Cell Irregularities Thunderstorm development is rapid. A course may become blocked within a short time. When displaying shorter ranges, periodically select a longer range to see if problems are developing further out. That can help prevent getting trapped in a blind alley or an area that is closed at one end by convective weather. Figure 6-95 The Blind Alley - Horizontal Scan 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 407 HAZARD AVOIDANCE In areas of multiple heavy cells, use the Vertical Scan feature along with antenna tilt management to examine the areas. Remember to avoid shadowed areas behind targets. The Blind Alley at Close Range The Large Storm Behind Figure 6-96 The Blind Alley Tornadoes There are no conclusive radar target return characteristics which identify a tornado. However, tornadoes may be present if the following characteristics are observed: • A narrow, finger-like portion extends and in a short time curls into a hook and closes on itself. • A hook, which may be in the general shape of the numeral 6 (numeral 9 in the southern hemisphere), especially if bright and projecting from the southwest quadrant (northeast quadrant in the southern hemisphere) of a major thunderstorm. • V-shaped notches. • Doughnut shapes. These shapes do not always indicate tornadoes, and tornado returns are not limited to these characteristics. Confirmed radar observations of tornadoes most often have not shown shapes different from those of a normal thunderstorm display. Hail Hail results from updrafts carrying water high enough to freeze. Therefore, the higher the top of a thunderstorm, the greater the probability that it contains hail. Vertically scanning the target return can give the radar top of a thunderstorm that contains hail. Radar top is the top of a storm cell as detected by radar. It is not the actual top, or true top of the storm. The actual top of a storm cell is seen with the eyes in clear air and may be much higher than the radar top. The actual top does not indicate the top of the hazardous area. Hail can fall below the minimum reflectivity threshold for radar detection. It can have a film of water on its surface, making its reflective characteristics similar to a very large water droplet. Because of this film of water, and because hail stones usually are larger than water droplets, thunderstorms with large amounts of wet hail return stronger signals than those with rain. Some hail shafts are extremely narrow (100 yards 408 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE or less) and make poor radar targets. In the upper regions of a cell where ice particles are dry (no liquid coating), target returns are less intense. Hail shafts are associated with the same radar target return characteristics as tornados. U-shaped cloud edges three to seven miles across can also indicate hail. These target returns appear quite suddenly along any edge of the cell outline. They also change in intensity and shape in a matter of seconds, making vigilant monitoring essential. OPERATION IN WEATHER MODE WARNING: Begin transmitting only when it is safe to do so. When transmitting while the aircraft is on the ground, no personnel or objects should be within 11 feet of the antenna. CAUTION: In Standby mode, the antenna is parked at the center line. It is always a good idea to put the radar in Standby mode before taxiing the aircraft to prevent the antenna from bouncing on the bottom stop and possibly causing damage to the radar assembly. When the weather radar system is in the Weather or Ground Map mode, the system automatically switches to Standby mode on landing. In Reversionary mode, the weather radar system automatically switches to Standby mode. The system remains in Standby mode until both displays are restored. In Reversionary mode, the weather radar system cannot be controlled. Radar Mode Scan Line Antenna Stabilization Status Figure 6-97 Horizontal Scan Display 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 409 HAZARD AVOIDANCE Displaying weather on the Weather Radar Page: 1) Select the Weather Radar Page in the Map Page Group with the FMS Knob. 2) Select the MODE Softkey. 3) While on the ground, select the STANDBY Softkey. A one-minute warm-up period is initiated (countdown is displayed on the screen). After the warm-up is complete, the radar enters the Standby Mode. a) Select the WEATHER Softkey. A confirmation window is displayed. Figure 6-98 Confirming Activating Radar b) Turn the small FMS Knob to highlight YES and press the ENT Key to continue radar activation. Or: If the aircraft is airborne, select the WEATHER Softkey. A 1 minute warm-up period is initiated (countdown is displayed on the screen). After the warm-up is complete, the radar begins transmitting. 4) Turn the Joystick to select the desired map range. 5) The horizontal scan is initially displayed (Figure 6-97). If desired, select the VERTICAL Softkey to change to vertical scanning. 410 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Vertically scanning a storm cell: NOTE: Vertical scanning of a storm cell should be done with the aircraft wings level to avoid constant adjustment of the Bearing Line. 1) While in the Horizontal Scan view, select the BRG Softkey. This places the cursor in the BEARING field and displays the Bearing Line. If the Bearing Line is not displayed, press the MENU Key and turn the large FMS Knob to select Show Bearing Line. Press the ENT Key. 2) Press the ENT Key. 3) Turn the small FMS Knob to place the Bearing Line on the desired storm cell or other area to be vertically scanned. Scan Line Bearing Line Figure 6-99 Bearing Line on Horizontal Scan 4) Select the VERTICAL Softkey. A vertical scan of the selected area is displayed (Figure 6-100). 5) The small FMS Knob may be used to move the scanned bearing line a few degrees right or left. 6) Turn the Joystick to adjust the range. 7) Press the FMS Knob to remove the cursor. 8) To select a new area to be vertically scanned, select the HORIZON Softkey to return to the Horizontal Scan view and repeat the previous steps. The Joystick can also be used to adjust bearing from left to right. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 411 HAZARD AVOIDANCE Figure 6-100 Vertical Scan Display Adjusting Antenna Tilt Angle In order to make an accurate interpretation of a storm cell, the radar beam should be pointed at the wet part of the weather cell to record the proper rainfall intensity (color level). The ideal aiming point is just below the freezing level of the storm. The best way to find this point is to use the Vertical Scan feature. The antenna tilt angle can be centered on the strongest return area in the vertical scan to get a more accurate view of the coverage and intensity of the target in the horizontal scan. Adjusting antenna tilt on the Horizontal Scan display: 1) Press the FMS Knob to activate the cursor in the TILT field. 2) Turn the small FMS Knob to select the desired antenna tilt angle. 3) Press the ENT Key. 4) Press the FMS Knob to remove the cursor. The Joystick can also be used to adjust tilt up and down. 412 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Adjusting antenna tilt on the Vertical Scan display: 1) Select the TILT Softkey to activate the cursor in the TILT field and display the Tilt Line. If the Tilt Line is not displayed, press the MENU Key and turn the large FMS Knob to select Show Tilt Line. Press the ENT Key. 2) Turn the small FMS Knob to adjust the antenna tilt angle. The selected tilt angle is implemented when Horizontal Scan is selected again. The Joystick can also be used to adjust tilt. Tilt Line Scan Line Figure 6-101 Adjusting Tilt on Vertical Scan Display 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 413 HAZARD AVOIDANCE Adjusting Gain: WARNING: Changing the gain in weather mode causes precipitation intensity to be displayed as a color not representative of the true intensity. Remember to return the gain setting to Calibrated for viewing the actual intensity of precipitation. 1) Select the GAIN Softkey to activate the cursor in the GAIN field. 2) Turn the small FMS Knob to adjust the gain for the desirable level. The gain setting is visible in the GAIN field as a movable horizontal bar in a flashing box. The line pointer is a reference depicting the calibrated position. 3) Press the FMS Knob to remove the cursor. 4) Select the GAIN Softkey again to recalibrate the gain. ‘CALIBRATED’ is displayed in the GAIN field. Manual Gain Set Below Calibrated Calibrated Gain Figure 6-102 Gain Calibration 414 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Sector Scan: 1) While in horizontal scan mode, select the BRG Softkey to display the Bearing Line and place the cursor in the BEARING field. If the Bearing Line is not displayed, press the MENU Key and turn the large FMS Knob to select Show Bearing Line. 2) Press the ENT Key. Figure 6-103 Selecting Sector Scan Position 3) Turn the small FMS Knob to place the Bearing Line in the desired position. The location of the Bearing Line becomes the center point of the Sector Scan. 4) Turn the large FMS Knob to place the cursor in the SECTOR SCAN field. 5) Turn the small FMS Knob to select FULL, 60˚, 40˚, or 20˚ scan. 6) If desired, readjust the Bearing Line as discussed previously to change the center of the Sector Scan. 7) Select the BRG Softkey again to remove the Bearing Line and cursor. The bearing reference is reset to 0º. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 415 HAZARD AVOIDANCE Figure 6-104 40˚ Sector Scan Antenna Stabilization When radar stabilization is active, the radar tilt is corrected for pitch and roll, and therefore is kept steady with respect to the horizon. The commanded tilt angle is kept constant with respect to the earth. When the stabilization is disabled, corrections are no longer made for pitch and roll, and the radar tilt angle is kept constant with respect to the aircraft reference system. Enabling/Disabling Antenna Stabilization: 1) To activate or deactivate the antenna stabilization, select the MODE Softkey. 2) Select the STAB ON Softkey to activate antenna stabilization or select the STAB OFF Softkey to deactivate. The current stabilization condition is shown in the upper right of the weather radar display. Weather Attenuated Color Highlight (WATCH®) WATCH® identifies deceptively strong or unknown intensity parts of a storm. While in horizontal scan mode, this feature can be used as a tool to determine areas of possible inaccuracies in displayed intensity due to weakening of the radar energy. This weakening is known as attenuation. The radar energy weakens as it passes through areas of intense precipitation, large areas of lesser precipitation, and distance. Issues with the radome attenuates the radar energy. All these factors have an effect on the return intensity. The more energy that dissipates, the lesser the displayed intensity of the return. Accuracy of the displayed intensity of returns located in the shaded areas are suspect. Make maneuvering decisions with this information in mind. Proper antenna tilt management should still be employed to determine the extent of attenuation in a shaded area. To activate or deactivate the WATCH® feature, select the WATCH Softkey. 416 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Displayed intensity is questionable. Potentially stronger than displayed. Horizontal Scan Without WATCH® Areas of Attenuated Signal Horizontal Scan With WATCH® Figure 6-105 Horizontal Scan Without and With WATCH® Weather Alert Target Bands and Alerts Window Message The Weather Alert feature indicates the presence of heavy precipitation between the ranges of 80 and 320 nm regardless of the currently displayed range. Weather Alert targets appear as red bands along the outer range ring at the approximate azimuth of the detected returns. If a Weather Alert is detected within ±10° of the aircraft heading, and the WX ALRT Softkey is enabled on the Weather Radar Page, the system also displays ‘WX ALERT - Possible severe weather ahead.’ on the PFD in the Messages Window. If the antenna tilt is adjusted too low, a weather alert can be generated by ground returns. To avoid unwanted weather alerts, deselect the WX ALRT Softkey. Weather Alert Target Bands Figure 6-106 Weather Alert Indications 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 417 HAZARD AVOIDANCE To enable or disable the Weather Alerts which appear in the Messages Window on the PFD, select the WX ALRT Softkey. The system continues to display weather alert target bands on the Weather Radar Page even if the PFD weather alert message is disabled. Figure 6-107 Weather Alert on PFD GROUND MAPPING AND INTERPRETATION A secondary use of the weather radar system is for the presentation of terrain. This can be a useful tool for verifying aircraft position. A picture of the ground is represented much like a topographical map that can be used as a supplement to the navigation map on the MFD. Ground Map mode uses a different gain range than Weather mode. Different colors are also used to represent the intensity levels. The displayed intensity of ground target returns are defined in the table below. Use of the GAIN and TILT controls help improve contrast so that specific ground targets can be recognized more easily. As previously discussed, the type and orientation of the target in relation to the aircraft affects the intensity displayed. When the weather radar system is in either the Weather or Ground Map mode, the system automatically switches to Standby mode upon landing. Ground Map Mode Color Black Light blue Yellow Magenta Blue Intensity 0 dB > 0 dB to < 9 dB 9 dB to < 18 dB 18 dB to < 27 dB 27 dB and greater Table 6-11 Ground Target Return Intensity Levels Operation in Ground Map Mode 1) Select the MODE Softkey. 2) Select the GROUND Softkey to place the radar in Ground Map mode. 3) Select the BACK Softkey. 4) Select the FMS Knob to activate the cursor. 5) Turn the large FMS Knob to place the cursor in the TILT field. 6) Adjust the antenna tilt angle by turning the small FMS Knob to display ground returns at the desired distance. 7) Press the FMS Knob to remove the cursor. 418 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE WEATHER RADAR OVERLAY ON THE NAVIGATION MAP PAGE The Map - Weather Radar Page is the principal map page for viewing airborne weather radar information. Weather radar information may also be shown as an overlay on the Navigation Map Page on the MFD as an additional reference. When the airborne weather radar overlay is enabled, a weather radar information box appears in the upperright corner of the Navigation Map Page. It indicates the selected weather mode, radar bearing, and antenna tilt angle. The overlay is capable of showing radar information while the radar is in horizontal scan mode. If the radar is operating in vertical scan mode while the overlay is enabled, the system indicates ‘N/A’ in the information box to indicate the airborne weather radar overlay is not available until the horizontal scan mode is selected on the Weather Radar Page. Radar Overlay Enabled Icon Radar Mode Selected Radar Bearing Radar Range Scan Line Antenna Tilt Angle Boundary of Selected Radar Scan Navigation Map Range Figure 6-108 Airborne Weather Radar Overlay on the Navigation Map Page Enabling/Disabling Airborne Weather Radar Overlay on the Navigation Map Page: 1) Select the Navigation Map Page. 2) Select the MAP Softkey. 3) Select the WX RADAR Softkey. Or: 1) On the Navigation Map Page, press the MENU Key. 2) With ‘Map Setup’ highlighted, press the ENT Key. 3) Turn the small FMS Knob to select the ‘Weather’ group, then press the ENT Key. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 419 HAZARD AVOIDANCE 4) Turn the large FMS Knob to scroll through the product selections and highlight the WX RADAR overlay selection (‘On’ or ‘Off’). Turn the small FMS knob to highlight the desired selection. 5) To remove the menu, press the FMS Knob or CLR Key. Weather radar controls on the Navigation Map Page are limited to adjustment of the radar range, bearing, and antenna tilt angle. The airborne weather radar overlay is viewable at Navigation Map Ranges between five and 800 nautical miles (ten to 1,500 kilometers). At map ranges beyond these limits, the system removes the weather radar information from the map. Adjusting the range on the Navigation Map Page simultaneously adjusts the range of the weather radar proportionally. This radar range is annunciated on the range arc that appears when the overlay is enabled and a radar scan is active. When the radar range is adjusted on the Navigation Map Page, system synchronizes the same range to the Weather Radar Page. The radar bearing is adjustable in one degree increments on the Navigation Map Page by pushing the Joystick left or right when the overlay is enabled. A left or right arrow next to the bearing readout indicates the direction of the selected bearing. The cyan radar bearing line is only viewable on the Weather Radar Page. While the bearing line is not shown on the Navigation Map Page, adjusting the bearing on the Navigation Map Page while Sector Scan is enabled centers the radar scan on the selected bearing, and the radar scan boundaries adjust accordingly on the Navigation Map Page. Radar antenna tilt angle is adjustable in 0.25 degree increments on the Navigation Map Page. Push the Joystick up to adjust the antenna tilt angle downward. Push the Joystick down to adjust the antenna tilt angle upward. An up or down arrow next to the antenna tilt angle setting indicates the direction of the antenna tilt angle. The weather radar overlay uses the same colors as those shown on the Weather Radar Page to indicate the intensity of radar returns. However, the display of gray WATCH radar attenuation and red weather alert target bands is exclusive to the Weather Radar Page. Because data link radar precipitation and terrain present information using similar colors, enabling the airborne weather radar overlay on the Navigation Map Page disables the display of the data link radar and terrain information for this page. SYSTEM STATUS The system displays the radar mode annunciation in the upper left corner of the Weather Radar Page. It also appears in the upper right corner of the Navigation Map Page when the Weather Radar overlay is enabled. Additional information may be displayed in the center of the Weather Radar Page as a banner annunciation. Radar Mode Radar Mode Annunciation Box (Weather Radar Page and Navigation Map Page) Weather Radar Page Center Banner Annunciation Standby STANDBY STANDBY Standby (During Warm-Up) STANDBY WARM-UP XX (XX indicates number of seconds remaining in warm-up) Weather WEATHER None Ground Mapping Off Radar Failed* GROUND MAPPING OFF FAIL None OFF RADAR FAIL * See Table 6-13 for additional failure annunciations Table 6-12 Radar Modes on the Weather Radar Page 420 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE The system displays the status of the radar antenna stabilization feature in the upper right corner of the Weather Radar Page. Radar Antenna Description Stabilization Status STAB ON Antenna stabilization is selected on. STAB OFF Antenna stabilization is selected off. The radar is not receiving pitch and roll information. STAB INOP The antenna stabilization feature is inoperative. Table 6-13 Antenna Stabilization Annunciations on the Weather Radar Page If the unit fails, an annunciation as to the cause of the failure is shown as a banner in the center of the Weather Radar Page Weather Radar Page Center Banner Description Annunciation BAD CONFIG The radar configuration is invalid. The radar should be serviced. RDR FAULT The radar unit is reporting a fault. The radar should be serviced. The system is not receiving valid data from the radar unit. The system RADAR FAIL should be serviced. Table 6-14 Abnormal Radar Status Annunciations on the Weather Radar Page 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 421 HAZARD AVOIDANCE 6.4 TAWS-B WARNING: Do not use TAWS information for primary terrain and obstacle avoidance. TAWS is intended only to enhance situational awareness. NOTE: Terrain and obstacle information is not displayed if the aircraft is outside of the installed terrain database coverage area. NOTE: The data contained in the TAWS databases comes from government agencies. Garmin accurately processes and cross-validates the data but cannot guarantee the accuracy and completeness of the data. TAWS-B (Terrain Awareness and Warning System - Class B) provides increased situational awareness and aids in reducing controlled flight into terrain (CFIT). TAWS-B provides visual annunciations and voice alerts when terrain and obstacles are within the given altitude threshold from the aircraft. The displayed alerts and warnings are advisory in nature only. TAWS-B satisfies TSO-C151b Class B requirements for certification. TAWS-B requires the following to operate properly: • A valid terrain/obstacle/airport terrain database • A valid 3-D GPS position solution TAWS-B uses terrain and obstacle information supplied by government sources. Terrain information is based on terrain elevation information in a database that may contain inaccuracies. Individual obstructions may be shown if available in the database. Garmin verifies the data to confirm accuracy of the content, per TSO-C151b. However, the displayed information should never be understood as being all-inclusive and data may be inaccurate. TAWS-B uses information provided from the GPS receiver to provide a horizontal position and altitude. GPS altitude is derived from satellite measurements. GPS altitude is then converted to the height above geodetic sea level (GSL), which is the height above mean sea level (MSL) calculated geometrically. The system uses GSL altitude to determine TAWS-B alerts. GSL altitude accuracy is affected by satellite geometry, but is not subject to variations in pressure and temperature that normally affect pressure altitude sensors. GSL altitude does not require local altimeter settings to determine MSL altitude. It is a widely-used MSL altitude source. Therefore, GSL altitude provides a highly accurate and reliable MSL altitude source to calculate terrain and obstacle alerts. The terrain and obstacle databases used by TAWS-B are referenced to MSL. Using the GPS position and GSL altitude, TAWS-B displays a 2-D picture of the surrounding terrain and obstacles relative to the position and altitude of the aircraft. Furthermore, the system uses the GPS position and GSL altitude to calculate and “predict” the aircraft’s flight path in relation to the surrounding terrain and obstacles. In this manner, TAWS-B can provide advanced alerts of predicted dangerous terrain and obstacle conditions. Baro-corrected altitude (or indicated altitude) is derived by adjusting the altimeter setting for local atmospheric conditions. The most accurate baro-corrected altitude can be achieved by frequently updating the altimeter setting to the nearest reporting station along the flight path. However, because actual atmospheric conditions seldom match the standard conditions defined by the International Standard Atmosphere (ISA) model (where pressure, temperature, and lapse rates have fixed values), it is common for the baro-corrected altitude (as read from the altimeter) to differ from the GSL altitude shown on the TAWS-B Page. 422 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE DISPLAYING TAWS-B DATA TAWS-B uses yellow (caution) and red (warning) to depict terrain and obstacles (with heights greater than 200 feet above ground level, AGL) alerts relative to aircraft altitude. Colors are adjusted automatically as the aircraft altitude changes. The colors and symbols in the figure and tables below are used to represent terrain, obstacles, and potential impact points. Figure 6-109 Terrain Altitude/Color Correlation for TAWS-B Unlighted Obstacle Lighted Obstacle < 1000’ AGL > 1000’ AGL < 1000’ AGL > 1000’ AGL Obstacle Location Red obstacle is above or within 100 ft below the aircraft altitude Yellow obstacle is between 100 ft and 1000 ft below the aircraft altitude Gray obstacle* is more than 1000 ft below aircraft altitude * Gray obstacles not shown on the TAWS-B Page. Table 6-15 TAWS-B Obstacle Colors and Symbology Potential Impact Point Symbol Alert Type Example Annunciation Warning Caution Table 6-16 TAWS-B Potential Impact Point Symbols with Alert Types 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 423 HAZARD AVOIDANCE TAWS-B information can be displayed on the following maps: • PFD Inset Navigation Map • Trip Planning Page • Navigation Map Page • Flight Plan Pages • TAWS-B Page • System Pages (when terrain is enabled on the Navigation Map Page) TAWS-B relative terrain and obstacle information is also available for display in the optional Profile View Window on the Navigation Map Page. Refer to the Profile View Terrain discussion in this section for more information. Displaying terrain and obstacle information (maps except the TAWS-B Page or PFD Inset Navigation Map): 1) Press the MAP Softkey. 2) Press the TERRAIN Softkey to display terrain and obstacle data. Displaying terrain and obstacle information on the PFD Inset Navigation Map: 1) On the PFD, press the INSET Softkey (in non-TCAS II installations) or the TRFC/MAP Softkey (TCAS II installations). 2) If the PFD Inset Map is showing the traffic map, press the TFRC-2 Softkey to display the navigation map. 3) Press the TERRAIN Softkey to display terrain and obstacle data. The system displays a TAWS-B icon with the terrain legend when terrain and obstacles are enabled on MFD maps. The legend appears without the terrain icon on the dedicated TAWS-B Page. Figure 6-110 TAWS-B Icon and Legend The Navigation Map Page Setup Menu provides a means in addition to the softkey for enabling/disabling display of terrain and obstacles. The setup menu also controls the map range settings above which terrain and obstacle data are decluttered from the display. If the crew selects a map range larger than the selected map range setting, the data is removed from the map. For terrain data, the enable/disable function applies only to the MFD, while the range setting also affects the PFD Inset Map. Terrain data can be selected for display independently of obstacle data; however, obstacles for which warnings and cautions are issued are shown when terrain is selected for display and the map range is within the setting limit. Maps besides the TAWS-B Page use settings based on those selected for the Navigation Map Page. The maximum display ranges for obstacles on each map are dependent on the range setting made for the Navigation Map. If the maximum range for obstacle display on the Navigation Map is adjusted to below 20 nm, the highest obstacle display range settings on the other applicable maps are also adjusted proportionally. 424 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Customizing terrain and obstacle display on the Navigation Map Page: 1) Select the Navigation Map Page. 2) Press the MENU Key. 3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-111). 4) Turn the small FMS Knob to select the ‘Map’ Group and press the ENT Key (Figure 6-112). 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-113). • TERRAIN DATA – Enables/disables display of terrain data and sets maximum range at which terrain is shown • OBSTACLE DATA – Enables/disables display off obstacle data and sets maximum range at which obstacles are shown 6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings). 7) Press the ENT Key to select an option. 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. Figure 6-111 Navigation Map Page Menu Figure 6-112 Navigation Map Page Setup Menu 190-00728-06 Rev. A Figure 6-113 Navigation Map Page Setup Menu, Map Group Embraer Prodigy® Flight Deck 100 Pilot’s Guide 425 HAZARD AVOIDANCE TAWS-B PAGE The Map - TAWS-B Page is specialized to show terrain, obstacle, and potential impact point data in relation to the aircraft’s current altitude, without clutter from the basemap. It is the principal map page for viewing TAWS-B information. Aviation data (airports, VORs, and other NAVAIDs) can be displayed for reference. If an obstacle and the projected flight path of the aircraft intersect, the display automatically zooms in to the closest potential point of impact on the TAWS-B Page. Aircraft orientation on this map is always heading up unless there is no valid heading. Two views are available relative to the position of the aircraft: the 360° default display and the radar-like ARC (120°) display. Map range is adjustable with the Joystick from one to 200 nm, as indicated by the map range rings (or arcs). Displaying the TAWS-B Page: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the TAWS-B Page. Changing the TAWS-B Page view: 1) Select the VIEW Softkey. 2) Select the 360 or ARC Softkey to select the desired view. Or: 1) Press the MENU Key. 2) Select ‘View Arc’ or ‘View 360º’ (choice dependent on current state) and press the ENT Key to change the view Showing/hiding aviation information on the TAWS-B Page: 1) Press the MENU Key. 2) Select ‘Show Aviation Data’ or ‘Hide Aviation Data’ (choice dependent on current state) and press the ENT Key. 426 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Red Terrain (Terrain Above or Within 100’ Below the Aircraft Altitude) Aircraft Altitude Above Geodetic Sea Level (GSL) Black Terrain (Terrain More than 1000’ Below the Aircraft Altitude) Red obstacle is above or within 100’ below the aircraft altitude Yellow Terrain (Terrain Between 100’ and 1000’ Below the Aircraft Altitude) Map Range Rings Yellow obstacle is between 100’ and 1000’ Below the Aircraft Altitude Terrain Legend Annunciation Window Figure 6-114 TAWS-B Page Red Terrain (Terrain Above or Within 100’ Below the Aircraft Altitude) Aircraft Altitude Above Geodetic Sea Level (GSL) Map Range Arc Black Terrain (Terrain More than 1000’ Below the Aircraft Altitude) Yellow Terrain (Terrain Between 100’ and 1000’ Below the Aircraft Altitude) Yellow obstacle is between 100’ and 1000’ below the aircraft altitude Red obstacle is above or within 100’ below the aircraft altitude Terrain Legend Annunciation Window Figure 6-115 TAWS-B Page (ARC View) 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 427 HAZARD AVOIDANCE TAWS-B ALERTS Alerts are issued when flight conditions meet parameters that are set within TAWS-B software algorithms. TAWS-B alerts typically employ a CAUTION or a WARNING alert severity level, or both. When an alert is issued, the system provides visual annunciations and voice alerts. Table 6-17 shows TAWS-B alert types with corresponding annunciations and voice alerts. When an alert is issued, annunciations appear on the PFD and MFD. The TAWS-B Alert Annunciation is shown to the upper left of the Altimeter on the PFD and below the Terrain Legend on the MFD. If the TAWS-B Page is not displayed at the time, a pop-up alert appears on the MFD. To acknowledge the pop-up alert: • Press the CLR Key (returns to the currently viewed page), or • Press the ENT Key (accesses the TAWS-B Page) Alert Annunciation Figure 6-116 TAWS-B PFD Alert Annunciation Figure 6-117 Navigation Map Page TAWS-B Pop-up Alert Terrain Display Enabled Terrain Legend Alert Annunciation Figure 6-118 Navigation Map Page (After TAWS-B Pop-up Alert Acknowledgment) 428 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Alert Type Excessive Descent Rate Warning (EDR) Reduced Required Terrain Clearance Warning (RTC) Imminent Terrain Impact Warning (ITI) Reduced Required Obstacle Clearance Warning (ROC) Imminent Obstacle Impact Warning (IOI) Reduced Required Terrain Clearance Caution (RTC) Imminent Terrain Impact Caution (ITI) Reduced Required Obstacle Clearance Caution (ROC) Imminent Obstacle Impact Caution (IOI) Premature Descent Alert Caution (PDA) Negative Climb Rate Caution (NCR) Excessive Descent Rate Caution (EDR) Altitude Voice Callout (VCO) PFD/MFD TAWS-B Page Annunciation MFD Map Page Pop-Up Alert (except TAWS-B Page) Voice Alert “Pull Up” “Terrain, Terrain; Pull Up, Pull Up” “Terrain, Terrain; Pull Up, Pull Up” “Obstacle, Obstacle; Pull Up, Pull Up” “Obstacle, Obstacle; Pull Up, Pull Up” “Caution, Terrain; Caution, Terrain” “Caution, Terrain; Caution, Terrain” “Caution, Obstacle; Caution, Obstacle” “Caution, Obstacle; Caution, Obstacle” “Too Low, Terrain” “Don’t Sink” “Sink Rate” None None “Five-Hundred” Table 6-17 TAWS-B Alerts 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 429 HAZARD AVOIDANCE EXCESSIVE DESCENT RATE ALERT The purpose of the Excessive Descent Rate (EDR) alert is to provide suitable notification when the aircraft is determined to be closing (descending) upon terrain at an excessive speed. Figure 6-119 shows the parameters for the alert as defined by TSO-C151b. 6000 5500 5000 Height Above Terrain (Feet) 4500 4000 NK : “SI ion Caut 3500 ” RATE 3000 2500 2000 Warning: “PULL UP” 1500 1000 12000 11000 Descent Rate (FPM) 10000 9000 8000 7000 6000 5000 4000 3000 2000 1000 0 0 500 Figure 6-119 Excessive Descent Rate Alert Criteria FORWARD LOOKING TERRAIN AVOIDANCE (FLTA) The Forward Looking Terrain Avoidance feature of TAWS-B compares the aircraft’s projected flight path with known terrain and obstacles in their respective databases and issues four types of alerts as either a caution or a warning: Reduced Required Terrain Clearance (RTC) and Reduced Required Obstacle Clearance (ROC) alerts are issued when the aircraft flight path is above terrain, yet is projected to come within the minimum clearance values in Figure 6-120. When an RTC alert is issued, a potential impact point is displayed on the TAWS-B Page. Imminent Terrain Impact (ITI) and Imminent Obstacle Impact (IOI) alerts are issued when the aircraft is below the elevation of a terrain or obstacle cell in the aircraft’s projected path. ITI and IOI alerts are accompanied by a potential impact point displayed on the TAWS-B Page. The alert is annunciated when the projected vertical flight path is calculated to come within minimum clearance altitudes in Figure 6-120. 430 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Required Terrain Clearance RTC Level (FT) RTC Descending (FT) 800 700 Required Terrain Clearance (FT) 600 500 400 300 200 100 0 0 5 10 15 20 25 30 Distance From Runway (NM) Figure 6-120 FLTA Minimum Terrain and Obstacle Values FLTA alerts are automatically inhibited when the aircraft is less than 200 feet above the destination runway elevation while within 0.5 nm of the approach runway or the aircraft is between runway ends. PREMATURE DESCENT ALERTING A Premature Descent Alert (PDA) is issued when the system detects that the aircraft is significantly below the normal approach path to a runway (Figure 6-121). PDA alerting begins when the aircraft is below 700 feet AGL within 15 nm of the destination airport and ends when the aircraft is 0.5 nm from the runway threshold. 800 Height Above Destination (Feet) 700 600 500 400 300 PDA ALERTING AREA 200 100 15 14 13 12 11 10 9 8 7 6 5 4 3 2 1 0 0 Distance to Destination (NM) Figure 6-121 PDA Alerting Threshold PDA and FLTA visual annunciations and voice alerts can be manually inhibited. Discretion should be used when inhibiting these alerts, and the system should be enabled when appropriate. When PDA and FLTA alerts are inhibited, the alert annunciation ‘TAWS INH’ is shown on the PFD and MFD (Figure 6-122). 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 431 HAZARD AVOIDANCE Figure 6-122 TAWS Alerting Disabled (TAWS-B Inhibited) Annunciation Inhibiting/enabling TAWS-B PDA and FLTA alerting: 1) Select the TAWS-B Page. 2) Select the INHIBIT Softkey to inhibit or enable TAWS (choice dependent on current state). Or: a) Press the MENU Key. b) Select ‘Inhibit TAWS’ or ‘Enable TAWS’ (choice dependent on current state) and press the ENT Key. If TAWS-B alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS approach, a ‘LOW ALT’ annunciation may appear on the PFD next to the Altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix. See the Flight Instruments Section for details. FIVE HUNDRED ALTITUDE VOICE CALLOUT ALERT The purpose of the voice alert “Five-hundred” is to provide an advisory alert of when the aircraft descends to within 500 feet above the terrain or runway threshold. When the aircraft is within 5 nm of an airport, the “Five Hundred” voice alert is based on the nearest runway threshold elevation. When the aircraft is more than 5 nm of the nearest airport, the “Five Hundred” voice alert is based on the height above terrain. There are no display annunciations or pop-up alerts that accompany the “Five Hundred” voice alert. NEGATIVE CLIMB RATE AFTER TAKEOFF ALERT The Negative Climb Rate (NCR) After Takeoff alert (also referred to as “Altitude Loss After Takeoff”) provides alerts when the system determines the aircraft is losing altitude (closing upon terrain) after takeoff. The voice alert “Don’t Sink” is given for NCR alerts, accompanied by an annunciation and a pop-up terrain alert on the display. NCR alerting is only active when departing from an airport and when the following conditions are met: • Height above the terrain is less than 700 feet • Distance from the departure airport is 2 nm or less • Heading change from the departure heading is less than 110 degrees Figures 6-114 and 6-115 shows the NCR alerting parameters based on altitude loss and sink rate, respectively, as defined by TSO-C151b. 432 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE 1000 Height Above Terrain (Feet) 900 800 700 600 500 “DON’T SINK” 400 300 200 100 0 0 20 40 60 80 100 120 140 Altitude Loss (Feet) Figure 6-123 Negative Climb Rate (NCR) Altitude Loss 1000 Height Above Terrain (Feet) 900 800 700 600 500 400 “DON’T SINK” 300 200 100 0 0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000 5500 6000 6500 7000 Sink Rate (FPM) Figure 6-124 Negative Climb Rate (NCR) Sink Rate 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 433 HAZARD AVOIDANCE SYSTEM STATUS During power-up, TAWS-B conducts a self-test of its visual annunciations and voice alerts. The system test can also be manually initiated. The system issues a voice alert when the test has concluded. TAWS-B System Testing is disabled when ground speed exceeds 30 knots. PFD/MFD Alert Annunciation Alert Type System Test in Progress System Test Pass None TAWS-B System Test Fail TAWS-B Page Center Annunciation Voice Alert TAWS TEST None None “TAWS System Test OK” TAWS FAIL “TAWS System Failure” Table 6-18 TAWS-B System Test Status Annunciations Manually testing the TAWS-B System: 1) Select the TAWS-B Page. 2) Press the MENU Key (Figure 6-125). 3) Select ‘Test TAWS System’ and press the ENT Key to confirm the selection. Figure 6-125 TAWS-B Page Menu TAWS-B continually monitors several system-critical items such as database validity, hardware status, and GPS status. If the terrain/obstacle database is not available, the voice alert “TAWS System Failure” is generated along with the ‘TAWS FAIL’ alert annunciation. TAWS-B requires a 3-D GPS navigation solution along with specific vertical accuracy minimums. Should the navigation solution become degraded or if the aircraft is out of the database coverage area, the annunciation ‘TAWS N/A’ is generated in the annunciation window and on the TAWS-B Page. The voice alert “TAWS Not Available” is generated. When sufficient GPS signal is received and the aircraft is within the terrain database coverage area, the voice alert “TAWS Available” is generated. 434 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Alert Cause MFD Terrain or Obstacle database unavailable or invalid. TAWS operating with PFD Terrain or Obstacle databases Terrain or Obstacle database unavailable or invalid on all displays, invalid software configuration, TAWS audio fault No GPS position PFD/MFD* Annunciation None TAWS-B Page Center Banner Annunciation Voice Alert TERRAIN DATABASE FAILURE None TAWS FAIL “TAWS System Failure” NO GPS POSITION “TAWS Not Available” None “TAWS Not Available” Excessively degraded GPS signal, aircraft outside of terrain database coverage area *Annunciation appears on MFD pages when terrain is displayed. Table 6-19 TAWS-B Abnormal Conditions 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 435 HAZARD AVOIDANCE 6.5 TAWS-A WARNING: Do not use TAWS information for primary terrain and obstacle avoidance. TAWS-A is intended only to enhance situational awareness. NOTE: Terrain and obstacle information is not displayed when the aircraft is outside of the installed database coverage area. NOTE: The data contained in the TAWS databases comes from government agencies. Garmin accurately processes and cross-validates the data but cannot guarantee the accuracy and completeness of the data. TAWS-A (Terrain Awareness and Warning System - Class A) is an optional feature designed to increase situational awareness and aid in reducing controlled flight into terrain (CFIT). TAWS-A provides visual annunciations and voice alerts when terrain and obstacles are within the given altitude threshold from the aircraft. The displayed alerts and warnings are advisory in nature only. When TAWS-A is installed, it supersedes the TAWS-B feature. TAWS-A satisfies TSO-C151b Class A and TSO-92c requirements for certification. Class A TAWS requires the following components: • A valid terrain, obstacle, and airport terrain database • A valid 3-D GPS position solution • Valid flap and landing gear status inputs • A valid radar altimeter TAWS-A uses terrain and obstacle information supplied by government sources. Terrain information is based on terrain elevation information in a database that may contain inaccuracies. Individual obstructions may be shown if available in the database. The data undergoes verification by Garmin to confirm accuracy of the content, per TSO-C151b. However, the displayed information should never be understood as being all-inclusive and data may be inaccurate. TAWS-A uses information from the GPS receiver to provide a horizontal position and altitude, along with additional altitude input from the radar altimeter. GPS altitude is derived from satellite measurements. GPS altitude is then converted to the height above geodetic sea level (GSL), which is the height above mean sea level (MSL) calculated geometrically. GSL altitude is used in part to determine TAWS-A alerts. GSL altitude accuracy is affected by satellite geometry, but is not subject to variations in pressure and temperature that normally affect pressure altitude sensors. GSL altitude does not require local altimeter settings to determine MSL altitude. It is a widely-used MSL altitude source. Therefore, GSL altitude provides a highly accurate and reliable MSL altitude source to calculate terrain and obstacle alerts. The terrain and obstacle databases are referenced to mean sea level (MSL). Using the GPS position and GPSGSL altitude, TAWS-A displays a 2-D picture of the surrounding terrain and obstacles relative to the position and altitude of the aircraft. Furthermore, the GPS position and GPS-GSL altitude are used to calculate and “predict” the aircraft’s flight path in relation to the surrounding terrain and obstacles. In this manner, TAWS-A can provide advanced alerts of predicted dangerous terrain and obstacle conditions. 436 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Class A TAWS incorporates radar altimeter input with the GPS-GSL altitude to provide a more accurate position reference when at lower altitudes for certain alert types, and to retain a level of ground proximity warning capability in the unlikely event of an airport, terrain or obstacle database failure. Baro-corrected altitude (or indicated altitude) is derived by adjusting the altimeter setting for local atmospheric conditions. The most accurate baro-corrected altitude can be achieved by frequently updating the altimeter setting to the nearest reporting station along the flight path. However, because actual atmospheric conditions seldom match the standard conditions defined by the International Standard Atmosphere (ISA) model (where pressure, temperature, and lapse rates have fixed values), it is common for the baro-corrected altitude (as read from the altimeter) to differ from the GPS-MSL altitude. This variation results in the aircraft’s true altitude differing from the baro-corrected altitude. TAWS-A provides the following alert types: • Forward Looking Terrain Avoidance (FLTA) Alerting, which consists of: • Required Terrain Clearance (RTC) / Required Obstacle Clearance (ROC) Alerting • Imminent Terrain Impact (ITI) / Imminent Obstacle Impact (IOI) Alerting • Premature Descent Alerting (PDA) • Ground Proximity Warning System (GPWS) Alerting, which consists of: • Excessive Descent Rate (EDR) Alerting • Excessive Closure Rate (ECR) to Terrain Alerting • Flight Into Terrain (FIT) Alerting • Negative Climb Rate (NCR) after takeoff Alerting • Excessive below Glideslope/Glidepath Deviation (GSD) Alerting • Altitude Voice Call Out (VCO) Alerting DISPLAYING TAWS-A DATA TAWS-A uses yellow (caution) and red (warning) colors to depict terrain and obstacles (with heights greater than 200 feet above ground level, AGL) alerts relative to aircraft altitude. Colors are adjusted automatically as the aircraft altitude changes. The colors and symbols in Figure 6-126 and Tables 6-18 and 6-19 are used to represent terrain, obstacles, and potential impact points. Figure 6-126 Terrain Altitude/Color Correlation for TAWS-A 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 437 HAZARD AVOIDANCE Unlighted Obstacle Lighted Obstacle < 1000’ AGL > 1000’ AGL < 1000’ AGL > 1000’ AGL Obstacle Location Red obstacle is above or within 100 ft below the aircraft altitude Yellow obstacle is between 100 ft and 1000 ft below the aircraft altitude Table 6-20 TAWS-B Obstacle Colors and Symbology Potential Impact Point Symbol Alert Type Example Annunciation Warning Caution Table 6-21 TAWS-B Potential Impact Point Symbols with Alert Types TAWS-A information can be displayed on the following maps: • PFD Inset Navigation Map • Trip Planning Page • Navigation Map Page • Flight Plan Pages • TAWS-A Page • System Pages (when terrain is enabled on the Navigation Map Page) TAWS-A relative terrain and obstacle information is also available for display in the optional Profile View Window on the Navigation Map Page. Refer to the Profile View Terrain discussion in this section for more information. Displaying terrain and obstacle information (maps except the TAWS-A Page or PFD Inset Navigation Map): 1) Press the MAP Softkey. 2) Press the TERRAIN Softkey to display terrain and obstacle data. Displaying terrain and obstacle information on the PFD Inset Navigation Map: 1) On the PFD, press the INSET Softkey (in non-TCAS II installations) or the TRFC/MAP Softkey (TCAS II installations). 2) If the PFD Inset Map is showing the traffic map, press the TFRC-2 Softkey to display the navigation map. 3) Press the TERRAIN Softkey to display terrain and obstacle data. The system displays a TAWS-A icon with the terrain legend when terrain and obstacles are enabled on MFD maps. The legend appears without the terrain icon on the dedicated TAWS-A Page. 438 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Figure 6-127 TAWS-A Icon and Legend The Navigation Map Page Setup Menu provides a means in addition to the softkey for enabling/disabling display of terrain and obstacles. The setup menu also controls the map range settings above which terrain and obstacle data are decluttered from the display. If the crew selects a map range larger than the selected map range setting, the data is removed from the map. For terrain data, the enable/disable function applies only to the MFD, while the range setting also affects the PFD Inset Map. Terrain data can be selected for display independently of obstacle data; however, obstacles for which warnings and cautions are issued are shown when terrain is selected for display and the map range is within the setting limit. Maps besides the TAWS-A Page use settings based on those selected for the Navigation Map Page. The maximum display ranges for obstacles on each map are dependent on the range setting made for the Navigation Map. If the maximum range for obstacle display on the Navigation Map is adjusted to below 20 nm, the highest obstacle display range settings on the other applicable maps are also adjusted proportionally. Customizing terrain and obstacle display on the Navigation Map Page: 1) Select the Navigation Map Page. 2) Press the MENU Key. 3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-128). 4) Turn the small FMS Knob to select the ‘Map’ Group and press the ENT Key (Figure 6-129). 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-130). • TERRAIN DATA – Enables/disables display of terrain data and sets maximum range at which terrain is shown • OBSTACLE DATA – Enables/disables display off obstacle data and sets maximum range at which obstacles are shown 6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings). 7) Press the ENT Key to select an option. 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 439 HAZARD AVOIDANCE Figure 6-128 Navigation Map Page Menu Figure 6-129 Navigation Map Page Setup Menu Figure 6-130 Navigation Map Page Setup Menu, Map Group TAWS-A PAGE The Map - TAWS-A Page shows terrain, obstacle, and potential impact point data in relation to the aircraft’s current altitude, without clutter from the basemap. It is the principal map page for viewing TAWS-A information. Aviation data (airports, VORs, and other NAVAIDs) can be displayed for reference. If an obstacle and the projected flight path of the aircraft intersect, the display automatically adjusts the map range as necessary to emphasize the display of potential impact points. Aircraft orientation on this map is always heading up unless there is no valid heading. Two views are available relative to the position of the aircraft: the 360° default display and the radar-like ARC (120°) display. Map range is adjustable with the Joystick from one to 200 nm, as indicated by the map range rings (or arcs). Displaying the TAWS-A Page: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the TAWS-A Page. Changing the TAWS-A Page view: 1) Select the VIEW Softkey. 2) Select the 360 or ARC Softkey to select the desired view. Or: 1) Press the MENU Key. 2) Select ‘View Arc’ or ‘View 360º’ (choice dependent on current state) and press the ENT Key to change the view 440 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Showing/hiding aviation information on the TAWS-A Page: 1) Press the MENU Key. 2) Select ‘Show Aviation Data’ or ‘Hide Aviation Data’ (choice dependent on current state) and press the ENT Key. Red Terrain (Terrain Above or Within 100’ Below the Aircraft Altitude) Aircraft Altitude Above Geodetic Sea Level (GSL) Black Terrain (Terrain More than 1000’ Below the Aircraft Altitude) Red obstacle is above or within 100’ below the aircraft altitude Yellow Terrain (Terrain Between 100’ and 1000’ Below the Aircraft Altitude) Map Range Rings Terrain Legend Annunciation Window Yellow obstacle is between 100’ and 1000’ below the aircraft altitude Figure 6-131 TAWS-A Page (360 View) Red Terrain (Terrain Above or Within 100’ Below the Aircraft Altitude) Aircraft Altitude Above Geodetic Sea Level (GSL) Map Range Arc Black Terrain (Terrain More than 1000’ Below the Aircraft Altitude) Yellow Terrain (Terrain Between 100’ and 1000’ Below the Aircraft Altitude) Terrain Legend Annunciation Window Red obstacle is above or within 100’ below the aircraft altitude Figure 6-32 TAWS-A Page (Arc View) 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 441 HAZARD AVOIDANCE TAWS-A ALERTS Alerts are issued when flight conditions meet parameters that are set within TAWS-A software algorithms. TAWS-A alerts typically employ a CAUTION or a WARNING alert severity level, or both. When an alert is issued, visual annunciations are displayed simultaneously with voice alerts. Table 6-22 shows TAWS-A alert types with corresponding visual annunciations and voice messages. When an alert is issued, annunciations appear on the PFD and MFD. The TAWS-A Alert Annunciation is shown to the upper left of the Altimeter or upper right of the Airspeed indicator on the PFD and below the Terrain Legend on the TAWS-A Page of the MFD. If the TAWS-A Page is not already displayed on the MFD, a pop-up alert appears on the MFD while an alert is active. To acknowledge the pop-up alert: • Press the CLR Key (returns to the currently viewed page), or • Press the ENT Key (accesses the TAWS-A Page) PFD with TAWS-A Annunciations MFD Pop-Up Alert (except TAWS-A Page) MFD TAWS-A Page with Alert Annunciation Figure 6-133 TAWS-A Annunciations 442 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Alert Type PFD/MFD TAWS-A Page Annunciation MFD Map Page Pop-Up Alert (except TAWS-A Page) Voice Alert Reduced Required Terrain Clearance Warning (RTC) “Terrain, Terrain; Pull Up, Pull Up” Imminent Terrain Impact Warning (ITI) “Terrain, Terrain; Pull Up, Pull Up” Reduced Required Obstacle Clearance Warning (ROC) “Obstacle, Obstacle; Pull Up, Pull Up” Imminent Obstacle Impact Warning (IOI) “Obstacle, Obstacle; Pull Up, Pull Up” Excessive Descent Rate Warning (EDR) “ Pull Up” Excessive Closure Rate Warning (ECR) “ Pull Up” Reduced Required Terrain Clearance Caution (RTC) “Caution, Terrain; Caution, Terrain” Imminent Terrain Impact Caution (ITI) “Caution, Terrain; Caution, Terrain” Reduced Required Obstacle Clearance Caution (ROC) “Caution, Obstacle; Caution, Obstacle” Imminent Obstacle Impact Caution (IOI) “Caution, Obstacle; Caution, Obstacle” Premature Descent Alert Caution (PDA) “Too Low, Terrain” Excessive Descent Rate Caution (EDR) “Sink Rate” Excessive Closure Rate Caution (ECR) “Terrain, Terrain” Negative Climb Rate Caution (NCR) “Don’t Sink” * Flight Into Terrain High Speed Caution (FIT) “Too Low, Terrain” Flight Into Terrain Gear Caution (FIT) “Too Low, Gear” Flight Into Terrain Flaps Caution (FIT) “Too Low, Flaps” Flight Into Terrain Takeoff Caution (FIT) “Too Low, Terrain” Glide Slope/Glide Path Deviation Caution (GSD) or or “Glide Slope” or “Glide Path” None None “Five-Hundred”, “Four-Hundred”, “Three-Hundred”, “Two-Hundred”, “One-Hundred” (depends on approach type) Altitude Voice Callout (VCO) Table 6-22 TAWS-A Alerts 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 443 HAZARD AVOIDANCE FORWARD LOOKING TERRAIN AVOIDANCE The Forward Looking Terrain Avoidance feature of TAWS-A compares the aircraft’s projected flight path with known terrain and obstacles in their respective databases and issues four types of alerts as either a caution or a warning: Reduced Required Terrain Clearance (RTC) and Reduced Required Obstacle Clearance (ROC) alerts are issued when the aircraft flight path is above terrain, yet is projected to come within the minimum clearance values in Figure 6-134. When an RTC alert is issued, a potential impact point is displayed on the TAWS-A Page. Imminent Terrain Impact (ITI) and Imminent Obstacle Impact (IOI) alerts are issued when the aircraft is below the elevation of a terrain or obstacle cell in the aircraft’s projected path. ITI and IOI alerts are accompanied by a potential impact point displayed on the TAWS-A Page. The alert is annunciated when the projected vertical flight path is calculated to come within minimum clearance altitudes in Figure 6-134. Required Terrain Clearance RTC Level (FT) RTC Descending (FT) 800 Required Terrain Clearance (FT) Required Terrain Clearance (FT) 700 600 500 400 300 200 100 0 0 5 10 15 20 25 30 Distance From Runway (NM) Distance From Runway (NM) Figure 6-134 FLTA Alert Minimum Terrain and Obstacle Clearance Values FLTA alerts are automatically disabled when the aircraft is less than 200 feet above the destination runway elevation while within 0.5 nm of the approach runway, or the aircraft is between runway ends. 444 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE PREMATURE DESCENT ALERTING A Premature Descent Alert (PDA) is issued when the system detects that the aircraft is significantly below the normal approach path to a runway (Figure 6-135). PDA alerting begins when the aircraft is below 700 feet AGL within 15 nm of the destination airport and ends when the aircraft is 0.5 nm from the runway threshold. 800 Height Above Destination (Feet) 700 600 500 400 300 PDA ALERTING AREA 200 100 15 14 13 12 11 10 9 8 7 6 5 4 3 2 1 0 0 Distance to Destination (NM) Figure 6-135 PDA Alerting Threshold Inhibiting FLTA and PDA Alerts NOTE: The ‘Inhibit TAWS’ function only inhibits FLTA and PDA alerts. Alerting for GPWS alerts (EDR, ECR, NCR, FIT) and GSD is controlled independently from FLTA and PDA alerts. FLTA and PDA voice alerts and visual annunciations can be manually inhibited. Discretion should be used when inhibiting alerts and the system should be enabled when appropriate. When PDA and FLTA alerts are inhibited, the alert annunciation ‘TAWS INH’ is shown on the PFD and on the TAWS-A Page annunciation window of the MFD (Figure 6-136). Figure 6-136 TAWS-A Page Menu and Inhibit Annunciation 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 445 HAZARD AVOIDANCE Inhibiting/enabling FLTA and PDA alerting: 1) Select the TAWS-A Page. 2) Select the TAWS INH Softkey to inhibit or enable TAWS-A (choice dependent on current state). Or: 1) Press the MENU Key. (Figure 6-136) 2) Select ‘Inhibit TAWS’ or ‘Enable TAWS’ (choice dependent on current state) and press the ENT Key. If PDA and FLTA alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS approach, a ‘LOW ALT’ annunciation may appear on the PFD next to the Altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix. See the Flight Instruments Section for details. EXCESSIVE DESCENT RATE ALERT The purpose of the Excessive Descent Rate (EDR) alert is to provide suitable notification when the aircraft is determined to be closing (descending) upon terrain at an excessive speed. Figure 6-137 shows the parameters for the alert as defined by TSO-C151b. 6000 5500 5000 Height Above Terrain (Feet) 4500 4000 NK : “SI ion Caut 3500 ” RATE 3000 2500 2000 Warning: “PULL UP” 1500 1000 12000 11000 10000 9000 8000 7000 6000 5000 4000 3000 2000 1000 0 0 500 Descent Rate (Feet Per Minute)) Figure 6-137 Excessive Descent Rate Alert Criteria EXCESSIVE CLOSURE RATE ALERT The Excessive Closure Rate (ECR) alert provides suitable notification when the aircraft is determined to be closing upon terrain at an excessive speed for a given aircraft gear and flap configuration. Figures 6-125 and 6-126 show the ECR alerting criteria for flaps in the landing configuration and for all other flight phases respectively. 446 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Height Above Terrain (Feet) ECR alerts are automatically inhibited when the aircraft is 5 nm from the nearest airport, except when FLTA is not available (causing the TAWS N/A or TAWS FAIL annunciation), in which case ECR alerting will remain active until landing. Closure Rate (FPM) Height Above Terrain (Feet) Figure 6-138 Excessive Closure Rate Alert Criteria (Flaps Up or Takeoff Configuration) Closure Rate (FPM) Figure 6-139 Excessive Closure Rate Alert Criteria (Flaps in Landing Configuration) FLIGHT INTO TERRAIN ALERT Flight Into Terrain (FIT) caution alerts occur when the aircraft is too low with respect to terrain and the gear or flaps are not configured for landing. The aircraft may also be above or below the recommended approach speed. FIT alerts are issued when flight conditions meet the criteria shown in Figure 6-140. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 447 Height Above Terrain (Feet) HAZARD AVOIDANCE * * Altitude Rate (FPM) * Flap position will not trigger alert if Flap Override option is enabled; see discussion below. Figure 6-140 Flight Into Terrain Alert Criteria (Aircraft Configuration) To reduce nuisance FIT alerts on approaches where flap extension is not desired (or is intentionally delayed), the pilot may override FIT alerting based on the flap position, while all other FIT alerting remains in effect. Figure 6-141 TAWS-A Page Menu and FIT Flap Override Annunciation Overriding Flaps-based FIT alerting: 1) Select the TAWS-A Page 2) Select the FLAP OVR Softkey Or: 1) Press the MENU Key. (Figure 6-141) 2) Select ‘Flap Override’ or ‘Disable Flap Override’ (choice dependent on current state) and press the ENT Key. 448 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE When the Flaps Override option is enabled, the annunciation ‘FLAP OVR’ is annunciated on the PFD and on the TAWS-A Page of the MFD (Figure 6-141). If GPWS alerts are also inhibited (which include FIT), the ‘FLAP OVR’ annunciation is not shown. Height Above Terrain (Feet) FIT alerts also occur during takeoff or go-around if the aircraft’s height above ground level (as determined by the radar altimeter) is too close to rising terrain. TAWS-A issues issue the voice alert “Too Low - Terrain” and visual annunciations when conditions enter the caution alert area (Figure 6-142). “TOO LOW, TERRAIN” Radio Altitude Loss (Feet) Figure 6-142 FIT Alerting After Takeoff NEGATIVE CLIMB RATE AFTER TAKEOFF ALERT The Negative Climb Rate (NCR) After Takeoff alert (also referred to as “Altitude Loss After Takeoff”) provides alerts when the system determines the aircraft is losing altitude (closing upon terrain) after takeoff. The voice alert “Don’t Sink” is given for NCR alerts, accompanied by a visual annunciation and a pop-up terrain alert on the MFD if the TAWS-A Page is not already displayed. NCR alerting for TAWS-A is only active when departing from an airport and when the following conditions are met: • Height above the terrain is less than 700 feet • Distance from the departure airport is 5 nm or less • Heading change from the departure heading is less than 110 degrees • Landing gear or flaps are configured for takeoff Figures 6-130 and 6-131 show the NCR alerting parameters based on altitude loss and sink rate, respectively, as defined by TSO-C151b 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 449 HAZARD AVOIDANCE 1000 Height Above Terrain (Feet) 900 800 700 600 500 “DON’T SINK” 400 300 200 100 0 0 20 40 60 80 100 120 140 Altitude Loss (Feet) Figure 6-143 Negative Climb Rate (NCR) Altitude Loss 1000 Height Above Terrain (Feet) 900 800 700 600 500 “DON’T SINK” 400 300 200 100 0 0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000 5500 6000 6500 7000 Sink Rate (FPM) Figure 6-144 Negative Climb Rate (NCR) Sink Rate 450 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Inhibiting GPWS Alerts (EDR, ECR, FIT, and NCR) NOTE: The ‘Inhibit GPWS’ function only affects GPWS alerts (EDR, ECR, NCR, and FIT). Alerting for FLTA, PDA, and GSD is controlled independently from the GPWS alerts listed below. EDR, ECR, FIT, and NCR alerts can be manually inhibited as a group. Discretion should be used when inhibiting alerts and the GPWS system should be enabled when appropriate. When these alerts are inhibited, the status annunciation ‘GPWS INH’ is shown on the PFD and on the TAWS-A Page annunciation window of the MFD (Figure 6-145). Figure 6-145 TAWS-A Page Menu and GPWS Inhibit Annunciation Inhibiting/enabling GPWS alerting: 1) Select the TAWS-A Page. 2) Select the GPWS INH Softkey to inhibit or enable GPWS alerts (choice dependent on current state). Or: a) Press the MENU Key. (Figure 6-145) b) Select ‘Inhibit GPWS’ or ‘Enable GPWS’ (choice dependent on current state) and press the ENT Key. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 451 HAZARD AVOIDANCE EXCESSIVE BELOW GLIDESLOPE/GLIDEPATH DEVIATION ALERT Radio Altitude (Feet) A Glideslope Deviation or Glidepath Deviation (GSD) caution alert is issued when the system detects that the aircraft is significantly below the glidepath for the selected approach in relation to the aircraft’s height above terrain (Figure 6-146). “GLIDESLOPE” or “GLIDEPATH” Number of Dots Below Glideslope/Glidepath Figure 6-146 Excessive Below Glideslope/Glidepath Deviation Alert Criteria GSD alerting is available as the aircraft approaches a runway and the following conditions are met: • An ILS, LPV, or LNAV/VNAV approach is active and vertical navigation indications are being displayed. • Aircraft altitude is below 1000 feet AGL. • Aircraft distance is within 5 nm of the runway, but greater than 1000 feet from the runway (if GPS position is available). • Gear is configured for landing. When a GSD caution alert occurs on an ILS approach, the visual annunciation and voice alert ‘GLIDESLOPE’ is issued. If a GSD caution alert occurs on an LPV or LNAV/VNAV approach, the visual annunciation and voice alert ‘GLIDEPATH’ is issued (Figure 6-147). Inhibiting GSD Alerts NOTE: GSD alerting may only be inhibited while a GSD alert is occurring. GSD alerts are inhibited independently from all other FLTA, PDA, and GPWS alerts. During a GSD alert, the PFD Softkeys are displayed as shown in Figure 6-147 to provide an option to inhibit the alert. A ‘GLIDESLOPE’ alert provides a GS INH Softkey to inhibit the alert. A ‘GLIDEPATH’ alert provides a GP INH Softkey to inhibit the alert. When an inhibit softkey is pressed, the PFD softkeys return to the top-level display. Press the BACK Softkey to return to the top level of the PFD softkeys without inhibiting the GSD alert. 452 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Or: Or: Figure 6-147 GSD Alert and PFD Softkeys GSD alerts may also be inhibited on the TAWS-A Page while a GSD alert is occurring. Inhibiting/Enabling GSD alerting (only available during a GSD alert): 1) Select the TAWS-A Page. 2) Select the GS INH or GP INH Softkey to inhibit or enable GSD alerts (softkey choice dependent on present GSD alert type). Or: 1) Press the MENU Key. (Figure 6-148) 2) Select the option to inhibit or enable the glideslope or glidepath alerting (choice dependent on present GSD alert type) and press the ENT Key. Figure 6-148 TAWS-A Page Menu and Glideslope Alerting Inhibited Annunciation 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 453 HAZARD AVOIDANCE The annunciation ‘GS INH’ or ‘GP INH’ is displayed on the PFD and TAWS-A Page when GSD Alerting is inhibited. Discretion should be used when inhibiting GSD alerts. Inhibiting GSD alerts has no effect on the vertical guidance provided by the flight instruments. ALTITUDE VOICE CALLOUT (VCO) TAWS-A provides altitude advisory voice alerts as the aircraft descends. VCO alerts are based on the height above terrain when the aircraft is more than 5 nm from an airport, or the height above the nearest runway threshold elevation if within 5 nm of an airport. VCO alerts begin at 500 feet with the voice alert “Five Hundred”. Maintenance personnel may configure additional VCO alerts to occur at 400, 300, 200 and 100 feet during descent. There are no display annunciations or pop-up alerts that accompany the VCO alert(s). SYSTEM STATUS During power-up, TAWS-A conducts a self-test of its visual annunciations and voice alerts. The system test can also be manually initiated. The system issues a voice alert when the test has concluded. TAWS-A System Testing is disabled when ground speed exceeds 30 knots. TAWS-A terrain alerts will not be issued while a test is in progress. PFD/MFD TAWS-A Page Status Annunciation Additional TAWS-A Page Annunciation Voice Alert TAWS System Fail TAWS FAIL “TAWS System Failure” GPWS System Fail None “GPWS System Failure” System Test in progress TAWS TEST None None “TAWS System Test OK” Alert Type System Test pass None Table 6-23 TAWS-A System Test Status Annunciations Manually testing the TAWS-A System: 1) Select the TAWS-A Page. 2) Press the MENU Key. 3) Select ‘Test TAWS System’ and press the ENT Key to confirm the selection (Figure 6-149). 454 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Figure 6-149 TAWS-A Page Menu TAWS-A ABNORMAL OPERATIONS TAWS-A continually monitors several system-critical items such as database validity, flap and landing gear position, radar altimeter input, and GPS status. If no GDU contains Terrain, Airport Terrain, and Obstacle databases (or the databases are invalid), the voice alert “TAWS System Failure” is generated along with the ‘TAWS FAIL’ alert annunciation. TAWS-A requires a 3-D GPS navigation solution along with specific vertical accuracy minimums. Should the navigation solution become degraded or if the aircraft is out of the database coverage area, the annunciation ‘TAWS N/A’ is generated in the annunciation window and on the TAWS-A Page. The voice alert “TAWS Not Available” is also generated if airborne, and some TAWS-A terrain alerts will not be issued (Table 6-24), while GPWS alerting (which are not dependent on GPS position) will continue to operate. When the GPS signal is restored and the aircraft is within the database coverage area, the voice alert “TAWS Available” is generated. TAWS-A also requires radar altimeter input. Should the radar altimeter input fail or become degraded, the annunciation ‘GPWS FAIL’ is generated in the annunciation window and on the TAWS-A Page. The voice alert “GPWS System Failure” is also generated. The ‘GPWS FAIL’ annunciation will also occur if both GPS altitude and barometric altitude are unavailable. If only the GPWS system has failed, GPWS-based alerts will not be available (Table 6-24), while other TAWS-A alerting remains unaffected. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 455 HAZARD AVOIDANCE PFD/MFD TAWS-A Page Annunciation Alert Type TAWS System Test Fail; Terrain, Airport Terrain or Obstacle database unavailable or invalid on all GDUs; software mismatch among GDUs; TAWS audio fault MFD Terrain or Obstacle database unavailable or invalid. TAWS operating with PFD Terrain or Obstacle databases No GPS position † None Excessively degraded GPS signal, or out of database coverage area Sufficient GPS signal reception restored Radar Altimeter invalid, Vertical Speed Invalid, GPS and Baro Altitude invalid, Software mismatch among GDUs, TAWS configuration mismatch among GDUs, TAWS audio fault TAWS-A Page Center Banner Annunciation Voice Alert TAWS Alert Types Not Available TAWS FAIL “TAWS System Failure” FLTA, PDA TERRAIN DATABASE FAILURE None NO GPS POSITION “TAWS Not Available” None None None † None “TAWS Not Available” “TAWS Available” (voice alert only in flight) “GPWS System Failure” FLTA, PDA, GSD* VCO † FLTA, PDA EDR, ECR, NCR, FIT, GSD * GSD alert will be available if a valid ILS is being used for navigation, even if no valid GPS signal is being received. † VCO alerts are not issued if both TAWS and GPWS systems have failed or are not available. Table 6-24 TAWS-A Abnormal Status Alerts If the aircraft bank angle exceeds 30˚, TAWS-A will disable ECR alerts. ECR alert availability returns when the bank angle is reduced for at least eight seconds. On an ILS, LPV, or LNAV/VNAV approach, GSD alerting will not be available if the glidepath exceeds ten degrees. 456 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE 6.8 PROFILE VIEW TERRAIN The system offers an optional Profile View of terrain and obstacles relative to the aircraft’s current flight path and altitude on the Navigation Map Page of the MFD. This Profile View does not provide terrain or obstacle caution or warning annunciations or voice alerts systems, nor does it display potential impact points inside the Profile View. The system uses the same colors as the respective TAWS System (TAWS-A or TAWS-B) colors and symbols to represent terrain and obstacles within the Profile View. Refer to the TAWS discussions for more information about terrain and obstacle color correlation and symbology for more information. Enabling/Disabling Profile View: 1) Select the Navigation Map Page. 2) Press the MAP Softkey. 3) Press the PROFILE Softkey to enable or disable Profile View. Or: 1) Press the MENU Key. 2) Select ‘Show Profile View’ or ‘Hide Profile View’ (choice dependent on current state) and press the ENT Key. Enabling/Disabling Profile View Terrain on the Navigation Map (when Profile View is enabled): 1) Select the Navigation Map Page. 2) Press the MAP Softkey. 3) Press the TERRAIN Softkey. PROFILE VIEW DISPLAY When the Profile View is enabled, it is displayed in a window below the Navigation Map. Altitude is shown along a vertical scale, with an aircraft icon positioned at the current altitude. Distance is represented horizontally along the bottom of the Profile View, and increases from left (present position) to right. When the Navigation Map range is adjusted with the Joystick, the horizontal distance of the Profile View is adjusted proportionately to be 1/2 of the Navigation Map range distance down to one nautical mile, at which point Profile View is no longer available (‘PROFILE NOT AVAILABLE’ is displayed). When terrain and obstacles are shown on the Navigation Map Page, this information also appears in the Profile View Window. If the Navigation Map range is adjusted beyond the maximum map range for terrain and obstacle data appear on the Navigation Map, this information is also removed from the Profile View Window. Refer to the TAWS discussions for information selecting the maximum map range to display terrain and obstacles on navigation maps. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 457 HAZARD AVOIDANCE Profile Path Range Markers Terrain Legend Navigation Map Range Altitude Scale Profile View Length is One Half of the Navigation Map Range Distance Scale Figure 6-150 Profile View on Navigation Map with Terrain Display Enabled Obstacles with heights greater than 200 feet AGL appear relative to aircraft altitude along the altitude scale. The top of the obstacle symbol on the scale represents the obstacle’s height AGL. If the obstacle’s height AGL is higher than can be represented by the obstacle symbol itself (e.g. for unusually tall obstacles), a vertical line appears below the obstacle symbol in order to depict the top of the obstacle symbol at its height AGL, as shown in Figure 6-151. Figure 6-151 Profile View with Tall Obstacles PROFILE PATH The contents of the Profile View Window are based on the current aircraft track (or heading if track is unavailable), and the system shows the highest known terrain or obstacles within a predetermined width from the present position to the end of the profile range inside the Profile View Window. This width is determined by 458 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE the phase of flight, as annunciated on the HSI, and is widest during enroute and oceanic phases, and narrowest during approach and departure phases (Table 6-25). Flight Phase Approach Departure Terminal Enroute Oceanic Total Profile View Width 0.6 nm 0.6 nm 2.0 nm 4.0 nm 4.0 nm Table 6-25 Profile View Width Scale The Profile Path display is a visual cue which represents the horizontal and lateral boundaries of the Profile View on the Navigation Map Page. This path is depicted as a white rectangle and is only available when Profile View is enabled. White range markers both edges of the Profile Path match the range markers along the distance scale inside the Profile View Window. The Profile View distance must be at least four nautical miles (or 7.5 km if configured for metric units) in order for the path display to appear on the Navigation Map Page. The pilot can enable or disable the Profile Path display on the Navigation Map. The pilot can also select the maximum navigation map range to show the Profile Path. If a map range is selected beyond the selected maximum range, the system removes the Profile Path display. Customizing the Profile Path display on the Navigation Map Page: 1) Select the Navigation Map Page. 2) Press the MENU Key. 3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-152). 4) Turn the small FMS Knob to select the ‘Profile’ Group and press the ENT Key (Figure 6-153). 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-154). • PROFILE PATH – Turns the display of the Profile Path on or off and sets maximum range at which Profile Path is shown 6) Turn the small FMS Knob to scroll through options (ON/OFF, range settings). 7) Press the ENT Key to select an option. 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 459 HAZARD AVOIDANCE Figure 6-152 Navigation Map Page Menu Figure 6-153 Navigation Map Page Setup Menu 460 Figure 6-154 Navigation Map Page Setup Menu, Profile Group Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE 6.7 TRAFFIC INFORMATION SERVICE (TIS) WARNING: Do not rely solely upon the display of traffic information to accurately depict all of the traffic information within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information from other aircraft, traffic may be present but not represented on the displays. WARNING: Do not rely solely upon the display of traffic information for collision avoidance maneuvering. The traffic display does not provide collision avoidance resolution advisories and does not under any circumstances or conditions relieve the pilot’s responsibility to see and avoid other aircraft. NOTE: TIS is available only when the aircraft is within the service volume of a TIS-capable terminal radar site. Aircraft without an operating transponder are invisible to Traffic Advisory Systems (TAS), Traffic Alert and Collision Avoidance Systems (TCAS), and to TIS. Aircraft without altitude reporting capability are shown without altitude separation data or climb descent indication. NOTE: TIS is disabled if another traffic system is installed. Traffic Information Service (TIS) assists the flight crew in detection and avoidance of other aircraft. TIS uses the Mode S transponder for the traffic data link. TIS receives traffic information from ground stations, and provides updates every five seconds. The system displays up to eight traffic targets within a 7.5-nm radius, from 3000 feet below to 3500 feet above the requesting aircraft. The system displays traffic with the following symbology: TIS Symbol Description Non-Threat Traffic Traffic Advisory (TA) Traffic Advisory Off Scale Table 6-26 TIS Traffic Symbols A Traffic Advisory (TA) indicates that the current track of the intruder could result in a collision. When traffic meets the advisory criteria for the TA, a solid yellow circle symbol appears. A TA which is detected, but is outside the range of the map, causes a banner message to appear in the lower left corner of the map and a half TA symbol to appear at the relative bearing of the intruder. TIS also provides a vector line showing the direction in which the traffic is moving, to the nearest 45°. Traffic information for which TIS is unable to determine the bearing (non-bearing traffic) is displayed in the center of the Traffic Map Page (Figure 6-159) or in a banner at the lower left corner of maps other than the Traffic Map Page on which traffic can be displayed. The altitude difference between the requesting aircraft and other intruder aircraft is displayed above/below the traffic symbol in hundreds of feet. If the other aircraft is above the requesting aircraft, the altitude separation appears above the traffic symbol; if below, the altitude separation appears below. Altitude trend is displayed as 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 461 HAZARD AVOIDANCE an up/down arrow (for vertical speeds at least 500 feet per minute in either direction) to the right of the target symbol. Traffic symbols for aircraft without altitude reporting capability appear without altitude separation or climb/descent information. DISPLAYING TRAFFIC DATA Traffic information can be displayed on the following maps (when TIS is operating): • PFD Inset Map • Trip Planning Page • Navigation Map Page • Nearest Pages • Traffic Map Page • Active Flight Plan Page Traffic information can also be displayed on the PFD when the Synthetic Vision Technology (SVT) option is installed and enabled. See the Additional Features Section for details. Displaying traffic information (maps other than the Traffic Map Page): 1) Select the MAP Softkey. 2) Select the TRAFFIC Softkey to display traffic data. When traffic is selected on maps other than the Traffic Map Page, an the system displays a status icon to indicate the feature is enabled for display. Non-Threat Traffic, 2500’ Above, Descending Traffic Advisory, 500’ Below, Climbing Non-Threat Traffic, Altitude Not Reported Traffic Display Enabled Icon TIS Banner Annunciations Figure 6-155 TIS Traffic on the Navigation Map Page 462 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Displaying traffic information (PFD Inset Map): 1) Press the INSET Softkey. 2) Press the TRAFFIC Softkey to display traffic data on the inset map (TRFC-1). 3) Press the softkey again to display the traffic-only inset (TRFC-2). 4) Press the softkey again to remove traffic data. The Navigation Map Page Setup Menu provides a means in addition to the softkey for enabling/disabling display of traffic. The setup menu also controls the map range settings above which traffic data (symbols and labels) are decluttered from the display. If a map range larger than the map range setting is selected, the data is removed from the map. Maps besides the Traffic Map Page use settings based on those selected for the Navigation Map Page. Customizing traffic display on the Navigation Map Page: 1) Select the Navigation Map Page. 2) Press the MENU Key. 3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-156). 4) Turn the small FMS Knob to select the ‘Traffic’ Group and press the ENT Key (Figure 6-157). 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-158). • TRAFFIC – Turns the display of traffic data on or off • TRAFFIC MODE – Selects the traffic mode for display; select from: - All Traffic - Displays all traffic - TA ONLY - Displays Traffic Advisories only • TRAFFIC SMBL – Selects the maximum range at which traffic symbols are shown • TRAFFIC LBL – Selects the maximum range at which traffic labels are shown (with the option to turn off) 6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings, etc.). 7) Press the ENT Key to select an option. 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 463 HAZARD AVOIDANCE Figure 6-156 Navigation Map Page Menu Figure 6-157 Navigation Map Page Setup Menu Figure 6-518 Navigation Map Page Setup Menu, Traffic Group TRAFFIC MAP PAGE The Traffic Map Page is specialized to show surrounding TIS traffic data in relation to the aircraft’s current position and altitude, without clutter from the basemap. It is the principal map page for viewing TIS traffic information. Aircraft orientation on this map is always heading up unless there is no valid heading. Map range is adjustable with the Joystick from two to 12 nm, as indicated by the map range rings. The traffic mode is annunciated in the upper left corner of the Traffic Map Page. When the aircraft is on the ground, TIS automatically enters Standby Mode. Once the aircraft is airborne, TIS switches from Standby to Operating Mode and the system begins to display traffic information. Refer to the System Status discussion for more information. Displaying traffic on the Traffic Map Page: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. 3) Confirm TIS is in Operating Mode: Select the OPERATE Softkey to begin displaying traffic. Or: a) Press the MENU Key. b) Select ‘Operate Mode’ (shown if TIS is in Standby Mode) and press the ENT Key. 464 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Traffic Mode Annunciation Non-Threat Traffic, 2500’ Above, Descending “TIS Not Available” Voice Alert Status Traffic Advisory 500’ Below, Climbing “Non-Bearing” Traffic (System Unable to Determine Bearing) Distance is 4.0 nm, 500’ Above, Descending Traffic Advisory OffScale, 400’ Below, Level Non-Threat Traffic, Altitude Not Reported Traffic Status Banners Figure 6-159 Traffic Map Page Select to Mute “TIS Not Available” Voice Alert TIS ALERTS When the number of TAs on the Traffic Map Page increases from one scan to the next, the following occur: • A single “Traffic” voice alert is generated. • A ‘TRAFFIC’ Annunciation appears to the top left of the Attitude Indicator on the PFD, flashing for 5 seconds and remaining displayed until no TAs are detected in the area. • The PFD Inset Map is automatically displayed with traffic. To reduce the number of nuisance alerts due to proximate aircraft, the “Traffic” voice alert is generated only when the number of TAs increases. For example, when the first TA is displayed, a voice and visual annunciation are generated. As long as a single TA remains on the display, no additional voice alerts are generated. If a second TA appears on the display or if the number of TAs initially decreases and then subsequently increases, another voice alert is generated. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 465 HAZARD AVOIDANCE Inset Map Displays When TA is Detected Figure 6-160 Traffic Annunciation (PFD) A “TIS Not Available” (TNA) voice alert occurs when the TIS service becomes unavailable or is out of range. TIS may be unavailable in the radar coverage area due to the following: • Radar site TIS Mode S sensor is not operational or is out of service • Traffic or requesting aircraft is beyond the maximum range of the TIS-capable Mode S radar site. • Traffic or requesting aircraft is above the radar site in the cone of silence and out of range of an adjacent site. • Traffic or requesting aircraft is below radar coverage. In flat terrain, the coverage extends from about 3000 feet upward at 55 miles. Terrain and obstacles around the radar site can further decrease radar coverage in all directions. • Traffic does not have an operating transponder. The “TIS Not Available” (TNA) voice alert can be manually muted to reduce nuisance alerting. TNA muting status is shown in the upper left corner of the Traffic Map Page. Muting the “TIS Not Available” voice alert: 1) Select the Traffic Map Page. 2) Select the TNA MUTE Softkey. The status is displayed in the upper left corner of the Traffic Map Page. Or: a) Press the MENU Key. b) Select ‘‘’Not Available” Mute On’ (shown if TNA muting is currently off) and press the ENT Key. 466 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE SYSTEM STATUS The system performs an automatic test of TIS during power-up. If TIS passes the test, TIS enters Standby Mode (on the ground) or Operating Mode (in the air). If TIS fails the power up test, the system displays an annunciation in the center of the Traffic Map Page. Traffic Map Page Center Banner Annunciation NO DATA DATA FAILED FAILED Description Data is not being received from the transponder* Data is being received from the transponder, but a failure is detected in the data stream* The transponder has failed* UNAVAILABLE TIS is unavailable or out of range * Contact a service center or Garmin dealer for corrective action Table 6-27 TIS Failure Annunciations System Test has Failed Data Not Received from Transponder Figure 6-161 TIS Power-up Test Failure The traffic mode is annunciated in the upper left corner of the Traffic Map Page. When the aircraft is on the ground, TIS automatically enters Standby Mode. If traffic is selected for display on another map while Standby Mode is selected, the traffic display enabled icon is crossed out (also the case whenever TIS has failed). Once the aircraft is airborne, TIS switches to Operating Mode and traffic information is displayed. The mode can be changed manually using softkeys or the page menu. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 467 HAZARD AVOIDANCE Mode Traffic Mode Annunciation (Traffic Map Page) TIS Operating OPERATING Traffic Display Status Icon (Other Maps) STANDBY (also shown in white in center of page) TIS Standby FAIL TIS Failed Table 6-28 TIS Modes Switching between TIS modes: 1) Select the Traffic Map Page. 2) Select the STANDBY or OPERATE Softkey to switch between modes. The mode is displayed in the upper left corner of the Traffic Map Page. Or: a) Press the MENU Key. b) Select ‘Operate Mode’ or ‘Standby Mode’ (choice dependent on current state) and press the ENT Key. The annunciations to indicate the status of traffic information appear in a banner at the lower left corner of maps on which traffic can be displayed (Table 6-26). Traffic Status Banner Annunciation TA OFF SCALE TA X.X ± XX ↕ AGE MM:SS TRFC COAST TRFC RMVD TRFC FAIL NO TRFC DATA TRFC UNAVAIL Description A Traffic Advisory is outside the selected display range* Annunciation is removed when traffic comes within the selected display range System cannot determine bearing of Traffic Advisory** Annunciation indicates distance in nm, altitude separation in hundreds of feet, and altitude trend arrow (climbing/descending) Appears if traffic data is not refreshed within 6 seconds If after another 6 seconds data is not received, traffic is removed from the display The quality of displayed traffic information is reduced as the age increases The displayed data is not current (6 to 12 seconds since last message) The quality of displayed traffic information is reduced when this message is displayed Traffic is removed because it is too old for coasting (12 to 60 seconds since last message) Traffic may exist within the selected display range, but it is not displayed Traffic data has failed Traffic has not been detected The traffic service is unavailable or out of range *Shown as symbol on Traffic Map Page **Shown in center of Traffic Map Page Table 6-29 TIS Traffic Status Annunciations 468 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE 6.8 GARMIN TCAS I TRAFFIC WARNING: Do not rely solely upon the display of traffic information to accurately depict all of the traffic within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information from aircraft or ground stations, traffic may be present that is not represented on the display. WARNING: Do not rely solely upon the display of traffic information for collision avoidance maneuvering. The traffic display does not provide collision avoidance resolution advisories and does not under any circumstances or conditions relieve the pilot’s responsibility to see and avoid other aircraft. NOTE: Pilots should be aware of TAS system limitations. TAS systems require transponders of other aircraft to respond to system interrogations. If the transponders do not respond to interrogations due phenomena such as antenna shading or marginal transponder performance, traffic may be displayed intermittently, or not at all. Aircraft without altitude reporting capability are shown without altitude separation data or climb descent indication. Pilots should remain vigilant for traffic at all times. NOTE: TIS is disabled when TCAS I is installed. The optional Garmin GTS 850 is a TSO-certified Traffic Alert and Collision Avoidance System (TCAS I). The GTS 850 enhances flight crew situational awareness by displaying traffic information for transponder-equipped aircraft. The GTS 850 also provides visual annunciations and voice traffic alerts to assist the crew in visually acquiring traffic. The GTS 850 is capable of tracking up to 45 intruding aircraft equipped with Mode A or C transponders, and up to 30 intruders equipped with Mode S transponders. A maximum of 30 aircraft with the highest threat potential can be displayed simultaneously. No TCAS I surveillance is provided for aircraft without operating transponders. THEORY OF OPERATION When the GTS 850 is in Operating Mode, the unit interrogates the transponders of aircraft in its vicinity while monitoring transponder replies. The GTS 850 uses this information to determine the distance, relative bearing, and if reported, the altitude vertical trend, and other information for each aircraft within its surveillance range. The GTS 850 then calculates a closure rate to each intruder based on the projected Closest Point of Approach (CPA). If the closure rate meets the threat criteria for a Traffic Advisory (TA), visual and aural alerting is provided. TCAS I SURVEILLANCE VOLUME The GTS 850 surveillance system monitors the airspace within ±10,000 feet of own altitude. Under ideal conditions, the unit scans transponder traffic up to 40 nm in the forward direction. Range is somewhat reduced to the sides and aft of own aircraft due to the directional interrogation signal patterns. In areas of greater transponder traffic density or when TCAS II systems are detected, the GTS 850 automatically reduces its interrogation transmitter power (and therefore range) in order to limit potential interference from other signals. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 469 HAZARD AVOIDANCE TRAFFIC SYMBOLOGY The GTS 850 uses the symbology shown in Table 6-20 to depict intruding traffic. TAS Symbol Description Non-Threat Traffic Proximity Advisory (PA) Traffic Advisory (TA) Traffic Advisory Off Scale Table 6-30 Traffic Symbol Description A Traffic Advisory (TA), displayed as a yellow circle, alerts the crew to a potentially hazardous intruding aircraft, if the closing rate, distance, and vertical separation meet TA criteria. A Traffic Advisory that is beyond the selected display range (off scale) is indicated by a half TA symbol at the edge of the screen at the relative bearing of the intruder. A Proximity Advisory (PA), displayed as a solid white diamond, indicates the intruding aircraft is within ±1200 feet and is within a 6 nm range, but is still not considered a TA threat. A Non-threat Advisory, shown as an open white diamond, is displayed for traffic beyond 6 nm that is neither a TA or PA. Relative altitude, when available, is displayed above or below the corresponding intruder symbol in hundreds of feet (Figure 6-162). When this altitude is above own aircraft, it is preceded by a ‘+’ symbol; a minus sign ‘-’ indicates traffic is below own aircraft. A vertical trend arrow to the right of the intruder symbol (Figure 6-162) indicates traffic climbing or descending at least five hundred feet per minute with an upward or downward-pointing arrow respectively. Relative Altitude Vertical trend arrow Figure 6-162 Intruder Altitude and Vertical Trend Arrow Flight IDs may also be displayed with traffic symbols; see the Flight IDs discussion in this section for more information. The GTS 850 automatically suppresses the display of on-ground traffic equipped with Mode S transponders. 470 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE TA ALERTING CONDITIONS The GTS 850 automatically adjusts its TA sensitivity level to reduce the likelihood of nuisance TA alerting during flight phases likely to be near airports. Level A (less) TA sensitivity is used when the aircraft’s groundspeed is less than 120 knots. In all other conditions, Level B (greater) TA sensitivity is used to assess TA threats. Sensitivity Intruder Altitude Level Available A Yes A No B Yes B No TA Alerting Conditions Intruder closing rate provides less than 20 seconds of vertical and horizontal separation. Or: Intruder closing rate provides less than 20 seconds of horizontal separation and vertical separation is within 600 feet. Or: Intruder range is within 0.2 nm and vertical separation is within 600 feet. Intruder closing rate provides less than 15 seconds of separation. Intruder closing rate provides less than 30 seconds of vertical and horizontal separation. Or: Intruder closing rate provides less than 30 seconds of horizontal separation and vertical separation is within 800 feet. Or: Intruder range is within 0.55 nm and vertical separation is within 800 feet. Intruder closing rate provides less than 20 seconds of separation.. Table 6-31 TA Sensitivity Level and TA Alerting Criteria 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 471 HAZARD AVOIDANCE TCAS I ALERTS When the GTS 850 detects a new TA, the following occur: • A single “Traffic!” voice alert is generated, followed by additional voice information about the bearing, relative altitude, and approximate distance from the intruder that triggered the TA (Table 6-32). The announcement “Traffic! 12 o’clock, high, four miles,” indicates the traffic is in front of own aircraft, above own altitude, and approximately four nautical miles away. • A ‘TRAFFIC’ Annunciation appears at the top right of the airspeed on the PFD, flashes for five seconds, and remains displayed until no TAs are detected in the area (Figure 6-163). • The PFD Inset Map is automatically displayed with TA traffic. If the bearing of TA traffic cannot be determined (Figures 6-147 and 6-150), a yellow text banner will be displayed in the center of the Traffic Map Page and in the lower-left of maps with traffic displayed instead of a TA symbol. The text will indicate “TA” followed by the distance, relative altitude, and vertical trend arrow for the TA traffic, if known. A TA will be displayed for at least eight seconds, even if the conditions that initially triggered the TA are no longer present. Inset Map Displays When TA is Detected Figure 6-163 Traffic Annunciation (PFD) Bearing Relative Altitude Distance “One o’clock” through “Twelve o’clock” or “No Bearing” “High”, “Low”, “Same Altitude” (if within 200 feet of own altitude), or “Altitude not available” “Less than one mile”, “One Mile” through “Ten Miles”, or “More than ten miles” Table 6-32 TA Descriptive Voice Announcements 472 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE SYSTEM TEST NOTE: GTS 850 traffic surveillance is not available during the system test. Use caution when performing a system test while in-flight. The GTS 850 provides a system test mode to verify the TCAS I system is operating normally. The test takes about ten seconds to complete. When the system test is initiated, a test pattern of traffic symbols is displayed on the Traffic Map Page (Figure 6-164). If the system test passes, system announces “TCAS System Test Passed”, otherwise the system announces “TCAS System Test Failed.” When the system test is complete, the GTS 850 enters Standby or Failure Mode based on the test result. 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. 3) Turn the Joystick to set the range to 2/6 nm to allow for full traffic test pattern display. 4) Select the TEST Softkey. Or: 1) Press the MENU Key and turn the small FMS knob to select ‘Test Mode’. 2) Press the ENT Key. Test Mode Annunciation Operating Mode Non-Threat Traffic at 11 o’clock, Distance 3.6 nm, 1000’ Above, Level Proximity Traffic at 1 o’clock, Distance 3.6 nm, 1000’ Below, Descending TA at 9 o’clock, Distance 2.0 nm, 200’ Below, Climbing Figure 6-164 System Test in Progress with Test Pattern 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 473 HAZARD AVOIDANCE OPERATION NOTE: The GTS 850 automatically transitions from STANDBY to OPERATE mode eight seconds after takeoff. The unit also automatically transitions from OPERATE to STANDBY mode 24 seconds after landing. After power-up, the GTS 850 is in Standby Mode. The unit must be in Operating Mode for traffic to be displayed and for TAs to be issued. Selecting the OPERATE Softkey allows the GTS 850 to switch from Standby Mode to Operating Mode as necessary. Selecting the STANDBY Softkey forces the unit into Standby Mode. Switching from Operating Mode to Standby Mode: On the Traffic Page, select the STANDBY Softkey Or: 1) Press the MENU Key and turn the small FMS knob to select ‘Standby Mode’. 2) Press the ENT Key. Switching from Standby Mode to Operating Mode: On the Traffic Page, select the OPERATE Softkey Or: 1) Press the MENU Key and turn the small FMS knob to select ‘Operate Mode’. 2) Press the ENT Key. The GTS 850 switches from Standby Mode to Operating Mode as necessary. TRAFFIC MAP PAGE The Map - Traffic Map Page shows surrounding traffic data in relation to the aircraft’s current position and altitude, without basemap clutter. It is the principal map page for viewing TCAS I traffic information. Aircraft orientation is always heading up unless there is no valid heading. Map range is adjustable with the Joystick from two to 40 nm, as indicated by the map range rings. The traffic mode and altitude display mode are annunciated in the upper left corner of the page. 474 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Operating Mode Traffic Display Range Altitude Mode Non-Threat Traffic, 2500’ Above, Descending Traffic Advisory, 500’ Below, Climbing “No Bearing” Traffic (Bearing Undetermined), Distance 4.0 nm, 500’ Above, Descending Traffic Advisory OffScale, 400’ Below, Level Proximity Traffic, 900’ Above, Level, Flight ID Displayed Non-Threat Traffic, Altitude Not Reported Figure 6-165 Traffic Map Page Displaying traffic on the Traffic Map Page: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. 3) Select the OPERATE Softkey to begin displaying traffic. ‘OPERATING’ is displayed in the Traffic mode field. 4) Select the STANDBY Softkey to place the system in the Standby mode. ‘STANDBY’ is displayed in the Traffic mode field. 5) Turn the Joystick clockwise to display a larger area or counter-clockwise to display a smaller area. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 475 HAZARD AVOIDANCE Altitude Display The Pilot can select the volume of airspace in which non-threat and proximity traffic is displayed. TAs occurring outside of these limits will always be shown. Changing the altitude range: 1) On the Traffic Map Page, select the ALT MODE Softkey. 2) Select one of the following Softkeys: • ABOVE: Displays non-threat and proximity traffic from 9000 feet above the aircraft to 2700 feet below the aircraft. Typically used during climb phase of flight. • NORMAL: Displays non-threat and proximity traffic from 2700 feet above the aircraft to 2700 feet below the aircraft. Typically used during enroute phase of flight. • BELOW: Displays non-threat and proximity traffic from 2700 feet above the aircraft to 9000 feet below the aircraft. Typically used during descent phase of flight. • UNREST (unrestricted): All traffic is displayed from 9900 feet above and 9900 feet below the aircraft. 3) To return to the Traffic Page, select the BACK Softkey. Or: 1) Press the MENU Key. 2) Turn the small FMS Knob to select one of the following (see softkey description in step 2 above): • ABOVE • NORMAL • BELOW • UNRESTRICTED 3) Select the ENT Softkey. Flight ID Display NOTE: This feature requires the installation of a transponder with the Automatic Dependent Surveillance - Broadcast (ADS-B) Out capability. The Flight IDs of other aircraft (when available) can displayed on the Traffic Map Page (Figure 6-166). When a flight ID is received, it will appear above or below the corresponding traffic symbol on the Traffic Map Page when this option is enabled. 476 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Flight ID Figure 6-166 Traffic Map Page with Flight IDs Enabled Enabling/Disabling Flight ID Display: On the Traffic Map Page, select the FLT ID Softkey. Or: 1) Press the MENU Key. 2) Turn the small FMS Knob to select ‘Show Flight IDs’ or ‘Hide Flight IDs’ (choice dependent on current state) (Figure 6-167). 3) Press the ENT Key. Figure 6-167 Traffic Map Page Menu 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 477 HAZARD AVOIDANCE Traffic Map Page Display Range The display range on the Traffic Map Page can be changed at any time. Map range is adjustable with the Joystick from two to 40 nm, as indicated by the map range rings. Changing the display range on the Traffic Map Page: 1) Turn the Joystick. 2) The following range options are available: • 2 nm • 2 and 6 nm • 6 and 12 nm • 12 and 24 nm • 24 and 40 nm ADDITIONAL TRAFFIC DISPLAYS Traffic information can be displayed on the following maps on the MFD when the unit is operating: • Navigation Map Page • Nearest Pages • Traffic Map Page • Active Flight Plan Page • Trip Planning Page • System Pages Traffic information can also be displayed on the PFD when the Synthetic Vision Technology (SVT) option is installed and enabled. See the Additional Features Section for details. Displaying traffic information (MFD maps other than the Traffic Map Page): 1) Select the MAP Softkey. 2) Select the TRAFFIC Softkey. Traffic is now displayed on the map. When traffic is selected on maps other than the Traffic Map Page, a traffic icon is shown to indicate traffic is enabled for display (Figure 6-168). Displaying traffic on the Navigation Map 1) Ensure the traffic system is operating. With the Navigation Map displayed, select the MAP Softkey. 2) Select the TRAFFIC Softkey. Traffic is now displayed on the map as shown in the figure. 478 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Non-Threat Traffic Traffic Advisory Proximity Traffic Proximity Traffic TA Off Scale Banner Traffic Icon “No Bearing” Traffic Advisory Figure 6-168 TCAS I Traffic on Navigation Map Customizing the traffic display on the Navigation Map Page: 1) Select the Navigation Map Page. 2) Press the MENU Key. 3) With Map Setup highlighted, press the ENT Key (Figure 6-169). 4) Turn the small FMS Knob to select the Traffic Group and press the ENT Key (Figure 6-170). 5) Turn the large FMS Knob or press the ENT Key to scroll through the selections (Figure 6-171). • TRAFFIC – Turns the display of traffic data on or off • TRAFFIC MODE – Selects the traffic mode for display; select from: - All Traffic - Displays all traffic - TA/PA - Displays Traffic Advisories and Proximity Advisories - TA ONLY - Displays Traffic Advisories only • TRAFFIC SMBL – Selects the maximum range at which traffic symbols are shown • TRAFFIC LBL – Selects the maximum range at which traffic labels are shown with the option to turn off 6) Turn the small FMS Knob to scroll through options (ON/OFF, range settings, etc.). 7) Press the ENT Key to select an option. 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 479 HAZARD AVOIDANCE Figure 6-169 Navigation Map Page Menu Figure 6-170 Navigation Map Page Setup Menu Figure 6-171 Navigation Map Page Setup Menu, Traffic Group The Navigation Map Page Setup Menu also controls the display of traffic. The setup menu controls the map range settings. Traffic data symbols and labels can be decluttered from the display. If a map range larger than the map range setting is selected, the data is removed from the map. Maps besides the Traffic Map Page use settings based on those selected for the Navigation Map Page. Traffic information can also be displayed on the PFD Inset Map by pressing the INSET Softkey. A traffic map will appear in heading up orientation. Traffic information can also be overlaid with navigation, topographic and optional data link weather information. Displaying traffic information (PFD Inset Map): 1) Press the INSET Softkey. 2) Press the TRAFFIC Softkey to display traffic data on the inset map (TRFC-1). 3) Press the softkey again to display the traffic-only inset (TRFC-2). 4) Press the softkey again to remove traffic data. 480 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE SYSTEM STATUS The traffic mode is annunciated in the upper left corner of the Traffic Map Page. Traffic Mode Annunciation (Traffic Map Page) Mode TCAS I Self-test Initiated TEST (also shown in white in center of page) TCAS I Operating OPERATING TCAS I Standby STANDBY (also shown in white in center of page) TCAS I Failed* FAIL Traffic Display Status Icon (Other Maps) * See Table 6-34 for additional failure annunciations Table 6-33 TCAS I Modes If the traffic unit fails, an annunciation as to the cause of the failure is shown in the center of the Traffic Map Page. During a failure condition, the Operating Mode cannot be selected. Traffic Map Page Annunciation NO DATA DATA FAILED FAILED Description Data is not being received from the TCAS I unit Data is being received from the TCAS I unit, but the unit is self-reporting a failure Incorrect data format received from the TCAS I unit, or optional radar altimeter was operational at system power-up but has subsequently failed Table 6-34 TCAS I Failure Annunciations 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 481 HAZARD AVOIDANCE The annunciations to indicate the status of traffic information appear in a banner at the lower left corner of maps on which traffic can be displayed. Traffic Status Banner Annunciation TA OFF SCALE TA X.X ± XX ↕ TRFC FAIL NO TCAS DATA Description A Traffic Advisory is outside the selected display range*. Annunciation is removed when traffic comes within the selected display range. System cannot determine bearing of Traffic Advisory**. Annunciation indicates distance in nm, altitude separation in hundreds of feet, and altitude trend arrow (climbing/ descending). TCAS I unit has failed (unit is self-reporting a failure or sending incorrectly formatted data) Data is not being received from the TCAS I unit *Shown as symbol on Traffic Map Page **Shown in center of Traffic Map Page Table 6-35 TCAS I Traffic Status Annunciations 482 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE 6.9 TCAS II TRAFFIC WARNING: Traffic information shown on system displays is provided to aid in visually acquiring traffic. Traffic avoidance maneuvers are based upon TCAS II Resolution Advisories, ATC guidance, or positive visual acquisition of conflicting traffic. NOTE: TIS is disabled when TCAS II is installed. NOTE: Refer to the TCAS II documentation for a detailed discussion of the TCAS II system.. TCAS II SYMBOLOGY The optional TCAS II system is designed to help in detection and avoidance of other aircraft. TCAS II uses an on-board interrogator-processor and the Mode S transponder for the air-to-air traffic data link. The system displays traffic using the TCAS II symbology shown in Table 6-36. TCAS Symbol Description Non-Threat Traffic Proximity Advisory (PA) Traffic Advisory (TA) Traffic Advisory Off Scale Resolution Advisory (RA) Resolution Advisory Off Scale Table 6-36 TCAS II Symbol Description A Non-threat Proximity Advisory, shown as an open white diamond, indicates that an intruding aircraft is at greater than ±1200 feet relative altitude or the distance is beyond 5 nm. A Proximity Advisory indicates that the intruding aircraft is within ±1200 feet and is within 6 nm range, but is still not considered a threat. A Traffic Advisory (TA) alerts the crew to a potentially hazardous intruding aircraft closing to within 20 to 48 seconds of a potential collision area. A Traffic Advisory that is beyond the selected display range is indicated by a half TA symbol at the edge of the screen at the relative bearing of the intruder. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 483 HAZARD AVOIDANCE A Resolution Advisory (RA) alerts the crew to intruding aircraft that are closing to within 15 to 35 seconds of a potential collision area. RAs include vertical guidance maneuvers designed to increase or maintain vertical separation from intruding aircraft. An RA that is beyond the selected display range is indicated by a half RA symbol at the edge of the screen at the relative bearing of the intruder. TCAS II ALERTS NOTE: Refer to the TCAS II documentation for information on alerts generated by the TCAS II equipment. When the TCAS II unit issues a TA or RA, the following occur: • The traffic system generates a voice alert when a TA or RA is displayed. • A ‘TRAFFIC’ annunciation appears at the top right of the airspeed indicator on the PFD, flashes for 5 seconds and remains displayed until no TAs or RAs are detected in the area. RA ‘TRAFFIC’ annunciations are white text with red backgrounds; TA ‘TRAFFIC’ annunciations are black text with yellow backgrounds. If a TA and RA occur simultaneously, only the red and white RA ‘TRAFFIC’ annunciation is shown. • The PFD Inset Map is automatically displayed with TA or RA traffic. • During an RA only, voice alert(s) provide vertical guidance to resolve the traffic conflict while the PFD displays pitch and vertical speed cues (Figure 6-172). Additional voice alerts occur to denote changes in the RA status. RA Annunciation TA Annunciation Fly-To Pitch Cue Fly-To Vertical Speed No-Fly Pitch Cue No-Fly Vertical Speed Range Inset Map Displays When TA or RA is Detected Traffic/Map Inset Softkey Figure 6-172 Traffic Annunciation with Resolution Advisory (PFD) 484 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE RESOLUTION ADVISORIES During an RA, vertical guidance indications appear on the Attitude Indicator and Vertical Speed indicators of the PFD to provide visual pitch cues for the flight crew to use to achieve (or maintain) vertical separation from intruding traffic (Figure 6-173). During an RA, the Attitude Indicator depicts a range of pitch attitudes to avoid using no-fly pitch cues positioned on the pitch ladder. The no-fly pitch cues are indicated by red open trapezoid-shaped areas encompassing the range of pitch attitudes to be avoided during an RA. If an RA requires a change in existing pitch attitude, a green rectangular fly-to pitch cue will appear above or below the no-fly pitch cue to indicate recommended pitch attitudes. If multiple intruding aircraft limit available pitch travel in both directions, two no-fly pitch cues will appear on the pitch ladder, indicating flight should occur between the two no-fly pitch cues. While an RA is occurring, the Vertical Speed Indicator (VSI) shows a range of vertical speeds required to resolve the traffic conflict. A red vertical bar appears on the VSI scale to indicate the range of vertical speeds to be avoided during the RA. If the current aircraft vertical speed is within this red range, the pointer on the VSI also becomes red. When an RA directs the flight crew to fly to (or maintain) a vertical speed, a green vertical bar appears on the VSI scale at the recommended vertical speed range. Pitch cues on the Attitude Indicator and vertical bars on the Vertical Speed Indicator are removed when the RA condition has been resolved. The TCAS II system will also issue a voice alert when the aircraft is clear of the RA conflict. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 485 HAZARD AVOIDANCE Descend Climb Maintain, Don’t Climb Maintain, Don’t Descend Maintain, Don’t Climb and Don’t Descend Adjust Vertical Speed Figure 6-173 Example Resolution Advisory Visual Cues 486 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE SYSTEM TEST NOTE: Refer to the TCAS II documentation for information on specific voice alerts issued during system tests. The TCAS II system can be tested on either the PFD or MFD. On the PFD: 1) Press the XPDR/TFC Softkey. 2) Press the TCAS Softkey. 3) Press the TEST Softkey. On the MFD: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. 3) Turn the Joystick to set the range to 2/6 nm to allow for full traffic test pattern display. 4) Select the TEST Softkey. Or: 1) Press the MENU Key. 2) Turn the small FMS knob to select ‘Test Mode’. 3) Press the ENT Key. When initiating the system test, the TCAS II unit issues the voice alert “TCAS Test”. A traffic test pattern is displayed on the Traffic Map Page of the MFD, and on the Inset Map on the PFD (which appears if not already displayed.) A Resolution Advisory (RA) alert annunciation is shown on the PFD, and pitch cues appear on the attitude indicator and vertical speed indicator indicating not to descend, and not to climb greater than 2000 feet per minute. The system test takes approximately eight seconds to complete. A voice alert indicates whether the test has passed or failed. Visual annunciations also indicate a system test has failed (Tables 6-34, 6-35, and 6-36). MFD Traffic Map Page PFD Figure 6-174 TCAS II System Test Displays 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 487 HAZARD AVOIDANCE OPERATION NOTE: The traffic system automatically changes modes based on certain flight parameters. Refer to the TCAS II unit’s documentation for information on automatic mode selection. To display TCAS II Traffic, the system must be in TA ONLY or TA/RA Mode. These modes can be accessed on the PFD or on the Traffic Map Page of the MFD. Switching from standby mode to TA only or TA/RA mode: On the MFD: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. 3) Select the TA ONLY or TA/RA Softkey Or: 1) Press the MENU Key and turn the small FMS knob to select ‘TA Only Mode’ or ‘TA/RA Mode’. 2) Press the ENT Key. The unit switches from Standby Mode to TA Only or TA/RA Mode as necessary. On the PFD: 1) Press the XPDR/TFC Softkey. 2) Press the MODE Softkey. 3) Press the TA ONLY or TA/RA Softkey to select an operating mode. Switching from TA ONLY or TA/RA mode to Standby Mode: On the MFD: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. 3) Select the TFC STBY Softkey Or: 1) Press the MENU Key and turn the small FMS knob to select ‘Traffic Standby Mode’. 2) Press the ENT Key. 488 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE TRAFFIC MAP PAGE The Map - Traffic Map Page shows surrounding TCAS II traffic data in relation to the aircraft’s current position and altitude, without basemap clutter. It is the principal MFD map page for viewing TCAS II traffic. Aircraft orientation is always heading up unless there is no valid heading. Map range is adjustable with the Joystick from two to 40 nm, as indicated by the map range rings. The traffic mode and altitude display mode are annunciated in the upper left corner of the Traffic Map Page. Operating Mode Altitude Mode Traffic Display Range Rings Proximity Traffic, 400’ Below, Level Off Scale Traffic Advisory Resolution Advisory, 100’ Below, Descending Traffic Advisory, 500’ Above, Climbing “Non-Bearing” (Bearing Unknown) Resolution Advisory, Distance 3.1 nm, 4500’ Below, Climbing Non-Threat Traffic, 400’ Below, Level Off Scale Resolution Advisory Figure 6-175 Traffic Map Page Displaying traffic on the Traffic Map Page: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. 3) Select the TA ONLY or TA/RA Softkey to begin displaying traffic. ‘TA ONLY’ or ‘TA/RA’ is displayed in the Traffic mode field. 4) Select the REL or ABS Softkey to display the relative or absolute altitude of other aircraft. 5) Select the TFC STBY Softkey to place the system in the Standby Mode. ‘STANDBY’ is displayed in the Traffic mode field. 6) Turn the Joystick clockwise to display a larger area or counter-clockwise to display a smaller area. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 489 HAZARD AVOIDANCE Altitude Display The flight crew can select the volume of airspace in which non-threat and proximity traffic is displayed. Traffic Advisories (TAs) and Resolution Advisories (RAs) outside of these limits will always be shown. Changing the altitude range: On the PFD: 1) Press the XPDR/TFC Softkey. 2) Press the TCAS Softkey 3) Press the ALT RNG Softkey 4) Press one of the following altitude range Softkeys: • ABOVE: Displays non-threat and proximity traffic from 9900 feet above the aircraft to 2700 feet below the aircraft. Typically used during climb phase of flight. • NORMAL: Displays non-threat and proximity traffic from 2700 feet above the aircraft to 2700 feet below the aircraft. Typically used during enroute phase of flight. • BELOW: Displays non-threat and proximity traffic from 2700 feet above the aircraft to 9900 feet below the aircraft. Typically used during descent phase of flight. • UNREST (unrestricted): All traffic is displayed 5) Press the BACK Softkey. On the MFD: 1) On the Traffic Map Page, select the ALT RNG Softkey. 2) Select one of the following Softkeys (see softkey description in step 4 above): • ABOVE • NORMAL • BELOW • UNRESTRICTED 3) To return to the Traffic Page, select the BACK Softkey. Or: 1) Press the MENU Key. 2) Turn the small FMS Knob to select one of the following (see softkey description in step 4 above): • ABOVE • NORMAL • BELOW • UNRESTRICTED 3) Select the ENT Softkey. 490 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE Traffic Map Page Display Range The display range on the Traffic Map Page can be changed at any time. Map range is adjustable with the Joystick from two to 40 nm, as indicated by the map range rings. Changing the display range on the Traffic Map Page: 1) Turn the Joystick. 2) The following range options are available: • 2 nm • 2 and 6 nm • 6 and 12 nm • 12 and 24 nm • 24 and 40 nm ADDITIONAL TRAFFIC DISPLAYS Traffic information can be displayed on the following maps on the MFD when the unit is operating: • Navigation Map Page • Nearest Pages • Traffic Map Page • Active Flight Plan Page • Trip Planning Page • System (SYS) Pages Traffic information can also be displayed on the PFD when the Synthetic Vision Technology (SVT) option is installed and enabled. See the Additional Features Section for details. Displaying traffic information (MFD maps other than the Traffic Map Page): 1) Select the MAP Softkey. 2) Select the TRAFFIC Softkey. Traffic is now displayed on the map. When traffic is selected on maps other than the Traffic Map Page, the system displays a traffic status icon indicates traffic is enabled for display (Figure 6-176). 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 491 HAZARD AVOIDANCE Displaying traffic on the Navigation Map 1) Ensure the TCAS II system is operating. With the Navigation Map displayed, select the MAP Softkey. 2) Select the TRAFFIC Softkey. Traffic is now displayed on the map as shown in the figure. Proximity Traffic Traffic Advisory Resolution Advisory Non-Threat Traffic TA Off Scale Banner Traffic Overlay Enabled Icon Non-Bearing Resolution and Traffic Advisories Figure 6-176 TCAS II Traffic on Navigation Map Customizing the traffic display on the Navigation Map Page: 1) Select the Navigation Map Page. 2) Press the MENU Key. 3) With Map Setup highlighted, press the ENT Key (Figure 6-177). 4) Turn the small FMS Knob to select the Traffic Group and press the ENT Key (Figure 6-178). 5) Turn the large FMS Knob or press the ENT Key to scroll through the selections (Figure 6-179). • TRAFFIC – Turns the display of traffic data on or off • TRAFFIC MODE – Selects the traffic mode for display; select from: - All Traffic - Displays all traffic - TA/RA/PA - Displays Traffic Advisories, Resolution Advisories, and Proximity Advisories - TA/RA ONLY - Displays Traffic Advisories and Resolution Advisories only • TRAFFIC SMBL – Selects the maximum range at which traffic symbols are shown • TRAFFIC LBL – Selects the maximum range at which traffic labels are shown with the option to turn off 492 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE 6) Turn the small FMS Knob to scroll through options (ON/OFF, range settings, etc.). 7) Press the ENT Key to select an option. 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page. Figure 6-177 Navigation Map Page Menu Figure 6-178 Navigation Map Page Setup Menu Figure 6-179 Navigation Map Page Setup Menu, Traffic Group The Navigation Map Page Setup Menu also controls the display of traffic. The setup menu controls the map range settings. Traffic data symbols and labels can be decluttered from the display. If a map range larger than the map range setting is selected, the data is removed from the map. Maps besides the Traffic Map Page use settings based on those selected for the Navigation Map Page. Traffic information can also be displayed on the PFD Inset Map by pressing the TRFC/MAP Softkey. A traffic map will appear in heading up orientation. Traffic information can also be overlaid with navigation, topographic and optional data link weather information. Displaying additional information with Traffic on the PFD Inset Map. 1) Press the TRFC/MAP Softkey. Traffic map (TRFC-2) is displayed heading up. 2) Press the TRFC-2 Softkey. 3) Press the softkey(s) for the item(s) to be included on the PFD Inset Map. 4) Press the BACK Softkey. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 493 HAZARD AVOIDANCE SYSTEM STATUS The traffic mode is annunciated in the upper left corner of the Traffic Map Page. Traffic Mode PFD Traffic Mode Annunciation TCAS II Self-test Initiated (TEST) None Traffic Advisory and Resolution Advisory (TA/RA) None MFD Traffic Map Page Mode Annunciation TEST (‘TEST MODE’ also shown in white on top center of page) TA/RA Traffic Advisory Only (TA ONLY) TCAS II Standby (TFC STBY) Traffic Display Status Icon (Other Maps) TA ONLY Or: * STANDBY (also shown in white in center of page on ground, yellow in the air) FAIL TCAS II Failed** * Annunciation appears in yellow while in the air. ** See Table 6-38 for additional failure annunciations. Table 6-37 TCAS II Modes If the traffic unit fails, an annunciation as to the cause of the failure is shown in the center of the Traffic Map Page. Traffic Map Page Annunciation NO DATA DATA FAILED FAILED Description Data is not being received from the TCAS II unit Data is being received from the TCAS II unit, but the unit is self-reporting a failure Incorrect data format received from the TCAS II unit Table 6-38 TCAS II Failure Annunciations 494 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A HAZARD AVOIDANCE The annunciations to indicate the status of traffic information appear in a banner at the lower left corner of maps on which traffic can be displayed. Traffic Status Banner Annunciation RA OFF SCALE TA OFF SCALE RA X.X ± XX ↕ TA X.X ± XX ↕ TRFC FAIL NO TCAS DATA Description A Resolution Advisory is outside the selected display range*. Annunciation is removed when traffic comes within the selected display range A Traffic Advisory is outside the selected display range*. Annunciation is removed when traffic comes within the selected display range. System cannot determine bearing of Resolution Advisory**. Annunciation indicates distance in nm, altitude separation in hundreds of feet, and altitude trend arrow (climbing/ descending). System cannot determine bearing of Traffic Advisory**. Annunciation indicates distance in nm, altitude separation in hundreds of feet, and altitude trend arrow (climbing/ descending). TCAS II unit has failed (unit is self-reporting a failure or sending incorrectly formatted data) Data is not being received from the TCAS II unit *Shown as symbol on Traffic Map Page **Shown in center of Traffic Map Page Table 6-39 TCAS II Traffic Status Annunciations 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 495 HAZARD AVOIDANCE Blank Page 496 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM NOTE: The approved Airplane Flight Manual (AFM) always supersedes this Pilot’s Guide. The Garmin Automatic Flight Control System (Garmin AFCS) is fully integrated within the avionics architecture. The System Overview section provides a block diagram to support this system description. The Garmin AFCS functionality is distributed across the following Line Replaceable Units (LRUs): • GDU 1240A Primary Flight Displays (PFDs) (2) • GSA 81 AFCS Servos (3) • GMC 715 AFCS Control Unit • GSM 85A Servo Gearboxes (3) • GIA 63W Integrated Avionics Units (IAUs) (2) The Garmin AFCS can be divided into these main operating functions: • Flight Director (FD) — The Garmin AFCS flight director function can be coupled to either the pilot-side or copilot-side PFD data. The CPL Key selects the PFD source for the Flight Director. Commands for the selected flight director source are displayed on both PFDs. The flight director provides: – Vertical/lateral mode selection and processing – Command Bars showing pitch/roll guidance – Pitch and roll commands to the autopilot • Autopilot (AP) — Autopilot operation occurs within the pitch and roll servos. It provides automatic flight control in response to flight director steering commands, Attitude and Heading Reference System (AHRS) attitude and rate information, and airspeed. • Yaw Damper (YD) — The yaw servo provides Dutch roll damping and turn coordination in response to yaw rate, roll angle, lateral acceleration, and airspeed. • Manual Electric Pitch Trim (MEPT) — The pitch trim system provides manual electric pitch trim capability. • Automatic Pitch Trim (APT) — The pitch trim system provides automatic pitch trim when the autopilot is engaged 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 497 AUTOMATIC FLIGHT CONTROL SYSTEM 7.1 AFCS CONTROLS The AFCS Control Unit is positioned above the MFD, and has the following controls: 1 10 FD Keys Activate/deactivate the selected flight director (pilot- or copilot-side) in default vertical and lateral modes Press the other FD Key to toggle the corresponding PFD’s Command Bars off/on 2 NAV Key HDG Key 4 AP Key 5 YD Key 6 ALT Key 7 VNV Key 8 VS Key 9 FLC Key 20 CRS Knobs 3 11 12 SPD SEL Knob UP/DN Wheel 14 ALT SEL Knob 13 15 CSC Key 16 CPL Key Selects/deselects Navigation Mode Selects/deselects Heading Select Mode Engages/disengages the autopilot Engages/disengages the yaw damper Selects/deselects Altitude Hold Mode Selects/deselects Vertical Path Tracking Mode for Vertical Navigation flight control Selects/deselects Vertical Speed Mode Selects/deselects Flight Level Change Mode Adjust the Selected Course (while in VOR, LOC, or OBS Mode) in 1° increments on the Horizontal Situation Indicator (HSI) of the corresponding PFD Press to re-center the Course Deviation Indicator (CDI) and return course pointer directly TO the bearing of the active waypoint/station Adjusts the Airspeed Reference and bug in 1-kt (0.01 M) increments Press to toggle the Airspeed Reference units from IAS to Mach Adjusts the Vertical Speed Reference and bug in 100-fpm increments Adjusts the Selected Altitude and bug in 100-ft increments (a finer resolution of 10 feet is available under approach conditions) Selects/deselects Current Speed Control (if available) when Altitude Hold Mode is active Selects the PFD data source (pilot-side or copilot-side) for the Flight Director. When the flight director source is switched, the modes revert to default. An arrow in the AFCS Status Box indicates the active FD source (pilot- or copilot-side). 17 HDG SEL Knob Adjusts the Selected Heading and bug in 1° increments on the HSI (both PFDs) APR Key 19 BANK Key 18 498 Press to synchronize the Selected Heading to the current heading on the pilot-side PFD Selects/deselects Approach Mode Manually selects/deselects Low Bank Mode Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM 1 2 3 20 19 18 17 4 16 5 6 15 14 7 8 9 10 13 12 11 Figure 7-1 GMC 715 AFCS Control Unit The following AFCS controls are located separately from the AFCS Control Unit: AP DISC Switch (Autopilot Disconnect) Disengages the autopilot and yaw damper, and interrupts pitch trim operation CWS Button (Control Wheel Steering) While pressed, allows manual control of the aircraft while the autopilot is engaged and synchronizes the flight director’s Command Bars with the current aircraft pitch (if not in Glideslope or Glidepath Mode) and roll (if in Roll Hold Mode) An AP DISC Switch is located on each control wheel. This switch may be used to acknowledge an autopilot disconnect alert and mute the associated aural alert. A CWS Button is located on each control wheel. Upon release of the CWS Button, the flight director may establish new pitch and roll references, depending on the current vertical and lateral modes. CWS operation details are discussed in the respective mode sections of this manual. TO/GA Switch (Go Around) Disengages the autopilot, if engaged, and selects flight director Takeoff Mode (on ground) or Go Around Mode (in air) The TO/GA Switch is located on the throttle handle. This switch also activates the missed approach when the selected navigation source is GPS or when the navigation source is VOR/LOC and a valid frequency has been tuned. Used to command manual electric pitch trim MEPT Switch (Manual Electric An MEPT Switch is located on each control wheel. Pitch Trim) The pilot side MEPT Switch has priority over the copilot side MEPT Switch. This composite switch is split into left and right sides. The left switch is the ARM contact and the right switch controls the DN (forward) and UP (rearward) contacts. Manual trim commands are generated only when both sides of the switch are operated simultaneously. Pushing either MEPT Switch disengages the autopilot, if engaged, but does not affect yaw damper operation. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 499 AUTOMATIC FLIGHT CONTROL SYSTEM 7.2 FLIGHT DIRECTOR OPERATION The flight director function provides pitch and roll commands to the AFCS and displays them on the PFDs. With the flight director active, the aircraft can be hand-flown to follow the path shown by the Command Bars. Maximum commanded pitch (±20°) and roll (30°) angles, vertical acceleration, and roll rate are limited to values established during AFCS certification. The flight director also provides commands to the autopilot. ACTIVATING THE FLIGHT DIRECTOR An initial press of a key listed in Table 7-1 activates the flight director in the listed modes. Control Pressed FD PFD Data Source Modes Selected FD Key (pilot-side)* FD Key (copilotside)* AP Key CWS Button Pilot-side Lateral Roll Hold (default) Pilot-side Roll Hold (default) ROL Pitch Hold (default) PIT Pilot-side Pilot-side GA Switch Pilot-side ALT Key VS Key Pilot-side Pilot-side Roll Hold (default) Roll Hold (default) Roll Hold (default) Roll Hold (default) Roll Hold (default) Roll Hold (default) ROL ROL ROL ROL ROL ROL PIT PIT TO GA ALT VS VNV Key Pilot-side Roll Hold (default) ROL Pitch Hold (default) Pitch Hold (default) Takeoff (on ground) Go Around (in air) Altitude Hold Vertical Speed Vertical Path Tracking** NAV Key Pilot-side Navigation*** APR Key Pilot-side Approach*** HDG Key Pilot-side Heading Select ROL Vertical Pitch Hold (default) PIT GPS VOR LOC BC GPS VOR LOC HDG VPTH Pitch Hold (default) PIT Pitch Hold (default) PIT Pitch Hold (default) PIT *Subsequent presses of the FD Key will toggle the flight director on/off on its respective side. However, pressing the FD Key for the inactive flight director only removes the Command Bars from the corresponding display. The FD Keys are disabled when the autopilot is engaged. ** Valid VNV flight plan must be entered before VNV Key press activates flight director. ***The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before NAV or APR Key press activates flight director. Table 7-1 Flight Director Activation 500 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM AFCS STATUS BOX Flight director mode annunciations are displayed on the PFDs when the flight director is active. Flight director selection, autopilot, yaw damper, and Current Speed Control (if available) statuses are shown in the center of the AFCS Status Box. Lateral flight director modes are displayed on the left and vertical on the right. Armed modes are displayed in white and active in green or magenta (if the mode reference is provided by the GPS navigation function). Yaw Current Autopilot Damper Speed Status Control Status Lateral Modes Armed Active Flight Director Indicator Arrow Vertical Modes Active Armed AFCS Status Box Selected Altitude Command Bars GPS is Selected Navigation Source Figure 7-2 PFD AFCS Display 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 501 AUTOMATIC FLIGHT CONTROL SYSTEM FLIGHT DIRECTOR MODES Flight director modes are normally selected independently for the pitch and roll axes. Unless otherwise specified, all mode keys are alternate action (i.e., press on, press off). In the absence of specific mode selection, the flight director reverts to the default pitch and/or roll modes(s). Armed modes are annunciated in white and active in green or magenta (if the mode reference is provided by the GPS navigation function) in the AFCS Status Box. Under normal operation, when the control for the active flight director mode is pressed, the flight director reverts to the default mode(s) for the axis(es). Automatic transition from armed to active mode is indicated by the white armed mode annunciation moving to the active mode field and flashing for 5 seconds. If the information required to compute a flight director mode becomes invalid or unavailable, the flight director automatically reverts to the default mode for that axis. A flashing yellow mode annunciation indicates loss of sensor (ADC) or navigation data (VOR, LOC, GPS, VNV, SBAS) required to compute commands. When such a loss occurs, the system automatically begins to roll the wings level (enters Roll Hold Mode) or maintain the pitch angle (enters Pitch Hold Mode), depending on the affected axis. The flashing annunciation stops when the affected mode key is pressed or another mode for the axis is selected. After 5 seconds, if no action is taken, the flashing annunciation stops and the flight director enters the default mode for the affected axis. Figure 7-3 Loss of VOR Signal The flight director is automatically disabled if the attitude information required to compute the default flight director modes becomes invalid or unavailable. FLIGHT DIRECTOR SELECTION The Garmin AFCS flight director can be coupled to either the pilot-side or copilot-side PFD data using the CPL Key. When the pilot-side or copilot-side data source is changed, the vertical and lateral modes revert to default. The autopilot follows the selected flight director only, indicated by an arrow pointing toward either the pilot or copilot side, in the center of the AFCS Status Box. The currently active flight director may be turned off and the Command Bars removed from the displays by pressing the active FD Key again. Pressing the FD Key for the inactive flight director only removes the Command Bars from the corresponding display. The FD key for the selected flight director is disabled when the autopilot is engaged. Pilot-side Flight Director Selected Copilot-side Flight Director Selected Figure 7-4 Flight Director Selection Indications 502 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM COMMAND BARS Upon activation of the flight director, Command Bars are displayed in magenta on the PFDs as single cues or cross pointers. The aircraft symbol (in yellow) changes to accommodate the Command Bar format; the Command Bars do not override the aircraft symbol. The single-cue Command Bars (Figure 7-5) move together vertically to indicate pitch commands and bank left or right to indicate roll commands. Command Bars displayed as a cross pointer (Figure 7-6) move independently to indicate pitch (horizontal bar) and roll (vertical bar) commands. Both PFDs show the same Command Bar format. Command Bars Aircraft Symbol Figure 7-5 Single-cue Command Bars Command Bars Aircraft Symbol Figure 7-6 Cross-pointer Command Bars Changing Command Bar format: 1) Use the FMS Knob to select the AUX - System Setup Page on the MFD. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight ‘Format Active’ in the ‘Flight Director’ box. 4) Turn the small FMS Knob to highlight the desired format. ’SNGL CUE’ to display Command Bars as a single cue (Aircraft Symbol in figure 7-5). Or: ’X-POINTER’ to display Command Bars as a cross pointer (Aircraft Symbol in Figure 7-6). If the attitude information being sent to the flight director becomes invalid or unavailable, the Command Bars are removed from the display. The flight director Command Bars also disappear if the pitch exceeds +30˚/-20˚ or bank exceeds 65˚. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 503 AUTOMATIC FLIGHT CONTROL SYSTEM 7.3 VERTICAL MODES Table 7-2 lists the AFCS vertical modes with their corresponding controls and annunciations. The mode reference is displayed next to the active mode annunciation for Altitude Hold, Vertical Speed, and Flight Level Change modes. The UP/DN Wheel can be used to change the vertical mode reference while operating under Vertical Speed Mode. Vertical Mode Pitch Hold Description Control Annunciation Holds the current aircraft pitch attitude; may be used to climb/descend to the (default) PIT Selected Altitude Selected Altitude Capture Captures the Selected Altitude Altitude Hold Holds the current altitude reference Reference Range ±20˚ * ALTS ALT Key ALT -1000 ft up to +41000 ft VS ±4000 fpm Maintains the current aircraft vertical speed; may be used to climb/descend to VS Key the Selected Altitude Maintains the current aircraft airspeed (in Flight Level Change IAS or Mach) while the aircraft is climbing/ FLC Key descending to the Selected Altitude Captures and tracks descent legs of an VNV Vertical Path Tracking active vertical profile Key Captures the Vertical Navigation (VNV) VNV Target Altitude Capture ** Target Altitude Captures and tracks the SBAS glidepath on Glidepath approach APR Key Captures and tracks the ILS glideslope on Glideslope approach Commands a constant pitch angle and Takeoff wings level on the ground in preparation for takeoff TO/GA Disengages the autopilot and commands a Switch Go Around constant pitch angle and wings level while in the air Vertical Speed FLC 80 – 275 kt 0.4 – 0.7 M VPTH ALTV GP GS TO 5.5 – 11˚ *** GA 2 – 7.5˚ *** * ALTS is armed automatically when PIT, VS, FLC, TO, or GA is active, and under VPTH when the Selected Altitude is to be captured instead of the VNV Target Altitude. ** ALTV is armed automatically under VPTH when the VNV Target Altitude is to be captured instead of the Selected Altitude. *** The specific reference value is based on the flap setting and the presence of icing conditions. Table 7-2 Flight Director Vertical Modes 504 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM PITCH HOLD MODE (PIT) When the flight director is activated (with the FD Key) or switched, Pitch Hold Mode is selected by default. Pitch Hold Mode is indicated as the active vertical mode by the ‘PIT’ annunciation. This mode may be used for climb or descent to the Selected Altitude (shown above the Altimeter), since Selected Altitude Capture Mode is automatically armed when Pitch Hold Mode is activated. In Pitch Hold Mode, the flight director maintains a constant pitch attitude, the pitch reference. The pitch reference is set to the aircraft pitch attitude at the moment of mode selection. If the aircraft pitch attitude exceeds the flight director pitch command limitations, the flight director commands a pitch angle equal to the nose-up/down limit. CHANGING THE PITCH REFERENCE When operating in Pitch Hold Mode, the pitch reference can be adjusted by pressing the CWS Button, hand-flying the aircraft to establish a new pitch reference, then releasing the CWS Button. Pitch Hold Mode Active Selected Altitude Capture Mode Armed Selected Altitude Command Bars Maintain Desired Pitch Reference Figure 7-7 Pitch Hold Mode 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 505 AUTOMATIC FLIGHT CONTROL SYSTEM SELECTED ALTITUDE CAPTURE MODE (ALTS) Selected Altitude Capture Mode is automatically armed with activation of the following modes: • Pitch Hold • Takeoff/Go Around (if the Selected Altitude is at least 400 feet above the current aircraft altitude) • Vertical Speed • Vertical Path Tracking (if the Selected Altitude is to be captured instead of the VNAV Target Altitude) • Flight Level Change The white ‘ALTS’ annunciation indicates Selected Altitude Capture Mode is armed (see Figure 7-7 for example). The ALT SEL Knob is used to set the Selected Altitude (shown above the Altimeter) until Selected Altitude Capture Mode becomes active. As the aircraft nears the Selected Altitude, the flight director automatically transitions to Selected Altitude Capture Mode with Altitude Hold Mode armed (Figure 7-8). This automatic transition is indicated by the green ‘ALTS’ annunciation flashing for up to 5 seconds and the appearance of the white ‘ALT’ annunciation. At 50 feet from the Selected Altitude, the flight director automatically transitions from Selected Altitude Capture to Altitude Hold Mode and holds the Selected Altitude (when within 50 feet of the selected altitude depending on vertical speed ALT mode may activate directly). As Altitude Hold Mode becomes active, the white ‘ALT’ annunciation moves to the active vertical mode field and flashes green for 5 seconds to indicate the automatic transition. Flash Up to 5 sec, Indicating Automatic Transition Figure 7-8 Automatic Mode Transitions During Altitude Capture CHANGING THE SELECTED ALTITUDE NOTE: Pressing the CWS Button while in Selected Altitude Capture Mode does not cancel the mode. Use of the ALT SEL Knob to change the Selected Altitude while Selected Altitude Capture Mode is active causes the flight director to revert to Pitch Hold Mode with Selected Altitude Capture Mode armed for the new Selected Altitude. ALTITUDE HOLD MODE (ALT) NOTE: To serve as a visual reminder of a target airspeed, the pilot can adjust the cyan Airspeed Reference Bug using the SPD SEL Knob when NOT in Flight Level Change Mode or Altitude Hold Mode (with CSC engaged). If Altitude Hold Mode is activated by pressing the ALT Key; the flight director maintains the current aircraft altitude (to the nearest 10 feet). Altitude Hold Mode active is indicated by an ‘ALT’ annunciation in the AFCS Status Box. 506 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM Altitude Hold Mode is automatically armed when the flight director is in either of the following modes: • Selected Altitude Capture (see Figure 7-7) • VNV Target Altitude Capture (see Figure 7-17) The transition to Altitude Hold Mode automatically occurs when the altitude error is less than 50 feet. In this case, the Selected or VNV Target Altitude becomes the flight director’s altitude reference. The active mode annunciation ‘ALT’ appears in magenta if the transition was made from VNV Target Altitude Capture Mode. CHANGING THE ALTITUDE REFERENCE NOTE: Turning the ALT SEL Knob while in Altitude Hold Mode changes the Selected Altitude, but not the flight director’s altitude reference, and does not cancel the mode. With the CWS Button pressed, the aircraft can be hand-flown to a new altitude reference. When the CWS Button is released at the desired altitude, the new altitude is established as the altitude reference. CURRENT SPEED CONTROL (IF AVAILABLE) Current Speed Control (if available) can be engaged if the autopilot is engaged and Altitude Hold Mode (ALT) or VNV Target Altitude Capture (ALTV) Mode is active. When the CSC Key is pressed, the Full Authority Digital Engine Control (FADEC) varies engine thrust to maintain the desired Airspeed Reference (green Airspeed Reference Bug), within a certain control range. NOTE: For CSC engagement and disengagement detailed conditions, see the approved Pilot’s Operating Handbook (POH). Current Speed Control Active Altitude Hold Mode Active Airspeed Reference Selected Altitude Airspeed Reference Bug Selected Altitude Bug Command Bars Hold Pitch Attitude to Maintain Altitude Reference Figure 7-9 Altitude Hold Mode 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 507 AUTOMATIC FLIGHT CONTROL SYSTEM VERTICAL SPEED MODE (VS) In Vertical Speed Mode, the flight director acquires and maintains a Vertical Speed Reference (shown above the Vertical Speed Indicator). Current aircraft vertical speed (to the nearest 100 fpm) becomes the Vertical Speed Reference at the moment of Vertical Speed Mode activation. This mode may be used for climb or descent to the Selected Altitude (shown above the Altimeter) since Selected Altitude Capture Mode is automatically armed when Vertical Speed Mode is selected. When Vertical Speed Mode is activated by pressing the VS Key, ‘VS’ is annunciated in green in the AFCS Status Box. The Vertical Speed Reference is displayed above the Vertical Speed Indicator. A Vertical Speed Reference Bug corresponding to the Vertical Speed Reference is shown on the indicator. CHANGING THE VERTICAL SPEED REFERENCE The Vertical Speed Reference (shown above the Vertical Speed Indicator) may be changed by: • Using the UP/DN Wheel • Pressing the CWS Button, hand-flying the aircraft to attain a new Vertical Speed Reference, then releasing the CWS Button Vertical Speed Mode Active Selected Altitude Capture Mode Armed Selected Altitude Vertical Speed Reference Vertical Speed Reference Bug Command Bars Indicate Climb to Attain Vertical Speed Reference Figure 7-10 Vertical Speed Hold Mode 508 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM FLIGHT LEVEL CHANGE MODE (FLC) NOTE: The Selected Altitude should be set before selecting Flight Level Change Mode. Flight Level Change Mode is selected by pressing the FLC Key. This mode acquires and maintains the Airspeed Reference (in IAS or Mach) while climbing or descending to the Selected Altitude (shown above the Altimeter). When Flight Level Change Mode is active, the flight director continuously monitors Selected Altitude, airspeed, Mach, and altitude. The Airspeed Reference is set to the current airspeed upon mode activation. Flight Level Change Mode is indicated by a green ‘FLC’ annunciation in the AFCS Status Box. The Airspeed Reference is displayed directly above the Airspeed Indicator, along with a cyan Airspeed Reference Bug corresponding to the Airspeed Reference along the tape. Engine power must be adjusted to allow the autopilot to fly the aircraft at a pitch attitude corresponding to the desired flight profile (climb or descent) while maintaining the Airspeed Reference. The flight director maintains the current altitude until either engine power or the Airspeed Reference are adjusted and does not allow the aircraft to climb or descend away from the Selected Altitude. Flight Level Change Mode Active Selected Altitude Capture Mode Armed Airspeed Reference Airspeed Reference Bug Command Bars Indicate Climb to Attain Selected Altitude Figure 7-11 Flight Level Change Mode (IAS) 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 509 AUTOMATIC FLIGHT CONTROL SYSTEM CHANGING THE AIRSPEED REFERENCE (FLC MODE) The Airspeed Reference (shown above the Airspeed Indicator) may be adjusted by: • Using the SPD SEL Knob • Pressing the CWS Button, hand-flying the aircraft to attain a new Airspeed Reference, then releasing the CWS Button During climb, the Airspeed Reference units automatically change from IAS to Mach when either the altitude or the airspeed listed in Table 7-3 are attained. For descent, the units switch back at the specified altitude or airspeed. The system determines aircraft climb or descent by the relationship between the current and Selected altitudes. Airspeed Reference Units Default Units Change To: Climb IAS Mach Descent Mach IAS Unit Type Changes At: Altitude Airspeed > 31,500 ft > M 0.55 < 30,500 ft < 250 kt Table 7-3 FLC Mode Unit Changes Airspeed Reference units can be manually toggled between IAS and Mach units by pressing the SPD SEL Knob. When the FLC Airspeed Reference is displayed in Mach, the Airspeed Reference Bug is displayed on the Airspeed Indicator at the IAS corresponding to the selected Mach target speed and the current Mach number is shown below the Airspeed Indicator. Flight Level Change Mode Active Selected Altitude Capture Mode Armed Airspeed Reference (Mach) Airspeed Reference Bug Command Bars Indicate Climb to attain Selected Altitude Figure 7-12 Flight Level Change Mode (Mach) The Airspeed Reference Bug can be set at all times (to be used as a visual reference) except when CSC is engaged. In CSC mode the Airspeed Reference Bug is fixed and set at the airspeed existing at the time of CSC engagement. While the bug can be set during these modes it is only being controlled when in FLC mode, when CSC is engaged, etc. 510 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM VERTICAL NAVIGATION MODES (VPTH, ALTV) NOTE: VNV is disabled when parallel track or Dead Reckoning Mode is active. Refer to the flight Management Section for more information on VNV flight plans. NOTE: The Selected Altitude takes precedence over any other vertical constraints. Vertical Navigation (VNV) flight control is available for enroute/terminal cruise and descent operations when VNV flight planning is available. Conditions for availability include, but are not limited to: • The selected navigation source is GPS. • A VNV flight plan (with at least one altitude-constrained waypoint) or direct-to (with vertical constraint) is active. • VNV is enabled (VNV ENBL Softkey pressed on the MFD). • Crosstrack error is valid and within certain limits. • Desired/actual track are valid or track angle error is within certain limits. • The VNV Target Altitude of the active waypoint is no more than 250 ft above the current aircraft altitude. • Parallel track is not active. The flight director may be armed for VNV at any time, but no target altitudes are captured during a climb. The Command Bars provide vertical profile guidance based on specified altitudes (entered manually or loaded from the database) at waypoints in the active flight plan or direct-to (with vertical constraint). The appropriate VNV flight control modes are sequenced by the flight director to follow the path defined by the vertical profile. Upon reaching the last waypoint in the VNV flight plan, the flight director transitions to Altitude Hold Mode and cancels any armed VNV modes. VERTICAL PATH TRACKING MODE (VPTH) NOTE: If another vertical mode key is pressed while Vertical Path Tracking Mode is selected, Vertical Path Tracking Mode reverts to armed. NOTE: Pressing the CWS Button while Vertical Path Tracking Mode is active does not cancel the mode. The autopilot guides the aircraft back to the descent path upon release of the CWS Button. When a vertical profile (VNV flight plan) is active and the VNV Key is pressed, Vertical Path Tracking Mode is armed in preparation for descent path capture. ‘VPTH’ (or ‘/V’ when Glidepath or Glideslope Mode is concurrently armed) is annunciated in white in addition to previously armed modes. If applicable, the appropriate altitude capture mode is armed for capture of the next VNV Target Altitude (ALTV) or the Selected Altitude (ALTS), whichever is greater. Figure 7-13 Vertical Path Tracking Armed Annunciations 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 511 AUTOMATIC FLIGHT CONTROL SYSTEM Prior to descent path interception, the Selected Altitude must be set below the current aircraft altitude by at least 75 feet. For the flight director to transition from Altitude Hold to Vertical Path Tracking Mode, acknowledgment is required within five minutes of descent path interception by: • Pressing the VNV Key • Adjusting the Selected Altitude If acknowledgment is not received within one minute of descent path interception, the white ‘VPTH’ annunciation starts to flash. Flashing continues until acknowledged or the descent path is intercepted. If the descent is not confirmed by the time of interception, Vertical Path Tracking Mode remains armed and the descent is not captured. In conjunction with the “TOD [top of descent] within 1 minute” annunciation in the PFD Navigation Status Box and the “Vertical track” voice message, VNV indications (VNV Target Altitude, vertical deviation, and vertical speed required) appear on the PFDs in magenta (Figure 7-14). Altitude Hold Mode Active Vertical Path Tracking Armed (Flashing Indicates Acknowledgment Required VNV Target Altitude Selected Altitude Required Vertical Speed Bug GPS is Selected Navigation Source Terminal Phase of Flight Vertical Deviation Indicator Figure 7-14 Vertical Path Capture 512 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM When a descent leg is captured (Figure 7-15), Vertical Path Tracking becomes active (magenta ‘VPTH’ annunciation shown) and tracks the descent profile. An altitude capture mode (‘ALTS’ or ‘ALTV’) is armed as appropriate. Vertical Path Tracking Active VNV Target Altitude Capture Armed VNV Target Altitude GPS is Selected Navigation Source Terminal Phase of Flight Command Bars Indicate Descent to Maintain Required Vertical Speed Required Vertical Speed Bug Vertical Deviation Indicator (VDI) Figure 7-15 Vertical Path Tracking Mode If the altimeter barometric setting is adjusted while Vertical Path Tracking is active, the flight director increases/decreases the descent rate by up to 500 fpm to re-establish the aircraft on the descent path (without commanding a climb). Adjusting the altimeter barometric setting creates discontinuities in VNV vertical deviation, moving the descent path. For large adjustments, it may take several minutes for the aircraft to reestablish on the descent path. If the change is made while nearing a waypoint with a VNV Target Altitude, the aircraft may not re-establish on the descent path in time to meet the vertical constraint. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 513 AUTOMATIC FLIGHT CONTROL SYSTEM Automatic Reversion to Pitch Hold Mode Several situations can occur while Vertical Path Tracking Mode is active which cause the flight director to revert to Pitch Hold Mode: • Vertical deviation exceeds 200 feet during an overspeed condition. • Vertical deviation experiences a discontinuity (not due to an altimeter barometric setting adjustment) that both exceeds 200 feet in magnitude and results in the vertical deviation exceeding 200 feet in magnitude. Such discontinuities are usually caused by flight plan changes that affect the vertical profile. • Vertical deviation becomes invalid (the Vertical Deviation Indicator is removed from the PFD). • A display enters Reversionary Mode (this does not apply to an active direct-to with vertical constraint). Unless VNV is disabled, Vertical Path Tracking Mode and the appropriate altitude capture mode become armed following the reversion to Pitch Hold Mode to allow for possible profile recapture. Non-Path Descents Pitch Hold, Vertical Speed, and Flight Level Change modes can also be used to fly non-path descents while VNV flight control is selected. If the VS or FLC Key is pressed while Vertical Path Tracking Mode is selected, Vertical Path Tracking Mode reverts to armed along with the appropriate altitude capture mode to allow profile re-capture. Figure 7-16 Flight Level Change VNV Non-Path Descent To prevent immediate profile re-capture, the following must be satisfied: • At least 10 seconds have passed since the non-path transition was initiated • Vertical deviation from the profile has exceeded 250 feet, but is now less than 200 feet Pressing the VNV Key twice re-arms Vertical Path Tracking for immediate profile re-capture. 514 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM VNV TARGET ALTITUDE CAPTURE MODE (ALTV) VNV Target Altitude Capture is analogous to Selected Altitude Capture Mode and is armed automatically after the VNV Key is pressed and the next VNV Target Altitude is to be intercepted before the Selected Altitude. The annunciation ‘ALTV’ indicates that the VNV Target Altitude is to be captured. VNV Target Altitudes are shown in the active flight plan or direct-to (with vertical constraint), and can be entered manually or loaded from a database (see the Flight Management Section for details). At the same time as “TOD within 1 minute” is annunciated in the Navigation Status Box, the active VNV Target Altitude is displayed above the Vertical Speed Indicator (see Figure 7-14). As the aircraft nears the VNV Target Altitude, the flight director automatically transitions to VNV Target Altitude Capture Mode with Altitude Hold Mode armed. This automatic transition is indicated by the magenta ‘ALTV’ annunciation flashing for up to 5 seconds and the appearance of the white ‘ALT’ annunciation. The active VNV Target Altitude is shown in magenta above the Vertical Speed Indicator. At 50 feet from the VNV Target Altitude, the flight director automatically transitions from VNV Target Altitude Capture to Altitude Hold Mode and tracks the level leg. As Altitude Hold Mode becomes active, the white ‘ALT’ annunciation moves to the active vertical mode field and flashes magenta for 5 seconds to indicate the automatic transition. The flight director automatically arms Vertical Path Tracking, allowing upcoming descent legs to be captured and subsequently tracked. Flash Up to 5 sec, Indicating Automatic Transition Figure 7-17 VNV Altitude Capture Changing the VNV Target Altitude NOTE: Pressing the CWS Button while in VNV Target Altitude Capture Mode does not cancel the mode. Changing the current VNV Target Altitude while VNV Target Altitude Capture Mode is active causes the flight director to revert to Pitch Hold Mode. Vertical Path Tracking and the appropriate altitude capture mode are armed in preparation to capture the new VNV Target Altitude or the Selected Altitude, depending on which altitude is to be intercepted first. VNV target altitudes can be changed while editing the active flight plan (see the Flight Management Section for details). Current Speed Control (if available) Current Speed Control (if available) can be engaged if the the autopilot is engaged and Altitude Hold Mode (ALT) or VNV Target Altitude Capture (ALTV) Mode is active. When the CSC Key is pressed, the Full Authority Digital Engine Control (FADEC) varies engine thrust to maintain the desired Airspeed Reference (green Airspeed Reference Bug), within a certain control range. NOTE: For CSC engagement and disengagement detailed conditions, see the approved Pilot’s Operating Handbook (POH). 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 515 AUTOMATIC FLIGHT CONTROL SYSTEM GLIDEPATH MODE (GP) (SBAS ONLY) NOTE: Pressing the CWS Button while Glidepath Mode is active does not cancel the mode. The autopilot guides the aircraft back to the glidepath upon release of the CWS Button. Glidepath Mode is used to track the SBAS-based glidepath. When Glidepath Mode is armed, ‘GP’ is annunciated in white in the AFCS Status Box. Selecting Glidepath Mode: 1) Ensure a GPS approach is loaded into the active flight plan. The active waypoint must be part of the flight plan (cannot be a direct-to a waypoint not in the flight plan). 2) Ensure that GPS is the selected navigation source (use the CDI Softkey to cycle through navigation sources if necessary). 3) Press the APR Key. NOTE: Some RNAV (GPS) approaches provide a vertical descent angle as an aid in flying a stabilized approach. These approaches are NOT considered Approaches with Vertical Guidance (APV). Approaches that are annunciated on the HSI as LNAV or LNAV+V are considered Nonprecision Approaches (NPA) and are flown to an MDA even though vertical glidepath (GP) information may be provided. WARNING: When flying an LNAV approach (with vertical descent angle) with the autopilot coupled, the aircraft will not level off at the MDA even if the MDA is set in the altitude preselect. Upon reaching the glidepath, the flight director transitions to Glidepath Mode and begins to capture and track the glidepath. Figure 7-18 Glidepath Mode Armed Once the following conditions have been met, the glidepath can be captured (magenta ‘GP’ annunciation): • A GPS approach with vertical guidance (LPV, LNAV/VNAV, LNAV+V) is loaded into the active flight plan • The active waypoint is at or after the final approach fix (FAF) • Vertical deviation is valid • The CDI is at less than full scale deviation • Automatic sequencing of waypoints has not been suspended (no ‘SUSP’ annunciation on the HSI) 516 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM GPS Approach Mode Active GPS is Selected Navigation Source LPV Approach Active Glidepath Mode Active Command Bars Indicate Descent on Glidepath Figure 7-19 Glidepath Mode 190-00728-06 Rev. A Glidepath Indicator Embraer Prodigy® Flight Deck 100 Pilot’s Guide 517 AUTOMATIC FLIGHT CONTROL SYSTEM GLIDESLOPE MODE (GS) NOTE: Pressing the CWS Button while Glideslope Mode is active does not cancel the mode. The autopilot guides the aircraft back to the glideslope upon release of the CWS Button. Glideslope Mode is available for LOC/ILS approaches to capture and track the glideslope. When Glideslope Mode is armed, LOC Approach Mode is armed as the lateral flight director mode. Selecting Glideslope Mode: 1) Ensure a valid localizer frequency is tuned. 2) Ensure that LOC is the selected navigation source (use the CDI Softkey to cycle through navigation sources if necessary). 3) Press the APR Key. Or: 1) Ensure that GPS is the selected navigation source (use the CDI Softkey to cycle through navigation sources if necessary). 2) Ensure a LOC/ILS approach is loaded into the active flight plan. 3) Ensure the corresponding LOC frequency is tuned. 4) Press the APR Key. Figure 7-20 Glideslope Mode Armed Once LOC is the navigation source, the localizer and glideslope can be captured. Upon reaching the glideslope, the flight director transitions to Glideslope Mode and begins to capture and track the glideslope. Active ILS Frequency Tuned NAV2 (localizer) is Selected Navigation Source Approach Mode Active Glideslope Mode Active Command Bars Indicate Descent on Localizer/Glideslope Path Figure 7-21 Glideslope Mode 518 Embraer Prodigy® Flight Deck 100 Pilot’s Guide Glideslope Indicator 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM TAKEOFF (TO) AND GO AROUND (GA) MODES In Go Around and Takeoff modes, the flight director commands a constant set pitch attitude. The TO/GA Switch is used to select both modes. The mode entered by the flight director depends on whether the aircraft is on the ground. Selected Altitude Capture Mode is automatically armed when the aircraft is at least 400 feet below the Selected Altitude at the time Takeoff or Go Around Mode is selected. When Takeoff or Go Around mode is activated, the lateral mode is annunciated as ‘ROL’. Takeoff Mode provides an attitude reference during rotation and takeoff. This mode can be selected only while on the ground by pushing the TO/GA Switch. The flight director Command Bars assume a wings-level, pitch-up attitude. Autopilot engagement while Takeoff Mode is active is inhibited while the aircraft is on the ground. Pressing the TO/GA Switch while in the air activates the flight director in a wings-level, pitch-up attitude, allowing the execution of a missed approach or a go around. Selecting Go Around Mode disengages the autopilot; however, subsequent autopilot engagement is allowed. Attempts to modify the aircraft attitude (i.e., with the CWS Button) result in reversion to Pitch Hold Mode. Autopilot Disconnect Annunciation Flashes Red 5 sec Go Around Mode Active Command Bars Indicate Climb Takeoff Mode Active Figure 7-22 Takeoff and Go Around Modes 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 519 AUTOMATIC FLIGHT CONTROL SYSTEM 7.4 LATERAL MODES The following table relates each Garmin AFCS lateral mode to its respective control and annunciation. Refer to the vertical modes section for information regarding Takeoff and Go Around mode. NOTE: The Garmin AFCS may generate a lower bank angle than the maximum roll command limit in degrees indicated in Table 7-4 by the amount needed to produce a turn rate equal to or less than standard rate. Lateral Mode Description Control Annunciation Holds the current aircraft roll attitude or rolls the wings level, (default) depending on the commanded bank angle Limits the maximum commanded BANK roll angle Key Captures and tracks the Selected HDG Key Heading Roll Hold Maximum Roll Command Limit ROL 30˚ * 15˚ HDG 30˚ Navigation, GPS ** GPS Navigation, VOR Enroute Capture/Track ** Captures and tracks the selected navigation source (GPS, VOR, LOC) Navigation, LOC Capture/Track VOR 30˚ 25˚ Capture 10˚ Track 25˚ Capture 10˚ Track 25˚ Capture 10˚ Track 30˚ 25˚ Capture 10˚ Track 25˚ Capture 10˚ Track Low Bank Heading Select ** NAV Key (No Glideslope) Navigation, Backcourse Arm/Capture/Track Captures and tracks a localizer signal for backcourse approaches LOC BC Approach, GPS GPS Approach, VOR Capture/Track Approach, LOC Capture/Track (Glideslope Mode automatically armed) Captures and tracks the selected navigation source (GPS, VOR, LOC) APR Key VAPP LOC * No annunciation appears in the AFCS Status Box. The acceptable bank angle range is indicated in green along the Roll Scale of the Attitude Indicator. ** The Heading, Navigation GPS and Navigation VOR mode maximum roll command limit will be limited to the Low Bank mode value if it is engaged. Table 7-4 Flight Director Lateral Modes The CWS Button does not change lateral references for Heading Select, Navigation, Backcourse, or Approach Mode. The autopilot guides the aircraft back to the Selected Heading/Course upon release of the CWS Button. 520 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM ROLL HOLD MODE (ROL) NOTE: If Roll Hold Mode is activated as a result of a mode reversion, the flight director rolls wings level. When the flight director is activated or switched, Roll Hold Mode is selected by default. This mode is annunciated as ‘ROL’ in the AFCS Status Box. The current aircraft bank angle is held, subject to the bank angle condition. Figure 7-23 Roll Hold Mode Annunciation Bank Angle < 6° 6 to 30° > 30° Flight Director Response Rolls wings level Maintains current aircraft roll attitude Limits bank to 30° Table 7-5 Roll Hold Mode Responses CHANGING THE ROLL REFERENCE The roll reference can be changed by pressing the CWS Button, establishing the desired bank angle, then releasing the CWS Button. LOW BANK MODE When in Low Bank Mode, the flight director limits the maximum commanded roll angle to 15°. Low bank arc limits are displayed in green along the Roll Scale. Low Bank Mode can be manually selected/deselected by pressing the BANK Key while in Heading Select or Navigation Modes (GPS and VOR). Low Bank Arc Figure 7-24 Low Bank Mode Limits 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 521 AUTOMATIC FLIGHT CONTROL SYSTEM HEADING SELECT MODE (HDG) Heading Select Mode is activated by pressing the HDG Key. Heading Select Mode acquires and maintains the Selected Heading. The Selected Heading is shown by a light blue bug on the HSI and in the box to the upper left of the HSI. CHANGING THE SELECTED HEADING NOTE: Pressing the HDG SEL Knob synchronizes the Selected Heading to the current heading. The Selected Heading is adjusted using the HDG SEL Knob. Pressing the CWS Button and hand-flying the aircraft does not change the Selected Heading. The autopilot guides the aircraft back to the Selected Heading upon release of the CWS Button. Turns are commanded in the same direction as Selected Heading Bug movement, even if the bug is turned more than 180° from the present heading (e.g., a 270° turn to the right). However, Selected Heading changes of more than 330° at a time result in turn reversals. Heading Select Mode Active Selected Heading Selected Heading Bug Command Bars Track Selected Heading Figure 7-25 Heading Select Mode 522 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM NAVIGATION MODES (GPS, VOR, LOC, BC) NOTE: The selected navigation receiver must have a valid VOR or LOC signal or active GPS course for the flight director to enter Navigation Mode. Pressing the NAV Key selects Navigation Mode. Navigation Mode acquires and tracks the selected navigation source (GPS, VOR, LOC). The flight director follows GPS roll steering commands when GPS is the selected navigation source. When the navigation source is VOR or LOC, the flight director creates roll steering commands from the Selected Course and deviation. Navigation Mode can also be used to fly non-precision GPS and LOC approaches where vertical guidance is not required. Backcourse Mode captures and tracks a localizer signal in the backcourse direction. The mode may be selected by pressing the NAV Key. When making a backcourse approach, set the Selected Course to the localizer front course. The flight director creates roll steering commands from the Selected Course and deviation. If the Course Deviation Indicator (CDI) shows greater than one dot when the NAV Key is pressed, the selected mode is armed. If the CDI is less than one dot, Navigation Mode is automatically captured when the NAV Key is pressed. The armed annunciation appears in white to the left of the active lateral mode. Figure 7-26 GPS Navigation Mode Armed When the CDI has automatically switched from GPS to LOC during a LOC/ILS approach, GPS Navigation Mode remains active, providing GPS steering guidance until the localizer signal is captured. LOC Navigation Mode is armed automatically when the navigation source switch takes place if the APR Key is not pressed prior to the automatic source switch. If Navigation Mode is active and either of the following occur, the flight director reverts to Roll Hold Mode (wings rolled level): • Different VOR tuned while in VOR Navigation Mode (VOR Navigation Mode reverts to armed) • Navigation source manually switched (with the CDI Softkey) • During a LOC/ILS approach, the FAF crossed while in GPS Navigation Mode after the automatic navigation source switch from GPS to LOC CHANGING THE SELECTED COURSE If the navigation source is VOR or localizer or OBS Mode has been enabled when using GPS, the Selected Course is controlled using the CRS Knob corresponding to the selected flight director (CRS1 for the pilot side, CRS2 for the copilot side). Pressing the CWS Button and hand-flying the aircraft does not change the Selected Course while in Navigation Mode. The autopilot guides the aircraft back to the Selected Course (or GPS flight plan) when the CWS Button is released. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 523 AUTOMATIC FLIGHT CONTROL SYSTEM GPS Navigation Mode Active GPS is Selected Navigation Source Command Bars Indicate Left Turn to Track GPS Course Figure 7-27 Navigation Mode Backcourse Mode Active LOC2 is Selected Navigation Source 524 Command Bars Hold Pitch Attitude Figure 7-28 Backcourse Mode Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM APPROACH MODES (GPS, VAPP, LOC) NOTE: The selected navigation receiver must have a valid VOR or LOC signal or active GPS course for the flight director to enter Approach Mode. Approach Mode is activated when the APR Key is pressed. Approach Mode acquires and tracks the selected navigation source (GPS, VOR, or LOC), depending on loaded approach. This mode uses the selected navigation receiver deviation and desired course inputs to fly the approach. Pressing the APR Key when the CDI is greater than one dot arms the selected approach mode (annunciated in white to the left of the active lateral mode). If the CDI is less than one dot, the LOC is automatically captured when the APR Key is pressed. VOR Approach Mode (VAPP) provides greater sensitivity for signal tracking than VOR Navigation Mode. Selecting VOR Approach Mode: 1) Ensure a valid VOR frequency is tuned. 2) Ensure that VOR is the selected navigation source (use the CDI Softkey to cycle through navigation sources if necessary). 3) Press the APR Key. When GPS Approach Mode is armed, Glidepath Mode is also armed. Selecting GPS Approach Mode: 1) Ensure a GPS approach is loaded into the active flight plan. The active waypoint must be part of the flight plan (cannot be a direct-to a waypoint not in the flight plan). 2) Ensure that GPS is the selected navigation source (use the CDI Softkey to cycle through navigation sources if necessary). 3) Press the APR Key. Figure 7-29 GPS Approach Mode Armed 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 525 AUTOMATIC FLIGHT CONTROL SYSTEM LOC Approach Mode allows the autopilot to fly a LOC/ILS approach with a glideslope. When LOC Approach Mode is armed, Glideslope Mode is also armed automatically. LOC captures are inhibited if the difference between aircraft heading and localizer course exceeds 105°. Selecting LOC Approach Mode: 1) Ensure a valid localizer frequency is tuned. 2) Ensure that LOC is the selected navigation source (use the CDI Softkey to cycle through navigation sources if necessary). 3) Press the APR Key. Or: 1) Ensure that GPS is the selected navigation source (use the CDI Softkey to cycle through navigation sources if necessary). 2) Ensure a LOC/ILS approach is loaded into the active flight plan. 3) Ensure the corresponding LOC frequency is tuned. 4) Press the APR Key. If the following occurs, the flight director reverts to Roll Hold Mode (wings rolled level): • Vectors-to-Final is activated • Navigation source is manually switched • During a LOC/ILS approach, GPS Navigation Mode is active and the FAF is crossed after the automatic navigation source switch from GPS to LOC CHANGING THE SELECTED COURSE If the navigation source is VOR or localizer or OBS Mode has been enabled when using GPS, the Selected Course is controlled using the CRS Knob corresponding to the selected flight director (CRS1 for the pilot side, CRS2 for the copilot side). Pressing the CWS Button and hand-flying the aircraft does not change the Selected Course while in Approach Mode. The autopilot guides the aircraft back to the Selected Course (or GPS flight plan) when the CWS Button is released. INTERCEPTING AND FLYING A DME ARC The AFCS will intercept and track a DME arc that is part of the active flight plan provided that GPS Navigation Mode is engaged, GPS is the active navigation source on the CDI, and the DME arc segment is the active flight plan leg. It is important to note that automatic navigation of DME arcs is based on GPS. Thus, even if the APR key is pressed and LOC or VOR Approach Mode is armed prior to reaching the Initial Approach Fix (IAF), Approach Mode will not activate until the arc segment is completed. If the pilot decides to intercept the arc at a location other than the published IAF (i.e. ATC provides vectors to intercept the arc) and subsequently selects Heading Mode or Roll Mode, the AFCS will not automatically intercept or track the arc unless the pilot activates the arc leg of the flight plan and arms GPS Navigation Mode. The AFCS will not intercept and fly a DME arc before reaching an IAF that defines the beginning of the arc segment. Likewise, if at any point while established on the DME arc the pilot deselects GPS Navigation Mode, the AFCS will no longer track the arc. 526 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM 7.5 AUTOPILOT AND YAW DAMPER OPERATION NOTE: Refer to the Airplane Flight Manual (AFM) for specific instructions regarding emergency procedures. The autopilot and yaw damper operate the flight control surface servos to provide automatic flight control. The autopilot controls the aircraft pitch and roll attitudes following commands received from the flight director. Pitch autotrim provides trim commands to the pitch trim actuator to relieve any sustained effort required by the pitch servo. The yaw damper reduces Dutch roll tendencies and coordinates turns. It can operate independently of the autopilot and may be used during normal hand-flight maneuvers. Yaw rate commands are limited by the yaw damper. FLIGHT CONTROL Pitch and roll commands are provided to the servos based on the active flight director modes. Yaw damping is provided by the yaw servo. Servo motor control limits the maximum servo speed and torque. The servo gearboxes are equipped with slip-clutches that allow the servos to be overridden in case of an emergency (i.e., a failure event when the servo motor and slip clutch remain abnormally engaged). PITCH AXIS AND TRIM The autopilot pitch axis uses pitch rate to stabilize the aircraft pitch attitude during upsets and flight director maneuvers. Flight director pitch commands are rate- and attitude-limited, combined with pitch damper control, and sent to the pitch servo motor. When the autopilot is engaged, the automatic pitch trim (APT) function commands the pitch trim actuator to reduce the average pitch servo effort. Manual electric pitch trim (MEPT) functionality is available at any time via the pilot and copilot MEPT Switches. Manual trim commands are generated only when both halves of the MEPT Switch are operated simultaneously. Operating the MEPT Switches when the autopilot is engaged will cause the autopilot to disconnect. Trim speeds are scheduled with airspeed to provide more consistent response. ROLL AXIS The autopilot roll axis uses roll rate to stabilize aircraft roll attitude during upsets and flight director maneuvers. The flight director roll commands are rate- and attitude-limited, combined with roll damper control, and sent to the roll servo motor. YAW AXIS The yaw damper uses yaw rate and roll attitude to dampen the aircraft’s natural Dutch roll response. It also uses lateral acceleration to coordinate turns. Yaw damper operation is independent of autopilot engagement. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 527 AUTOMATIC FLIGHT CONTROL SYSTEM ENGAGING THE AUTOPILOT AND YAW DAMPER NOTE: Autopilot engagement/disengagement is not equivalent to servo engagement/disengagement. Use the CWS Button to disengage the pitch and roll servos while the autopilot remains active. When the AP Key is pressed, the autopilot, yaw damper, and flight director (if not already active) are activated. The flight director engages in Pitch and Roll Hold Modes when initially activated. When the YD Key is pressed, the system engages the yaw damper independently of the autopilot. Autopilot and yaw damper status are displayed in the center of the AFCS Status Box. Engagement is indicated by green ‘AP’ and ‘YD’ annunciations, respectively. Autopilot Engaged Yaw Damper Engaged Figure 7-30 Autopilot and Yaw Damper Engaged CONTROL WHEEL STEERING During autopilot operation, the aircraft may be hand-flown without disengaging the autopilot. Pressing and holding the CWS Button disengages the pitch and roll servos from the flight control surfaces and allows the aircraft to be hand-flown. At the same time, the flight director is synchronized to the aircraft attitude during the maneuver. Pitch trim operation is interrupted during CWS activity; yaw damper engagement is unaffected. The ‘AP’ annunciation is temporarily replaced by ‘CWS’ in white for the duration of CWS maneuvers. Control Wheel Steering Figure 7-31 CWS Annunciation In most scenarios, releasing the CWS Button re-engages the autopilot with a new reference. Refer to flight director mode descriptions for specific CWS behavior in each mode. 528 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM DISENGAGING THE AUTOPILOT AND YAW DAMPER NOTE: Pressing the AP Key does not disengage the yaw damper. Manual autopilot disengagement is indicated by a five-second flashing red ‘AP’ annunciation and an autopilot disconnect aural alert, “Autopilot”. The autopilot is manually disengaged by pushing the AP Key on the AFCS Control Unit, the TO/GA Switch, or the AP DISC Switch (also disengages the yaw damper, if engaged). Pressing the YD Key disengages the yaw damper independently of the autopilot. The ‘YD’ annunciation is removed upon disengagement. After manual disengagement, the autopilot disconnect aural alert and flashing ‘AP’ annunciation may be cancelled by pushing the AP DISC Switch. Figure 7-32 Manual Autopilot Disengagement Automatic autopilot disengagement is indicated by a flashing red and white ‘AP’ annunciation and the autopilot disconnect aural alert, which continue until acknowledged by pushing the AP DISC Switch. Automatic autopilot disengagement occurs due to: • System failure • Invalid sensor data • Inability to compute default flight director modes (FD also disengages automatically) • Stall warning (YD also disengages) • Backup pitch trim channel selection • Pushing the MEPT switches Automatic yaw damper disengagement is indicated by a five-second flashing yellow ‘YD’ annunciation. The yaw damper automatically disengages when autopilot disengagement is caused by failure in a parameter also affecting the yaw damper. This means the yaw damper can remain operational in some cases where the autopilot automatically disengages. A localized failure in the yaw damper system or invalid sensor data also cause yaw damper disengagement. Figure 7-33 Automatic Autopilot and Yaw Damper Disengagement 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 529 AUTOMATIC FLIGHT CONTROL SYSTEM 7.6 EXAMPLE FLIGHT PLAN NOTE: The following example flight plan and diagrams (not to be used for navigation) in this section are for instructional purposes only and should be considered not current. Numbered portions of accompanying diagrams correspond to numbered procedure steps. This scenario-based set of procedures (based on the example flight plan found in the Flight Management Section) shows various Garmin AFCS modes used during a flight. In this scenario, the aircraft departs Charles B. Wheeler Downtown Airport (KMKC), enroute to Colorado Springs Airport (KCOS). After departure, the aircraft climbs to 12,000 ft and airway V4 is intercepted, following ATC vectors. Airway V4 is flown to Salina VOR (SLN) using VOR navigation, then airway V244 is flown using a GPS flight plan. The ILS approach for runway 35L and LPV (WAAS) approach for runway 35R are shown and a missed approach is executed. 0 33 3 27 30 27 30 24 24 21 27 24 27 15 12 21 18 15 18 9 24 21 12 6 Lamar VOR (LAA) Topeka VOR (TOP) 12 Hays VOR (HYS) 9 V 244 Salina VOR (SLN) 9 3 V4 18 V 244 9 6 0 33 15 6 KCOS KMKC 30 6 3 3 30 33 0 33 0 12 21 15 18 Figure 7-34 Flight Plan Overview 530 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM DEPARTURE Climbing to the Selected Altitude and flying an assigned heading: 1) Before takeoff: a) Use the ALT SEL Knob to set the Selected Altitude to 12,000 feet. b) Push the TO/GA Switch to activate Takeoff Mode. The flight director Command Bars establish a pitch up attitude to follow. c) Press the AP Key to engage the autopilot in a climb, holding the pitch angle commanded in Takeoff Mode and wings level. 2) In this example, Vertical Speed Mode is used to capture the Selected Altitude (Pitch Hold, Vertical Speed, or Flight Level Change Mode may be used). a) Press the VS Key to activate Vertical Speed and Roll Hold modes and arm Selected Altitude Capture Mode. The Vertical Speed Reference may be adjusted after Vertical Speed Mode is selected using the UP/DN Wheel or pushing the CWS Button while hand-flying the aircraft to establish a new Vertical Speed Reference. 3) Use the HDG SEL Knob to set the Selected Heading, complying with ATC vectors to intercept Airway V4. Press the HDG Key to activate Heading Select Mode while the autopilot is engaged in the climb. The autopilot follows the Selected Heading Bug on the HSI and turns the aircraft to the desired heading. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 531 AUTOMATIC FLIGHT CONTROL SYSTEM 4) As the aircraft nears the Selected Altitude, the flight director transitions to Selected Altitude Capture Mode, indicated by the green ‘ALTS’ annunciation flashing for up to 5 seconds. At 50 feet from the Selected Altitude, the green ‘ALT’ annunciation flashes for up to 5 seconds; the autopilot transitions to Altitude Hold Mode and levels the aircraft. HD GM od e TO M o de 3 Selected Altitude of 12,000 MSL ALT Mode 4 KMKC 1 2 VS e Mod ode M TO Figure 7-35 Departure 532 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM INTERCEPTING A VOR RADIAL During climb-out, the autopilot continues to fly the aircraft in Heading Select Mode. Airway V4 to Salina VOR (SLN) should now be intercepted. Since the enroute flight plan waypoints correspond to VORs, flight director Navigation Mode using either VOR or GPS as the navigation source may be used. In this scenario, VOR Navigation Mode is used for navigation to the first VOR waypoint in the flight plan. Intercepting a VOR radial: 1) Arm VOR Navigation Mode: a) Tune the VOR frequency. b) Press the CDI Softkey to set the navigation source to VOR. c) Use the CRS1 or CRS2 Knob to set the Selected Course to the desired value, 255°. Note that at this point, the flight director is still in Heading Select Mode and the autopilot continues to fly the Selected Heading, 290°. d) Press the NAV Key. This arms VOR Navigation Mode and the white ‘VOR’ annunciation appears to the left of the active lateral mode. 2) As the aircraft nears the Selected Course, the flight director transitions from Heading Select to VOR Navigation Mode and the ‘VOR’ annunciation flashes green. The autopilot begins turning to intercept the Selected Course. 3) The autopilot continues the turn until the aircraft is established on the Selected Course. 0 33 3 30 Hd 29 g 0o V4 6 27 3 9 o 255 Salina VOR (SLN) 24 VO R NA V Mo de 2 HD G 12 M od e, VO R Ar m ed 15 1 21 18 Figure 7-36 Intercepting a VOR Radial 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 533 AUTOMATIC FLIGHT CONTROL SYSTEM FLYING A FLIGHT PLAN/GPS COURSE NOTE: Changing the navigation source cancels the Navigation Mode and causes the flight director to revert back to Roll Hold Mode (wings rolled level). As the aircraft closes on Salina VOR, GPS is used to navigate the next leg, airway V244. The aircraft is currently tracking inbound on Airway V4. Flying a GPS flight plan: 1) Transition from VOR to GPS Navigation Mode: a) Press the CDI Softkey until GPS is the selected navigation source. b) Press the NAV Key to activate GPS Navigation Mode. The autopilot steers the aircraft toward the active flight plan leg. 2) Following the flight plan, the autopilot continues to steer the aircraft under GPS guidance. Note that in GPS Navigation Mode, course changes defined by the flight plan are automatically made without pilot action required. 0 33 33 3 30 0 V4 6 3 o 075 30 e V Mod PS NA 6 27 G 2 12 21 18 12 15 24 9 Hays VOR (HYS) Salina VOR (SLN) V 244 1 24 27 076 Mode 9 o 260 o AV VOR N 15 21 18 Figure 7-37 Transition to GPS Flight Plan 534 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM DESCENT While flying the arrival procedure, the aircraft is cleared for descent in preparation for the approach to KCOS. Three methods are presented for descent: • Flight Level Change descent – Flight Level Change Mode can be used to descend to the Selected Altitude at a constant airspeed. This descent method does not account for flight plan waypoint altitude constraints. • Vertical Path Tracking descent – Vertical Path Tracking Mode is used to follow the vertical descent path defined in the GPS flight plan. Altitude constraints correspond to waypoints in the flight plan. Before VNV flight control can provide vertical profile guidance, a VNV flight plan must be entered and enabled. • Non-path descent in a VNV scenario – A VNV flight plan is entered and enabled however, Pitch Hold, Vertical Speed, or Flight Level Change Mode can be used to descend to the VNV Target Altitude prior to reaching the planned TOD. Flight Level Change Mode is used in the example. Flight Level Change descent: 1) Select Flight Level Change Mode: a) Using the ALT SEL Knob, set the Selected Altitude to 10,000 feet. b) Press the FLC Key to activate Flight Level Change Mode. The annunciation ‘FLC’ appears in the AFCS Status Box and the Airspeed Reference (above the Airspeed Indicator) defaults to the current aircraft airspeed. Selected Altitude Capture Mode is armed automatically. c) If desired press the SPD SEL Knob to change the Airspeed Reference units to Mach. 2) Use the SPD SEL Knob or push the CWS Button while hand-flying the aircraft to adjust the commanded airspeed while maintaining the same power, or reduce power to allow descent in Flight Level Change Mode while the autopilot maintains the current airspeed. 3) As the aircraft nears the Selected Altitude, the flight director transitions to Selected Altitude Capture Mode, indicated by the green ‘ALTS’ annunciation flashing for up to 5 seconds. The green ‘ALT’ annunciation flashes for up to 5 seconds upon reaching 50 feet from the Selected Altitude; the autopilot transitions to Altitude Hold Mode and levels the aircraft. 1 Cruise Altitude of 12,000 MSL ALT Mode 2 FLC Mod e 3 Selected Altitude of 10,000 MSL ALT Mode Figure 7-38 FLC Descent 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 535 AUTOMATIC FLIGHT CONTROL SYSTEM Vertical Path Tracking descent to VNV Target Altitude: 1) Select VNV flight control: a) Press the VNV Key to arm Vertical Path Tracking Mode. The white annunciation ‘VPTH’ appears. b) Using the ALT SEL Knob, set the Selected Altitude below the flight plan’s VNV Target Altitude of 10,000 feet. If the Selected Altitude is not at least 75 ft below the VNV Target Altitude, the flight director commands descent to the Selected Altitude rather than the VNV Target Altitude once Vertical Path Tracking Mode becomes active (ALTS is armed rather than ALTV). c) If Vertical Path Tracking Mode is armed more than 5 minutes prior to descent path capture, acknowledgment is required for the flight director to transition from Altitude Hold to Vertical Path Tracking Mode. To proceed with descent path capture if the white ‘VPTH’ annunciation begins flashing, do one of the following • Press the VNV Key • Turn the ALT SEL Knob to adjust the Selected Altitude If the descent is not confirmed by the time of interception, Vertical Path Tracking Mode remains armed and the descent is not captured. 2) When the top of descent (TOD) is reached, the flight director transitions to Vertical Path Tracking Mode and begins the descent to the VNV Target Altitude. Intention to capture the VNV Target Altitude is indicated by the white ‘ALTV’ annunciation. 3) As the aircraft nears the VNV Target Altitude, the flight director transitions to VNV Target Altitude Capture Mode, indicated by the magenta ‘ALTV’ annunciation flashing for up to 5 seconds. The magenta ‘ALT’ annunciation flashes for up to 5 seconds upon reaching 50 feet from the VNV Target Altitude; the autopilot transitions to Altitude Hold Mode and levels the aircraft at the vertical waypoint. 1 ALT Mode TOD Cruise Altitude of 12,000 MSL 2 VPT HM ode 3 BOD VNAV Target Altitude of 10,000 MSL ALT Mode Selected Altitude (set below VNAV Target Altitude) Along-track Offset, 3 nm before OPSHN 3 nm Figure 7-39 VPTH Descent 536 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM Non-path descent using Flight Level Change Mode: 1) Using Flight Level Change Mode, command a non-path descent to an intermediate altitude above the next VNV flight plan altitude: a) Using the ALT SEL Knob, set the Selected Altitude below the current aircraft altitude to an altitude (in this case, 9,400 feet) at which to level off between VNV flight plan altitudes. b) Press the FLC Key before the planned TOD during an altitude hold while VPTH is armed. The Airspeed Reference defaults to the current aircraft airspeed. Vertical Path Tracking and Selected Altitude Capture Mode are armed automatically. 2) Reduce power to allow descent in Flight Level Change Mode. The autopilot maintains the Airspeed Reference. 3) As the aircraft nears the Selected Altitude, the flight director transitions to Selected Altitude Capture Mode, indicated by the green ‘ALTS’ annunciation flashing for up to 5 seconds. The green ‘ALT’ annunciation flashes for up to 5 seconds upon reaching 50 feet from the Selected Altitude; the autopilot transitions to Altitude Hold Mode and levels the aircraft. After leveling off reset Selected Altitude at or below 9,000 ft. 4) When the next TOD is reached, Vertical Path Tracking becomes active (may require acknowledgment to allow descent path capture). 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 537 AUTOMATIC FLIGHT CONTROL SYSTEM 5) As the aircraft nears the VNV Target Altitude, the flight director transitions to VNV Target Altitude Capture Mode, indicated by the magenta ‘ALTV’ annunciation flashing for up to 5 seconds. The magenta ‘ALT’ annunciation flashes for up to 5 seconds upon reaching 50 feet from the VNV Target Altitude; the autopilot transitions to Altitude Hold Mode and levels the aircraft at the vertical waypoint. VP TH M od e Planned TOD 2 BOD ALT Mode 1 FL C Pla nn M od e Selected Altitude of 9,400 MSL VNAV Target Altitude of 10,000 MSL 3 ed De sce nt Pa th ALT Mode TOD 4 VP TH VNAV Target Altitude of 9,000 MSL Mo de 5 BOD ALT Mode Selected Altitude 3 nm OPSHN HABUK Figure 7-40 Non-path Descent 538 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM APPROACH NOTE: If an approach contains a DME arc, the arc must be flown in Navigation Mode with the Garmin AFCS. When receiving vectors from ATC, Navigation Mode must be selected prior to intercepting the ARC. Flying an ILS approach: 1) Transition from GPS Navigation Mode to Heading Select Mode. a) Select the Runway 35L ILS approach for KCOS and select ‘VECTORS’ for the transition. Load and activate the approach into the flight plan. b) Use the HDG SEL Knob to set the Selected Heading after getting vectors from ATC. c) Press the HDG Key. The autopilot turns the aircraft to the desired heading. d) Use Heading Select Mode to comply with ATC vectors as requested. 2) Arm LOC Approach and Glideslope modes. a) Ensure the appropriate localizer frequency is tuned. b) Press the APR Key when cleared for approach to arm Approach and Glideslope modes. ‘LOC’ and ‘GS’ appear in white as armed mode annunciations. c) The navigation source automatically switches to LOC. After this switch occurs, the localizer signal can be captured and the flight director determines when to begin the turn to intercept the final approach course. The flight director now provides guidance to the missed approach point. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 539 AUTOMATIC FLIGHT CONTROL SYSTEM 3) There are two options available at this point, as the autopilot flies the ILS approach: • Push the AP DISC Switch at the decision height and land the aircraft. • Use the TO/GA Switch to execute a missed approach. KCOS LOC APR/ GS Mode 3 PETEY 2 G HD e od M PYNON 1 GPS NAV Mode Figure 7-41 ILS Approach to KCOS 540 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM Flying a RNAV GPS approach with vertical guidance: 1) Arm flight director modes for a RNAV GPS approach with vertical guidance: a) Make sure the navigation source is set to GPS (use CDI Softkey to change navigation source). b) Select the Runway 35R LPV approach for KCOS. Load and activate approach into the flight plan. 2) Press the APR Key once clearance for approach has been received. GPS Approach Mode is activated and Glidepath Mode is armed. 3) Once the glidepath is captured, Glidepath Mode becomes active. The flight director now provides guidance to the missed approach point. 4) There are two options available at this point, as the autopilot flies the approach: • Push the AP DISC Switch at the decision height and land the aircraft. • Use the TO/GA Switch to execute a missed approach. KCOS 4 3 GPS APR/ GP Mode CEGIX 2 FALUR HABUK PYNON 1 GPS NAV Mode Figure 7-42 LPV Approach to KCOS 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 541 AUTOMATIC FLIGHT CONTROL SYSTEM GO AROUND/MISSED APPROACH NOTE: As a result of calculations performed by the system while flying the holding pattern, the display may re-size automatically and the aircraft may not precisely track the holding pattern as depicted on the PFD and MFD. Flying a missed approach: 1) Push the TO/GA Switch at the decision height and apply go around power to execute a missed approach. The flight director Command Bars establish a nose-up climb to follow. If flying an ILS or LOC approach, the CDI also switches to GPS as the navigation source. Note that when the TO/GA Switch is pushed, the missed approach is activated and the autopilot disconnects, indicated by the ‘AP’ annunciation flashing red for 5 seconds. Flashes 5 sec 2) Start the climb to the prescribed altitude in the published Missed Approach Procedure (in this case, 10,000 ft). a) Press the AP Key to re-engage the autopilot. b) Press the NAV Key to have the autopilot fly to the hold. 3) Use the ALT SEL Knob to set a Selected Altitude to hold. To hold the current airspeed during the climb, press the FLC Key. As the aircraft nears the Selected Altitude, the flight director transitions to Selected Altitude Capture Mode, indicated by the green ‘ALTS’ annunciation flashing for up to 5 seconds. The green ‘ALT’ annunciation flashes for up to 5 seconds upon reaching 50 feet from the Selected Altitude; the autopilot transitions to Altitude Hold Mode and levels the aircraft. 542 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM 4) The autopilot flies the holding pattern after the missed approach is activated. Annunciations are displayed in the Navigation Status Box, above the AFCS Status Box. 4 MOGAL GPS NAV Mode 3 2 GA Mode KCOS 1 Figure 7-43 Go Around/Missed Approach 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 543 AUTOMATIC FLIGHT CONTROL SYSTEM 7.7 AFCS ANNUNCIATIONS AND ALERTS AFCS CAS MESSAGES Crew Alerting System (CAS) messages related to the AFCS are listed in Table 7-6. CAS messages appear on the PFDs in the window to the right of the Altimeter (see Figure 7-44). Refer to the EAS Section for details. CAS Message AP FAIL Description Loss of AP function AUTO PTRIM FAIL Auto pitch trim failure; other pitch trim functions still available AP PITCH MISTRIM Airplane mistrimmed in pitch axis when AP is engaged AP ROLL MISTRIM Airplane mistrimmed in roll axis when AP is engaged YD FAIL YD MISTRIM Loss of yaw damper function Airplane mistrimmed in yaw axis when YD is engaged PTRIM NML FAIL Loss of normally-operating pitch trim actuator PTRIM BKP FAIL Loss of backup pitch trim actuator PTRIM DISCONNECT Pitch trim disconnected PTRIM SW1 FAIL Failure of pilot pitch trim switch PTRIM SW2 FAIL Failure of copilot pitch trim switch Table 7-6 AFCS CAS Messages CAS Window CAS Scrolling Softkey (Softkey Becomes Disabled When Less Than 14 Messages are Displayed) Figure 7-44 CAS Display 544 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A AUTOMATIC FLIGHT CONTROL SYSTEM AFCS VOICE ALERTS The voice alerts listed in Table 7-7 relate to the AFCS; for a complete list of voice alerts, see Appendix A. Voice Alert “Autopilot” Description Warning – Autopilot is disengaged Single alert for manual AP disengagement Continuous alert for automatic AP disengagement; cancelled with AP DISC Switch “Flight Director” Single warning – Flight director has reverted to a default mode “Trim, Trim, Trim” Continuous advisory (stops after 6 seconds) – MEPT Switch malfunction “Thrust Thrust” CSC disengages abnormally Table 7-7 AFCS Voice Alerts OVERSPEED PROTECTION While Pitch Hold, Vertical Speed, Flight Level Change, Vertical Path Tracking, or an altitude capture mode is active, airspeed is monitored by the flight director and pitch commands are limited for overspeed protection. Overspeed protection is provided in situations where the flight director cannot acquire and maintain the mode reference for the selected vertical mode without exceeding the certified maximum autopilot airspeed. When an autopilot overspeed condition occurs, a flashing yellow ‘MAXSPD’ annunciation appears above the Airspeed Indicator and the voice alert “High Speed” is generated. Engine power should be reduced and/or the pitch reference adjusted to slow the aircraft. The annunciation disappears when the overspeed condition is resolved. Airspeed Indicator Figure 7-45 Overspeed Annunciation 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 545 AUTOMATIC FLIGHT CONTROL SYSTEM Blank Page 546 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES SECTION 8 ADDITIONAL FEATURES NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts®, it may be necessary to carry another source of charts on-board the aircraft. Additional features of the system include the following: • Synthetic Vision Technology (SVT) • SafeTaxi® diagrams • ChartView and FliteCharts® electronic charts • AOPA or AC-U-KWIK Airport Directory • Satellite telephone and SMS messaging services • Wi-Fi Connections • Maintenance Logs • SiriusXM Satellite Radio entertainment • Scheduler • Electronic Checklists The optional Synthetic Vision Technology (SVT) provides a three-dimensional forward view of terrain features on the PFD. SVT imagery shows the pilot’s view of relevant features in relation to the aircraft attitude, as well as the flight path pertaining to the active flight plan. SafeTaxi diagrams provide detailed taxiway, runway, and ramp information at more than 700 airports in the United States. By decreasing range on an airport that has a SafeTaxi diagram available, a close up view of the airport layout can be seen. The FliteCharts and optional ChartView provide on-board electronic terminal procedures charts. Electronic charts offer the convenience of rapid access to essential information. Either ChartView or FliteCharts may be configured in the system, but not both. The AOPA and AC-U-KWIK Airport Directories offer detailed information for a selected airport, such as available services, hours of operation, and lodging options. Iridium Telephone Services and SMS messaging is an optional subscription service offered through Garmin Connext and Iridium Satellite LLC. Wi-Fi setup allows for the transmission of data recorded by the Maintenance Log feature. The recording of this data is not visible to the pilot and requires no pilot interaction, other than setting up Wi-Fi connections where applicable. The optional SiriusXM Satellite Radio entertainment audio feature of the GDL 69A Data Link Receiver handles more than 170 channels of music, news, and sports. SiriusXM Satellite Radio offers more entertainment choices and longer range coverage than commercial broadcast stations. The Scheduler feature can be used to enter and display short term or long term reminder messages such as Switch fuel tanks, Phase 1 inspection, or Altimeter/Transponder Check in the Messages Window on the PFD. Optional checklists help to quickly find the proper procedure on the ground or during flight. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 547 ADDITIONAL FEATURES 8.1 SYNTHETIC VISION TECHNOLOGY (SVT) WARNING: Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance. SVT is intended as an aid to situational awareness only and may not provide either the accuracy or reliability upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or traffic. The optional Synthetic Vision Technology (SVT) is a visual enhancement to the Prodigy® Flight Deck 100. SVT depicts a forward-looking attitude display of the topography immediately in front of the aircraft. The field of view is 30 degrees to the left and 35 degrees to the right. SVT information is shown on the Primary Flight Display (PFD), or on the Multifunction Display (MFD) in Reversionary Mode (Figure 8‑125). The depicted imagery is derived from the aircraft attitude, heading, GPS three-dimensional position, and a nine arc-second database of terrain, obstacles, and other relevant features. The terrain data resolution of nine arc-seconds, meaning that the terrain elevation contours are stored in squares measuring nine arc-seconds on each side, is required for the operation of SVT. Loss of any of the required data, including temporary loss of the GPS signal, will cause SVT to be disabled until the required data is restored. The SVT terrain display shows land contours (colors are consistent with those of the topographical map display), large water features, towers, and other obstacles over 200’ AGL that are included in the obstacle database. Cultural features on the ground such as roads, highways, railroad tracks, cities, and state boundaries are not displayed even if those features are found on the MFD map. The terrain display also includes a north–south east–west grid with lines oriented with true north and spaced at one arc-minute intervals to assist in orientation relative to the terrain. The Terrain Awareness and Warning System (TAWS) is integrated within SVT to provide visual and auditory alerts to indicate the presence of terrain and obstacle threats relevant to the projected flight path. Terrain alerts are displayed in red and yellow shading on the PFD. The terrain display is intended for situational awareness only. It may not provide the accuracy or fidelity on which to base decisions and plan maneuvers to avoid terrain or obstacles. Navigation must not be predicated solely upon the use of the TAWS terrain or obstacle data displayed by the SVT. The following SVT enhancements appear on the PFD: 548 • Pathways • Airport Signs • Flight Path Marker • Runway Display • Horizon Heading Marks • Terrain Alerting • Traffic Display • Obstacle Alerting Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Figure 8-1 Synthetic Vision Imagery SVT OPERATION SVT is activated from the PFD using the softkeys located along the bottom edge of the display. Pressing the softkeys turns the related function on or off. When SVT is enabled, the pitch scale increments are reduced to 10 degrees up and 7.5 degrees down. SVT functions are displayed on three levels of softkeys. The PFD Softkey leads into the PFD function Softkeys, including synthetic vision. Pressing the SYN VIS Softkey displays the SVT feature softkeys. The softkeys are labeled PATHWAY, SYN TERR, HRZN HDG, and APTSIGNS. The BACK Softkey returns to the previous level of softkeys. Synthetic Terrain must be active before any other SVT feature may be activated. HRZN HDG, APTSIGNS, and PATHWAY Softkeys are only available when the SYN TERR Softkey is activated (gray with black characters). After activating the SYN TERR Softkey, the HRZN HDG, APTSIGNS, and PATHWAY softkeys may be activated in any combination to display desired features. When system power is cycled, the last selected state (on or off) of the SYN TERR, HRZN HDG, APTSIGNS, and PATHWAY softkeys is remembered by the system. • PATHWAY Softkey enables display of rectangular boxes that represent course guidance. • SYN TERR Softkey enables synthetic terrain depiction. • HRZN HDG Softkey enables horizon heading marks and digits. • APTSIGNS Softkey enables airport signposts. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 549 ADDITIONAL FEATURES PFD SYN VIS BACK Pressing the BACK Softkey returns to the top-level softkeys. BACK PATHWAY SYN TERR HRZN HDG APTSIGNS Pressing the BACK Softkey returns to the previous level of softkeys. Figure 8-2 SVT Softkeys Activating and deactivating SVT: 1) Press the PFD Softkey. 2) Press the SYN VIS Softkey. 3) Press the SYN TERR Softkey. The SVT display will cycle on or off with the SYN TERR Softkey. Activating and deactivating Pathways: 1) Press the PFD Softkey. 2) Press the SYN VIS Softkey. 3) Press the PATHWAY Softkey. The Pathway feature will cycle on or off with the PATHWAY Softkey. Activating and deactivating Horizon Headings: 1) Press the PFD Softkey. 2) Press the SYN VIS Softkey. 3) Press the HRZN HDG Softkey. The horizon heading display will cycle on or off with the HRZN HDG Softkey. Activating and deactivating Airport Signs: 1) Press the PFD Softkey. 2) Press the SYN VIS Softkey. 3) Press the APTSIGNS Softkey. Display of airport signs will cycle on or off with the APTSIGNS Softkey. 550 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES SVT FEATURES Selected Altitude Airport Runway Pathways Color Matches CDI Indicating NAV Source Flight Path Marker Zero Pitch Line (ZPL) with Compass Heading Marks Airplane Symbol Synthetic Terrain SVT Softkeys Figure 8-3 SVT on the Primary Flight Display NOTE: Pathways and terrain features are not a substitute for standard course and altitude deviation information provided by the altimeter, CDI, and VDI. NOTE: Pathways are not available when the cross-pointer (X-Pointer) flight director format is selected. PATHWAYS Pathways provide a three-dimensional perspective view of the selected route of flight shown as colored rectangular boxes representing the horizontal and vertical flight path of the active flight plan. The box size represents 700 feet wide by 200 feet tall during enroute, oceanic, and terminal flight phases. During an approach, the box width is 700 feet or one half full scale deviation on the HSI, whichever is less. The height is 200 feet or one half full scale deviation on the VDI, whichever is less. The altitude at which the pathway boxes are displayed is determined by the selected altitude during climb, cruise, and when the active leg is the final approach course prior to intercepting the glidepath/glideslope. During a descent (except while on the approach glidepath/glideslope), the pathway boxes are displayed at the selected altitude, or the VNAV altitude programmed for the active leg in the flight plan, or the published altitude constraint, whichever is higher (Figure 8-4). Just prior to intercepting the glidepath/glideslope, the pathway boxes are displayed on the glidepath/glideslope, or the selected altitude, whichever is lower. The color of the rectangular boxes may be magenta, green, or white depending on the route of flight and navigation source selected. The active GPS or GPS overlay flight plan leg is represented by magenta boxes that correspond to the Magenta CDI. A localizer course is represented by green boxes that correspond to a green CDI. An inactive leg of an active flight plan is represented by white boxes corresponding to a white line drawn on the Inset map or MFD map indicating an inactive leg. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 551 ADDITIONAL FEATURES Selected Altitude Programmed Altitudes Figure 8-4 Programmed and Selected Altitude Pathways provide supplemental glidepath/glideslope information on an active ILS, LPV, LNAV/VNAV, and some LNAV approaches. Pathways are intended as an aid to situational awareness and should not be used independent of the CDI, VDI, glide path indicator, and glide slope indicator. They are removed from the display when the selected navigation information is not available. Pathways are not displayed beyond the active leg when leg sequencing is suspended and are not displayed on any portion of the flight plan leg that would lead to intercepting a leg in the wrong direction. Pathways are also automatically removed from the display in the event a Resolution Advisory (RA) is issued by the optional TCAS II system. Pathways may then be re-displayed by pressing the PATHWAY Softkey. Departure and Enroute Prior to intercepting an active flight plan leg, pathways are displayed as a series of boxes with pointers at each corner that point in the direction of the active waypoint. Pathways are not displayed for the first leg of the flight plan if that segment is a Heading-to-Altitude leg. The first segment displaying pathways is the first active GPS leg or active leg with a GPS overlay. If this leg of the flight plan route is outside the SVT field of view, pathways will not be visible until the aircraft has turned toward this leg. While approaching the center of the active leg and prescribed altitude, the number of pathway boxes decreases to a minimum of four. Climb profiles cannot be displayed due to the variables associated with aircraft performance. Flight plan legs requiring a climb are indicated by pathways displayed at a level above the aircraft at the altitude selected or programmed. 552 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Descent and Approach Pathways are shown descending only for a programmed descent (Figures 8-5, 8-6). When the flight plan includes programmed descent segments, pathways are displayed along the descent path provided that the selected altitude is lower than the programmed altitude. When an approach providing vertical guidance is activated, Pathways are shown level at the selected altitude up to the point along the final approach course where the altitude intercepts the extended vertical descent path, glidepath, or glideslope. From the vertical path descent, glidepath, or glideslope intercept point, the pathways are shown inbound to the Missed Approach Point (MAP) along the published lateral and vertical descent path, or at the selected altitude, whichever is lower. During an ILS approach, the initial approach segment is displayed in magenta at the segment altitudes if GPS is selected as the navigation source on the CDI. When switching to localizer inbound with LOC selected as the navigation source on the CDI, pathways are displayed in green along the localizer and glide slope. VOR, LOC BC, and ADF approach segments that are approved to be flown using GPS are displayed in magenta boxes. Segments that are flown using other than GPS or ILS, such as heading legs or VOR final approach courses are not displayed. Selected Altitude set for Enroute Selected Altitude set for Departure Climbs NOT displayed by pathway Non-programmed descents NOT displayed by pathway TOD Selected Altitude for Step Down Programmed descent displayed by pathway Selected Altitude or Programmed Altitude (whichever is higher) Figure 8-5 SVT Pathways, Enroute and Descent 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 553 ADDITIONAL FEATURES Missed Approach Upon activating the missed approach, pathways lead to the Missed Approach Holding Point (MAHP) and are displayed as a level path at the published altitude for the MAHP, or the selected altitude, whichever is the highest. If the initial missed approach leg is a Course-to-Altitude (CA) leg, the pathways boxes will be displayed level at the altitude published for the MAHP. If the initial missed approach leg is defined by a course using other than GPS, pathways are not displayed for that segment. In this case, the pathways displayed for the next leg may be outside the field of view and will be visible when the aircraft has turned in the direction of that leg. Pathways are displayed along each segment including the path required to track course reversals that are part of a procedure, such as holding patterns. Pathways boxes will not indicate a turn to a MAHP unless a defined geographical waypoint exists between the MAP and MAHP. FAF Descent displayed by pathway Selected Altitude or Programmed Altitude (whichever is higher) MAP Climbs NOT displayed by pathway Turn Segment NOT displayed by pathway MAHP Figure 8-6 SVT Pathways, Approach, Missed Approach, and Holding 554 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES FLIGHT PATH MARKER The Flight Path Marker (FPM), also known as a Velocity Vector, is displayed on the PFD at groundspeeds above 30 knots. The FPM depicts the approximate projected path of the aircraft accounting for wind speed and direction relative to the three-dimensional terrain display. The FPM is always available when the Synthetic Terrain feature is in operation. The FPM represents the direction of the flight path as it relates to the terrain and obstacles on the display, while the airplane symbol represents the aircraft heading. The FPM works in conjunction with the Pathways feature to assist the pilot in maintaining desired altitudes and direction when navigating a flight plan. When on course and altitude the FPM is aligned inside the pathway boxes as shown (Figure 8-7). The FPM may also be used to identify a possible conflict with the aircraft flight path and distant terrain or obstacles. Displayed terrain or obstacles in the aircraft’s flight path extending above the FPM could indicate a potential conflict, even before an alert is issued by TAWS. However, decisions regarding terrain and/or obstacle avoidance should not be made using only the FPM. Flight Path Marker (FPM) Wind Vector Figure 8-7 Flight Path Marker and Pathways ZERO PITCH LINE The Zero Pitch Line is drawn completely across the display and represents the horizon when the terrain horizon is difficult to distinguish from other terrain being displayed. It may not align with the terrain horizon, particularly when the terrain is mountainous or when the aircraft is flown at high altitudes. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 555 ADDITIONAL FEATURES HORIZON HEADING The Horizon Heading is synchronized with the HSI and shows approximately 60 degrees of compass heading in 30‑degree increments on the Zero Pitch Line. Horizon Heading tick marks and digits appearing on the zero pitch line are not visible behind either the airspeed or altitude display. Horizon Heading is used for general heading awareness, and is activated and deactivated by pressing the HRZN HDG Softkey. TRAFFIC WARNING: Intruder aircraft at or below 500 ft. AGL may not appear on the SVT display or may appear as a partial symbol. Traffic symbols are displayed in their approximate locations as determined by the related traffic systems. Traffic symbols are displayed in three dimensions, appearing larger as they are getting closer, and smaller when they are further away. Traffic within 250 feet laterally of the aircraft will not be displayed on the SVT display. Traffic symbols and coloring are consistent with that used for traffic displayed in the Inset map or MFD traffic page. If the traffic altitude is unknown, the traffic will not be displayed on the SVT display. For more details refer to the traffic system discussion in the Hazard Avoidance section. AIRPORT SIGNS Airport Signs provide a visual representation of airport location and identification on the synthetic terrain display. When activated, the signs appear on the display when the aircraft is approximately 15 nm from an airport and disappear at approximately 4.5 nm. Airport signs are shown without the identifier until the aircraft is approximately eight nautical miles from the airport. Airport signs are not shown behind the airspeed or altitude display. Airport signs are activated and deactivated by pressing the APTSIGNS Softkey. Traffic Airport Sign without Identifier (Between 8 nm and 15 nm) Airport Sign with Identifier (Between 4.5 nm and 8 nm) Figure 8-8 Airport Signs 556 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES RUNWAYS WARNING: Do not use SVT runway depiction as the sole means for determining the proximity of the aircraft to the runway or for maintaining the proper approach path angle during landing. NOTE: Not all airports have runways with endpoint data in the database, therefore, these runways are not displayed. Runway data provides improved awareness of runway location with respect to the surrounding terrain. All runway thresholds are depicted at their respective elevations as defined in the database. In some situations, where threshold elevations differ significantly, crossing runways may appear to be layered. As runways are displayed, those within 45 degrees of the aircraft heading are displayed in white. Other runways will be gray in color. When an approach for a specific runway is active, that runway will appear brighter and be outlined with a white box, regardless of the runway orientation as related to aircraft heading. As the aircraft gets closer to the runway, more detail such as runway numbers and centerlines will be displayed. Runway Selected for Approach Other Runway on Airport Figure 8-9 Airport Runways 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 557 ADDITIONAL FEATURES TAWS ALERTING Terrain alerting on the synthetic terrain display is triggered by Forward-looking Terrain Avoidance (FLTA) alerts. In addition to the yellow terrain shading for a caution alert and the red shading for a warning alert, TAWS-B alerting will also indicate potential impact points. These potential impact points correspond to red and/or yellow X symbols on the PFD Inset Map (as shown in Figure 8-10), MFD map displays, and TAWS-B Page on the MFD. Terrain shading will only occur on the synthetic terrain display on the PFD and TAWS-A Page on the MFD when using the optional TAWS-A system. No terrain shading nor potential impact points will be displayed on the PFD inset map or the MFD map display. For more detailed information regarding TAWS, refer to the Hazard Avoidance Section. In some instances, a terrain or obstacle alert may be issued with no conflict shading displayed on the synthetic terrain. In these cases, the conflict is outside the SVT field of view to the left or right of the aircraft. TERRAIN Annunciation Terrain Caution Potential Impact Point Figure 8-10 Terrain Alert 558 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Obstacles are represented on the synthetic terrain display by standard two-dimensional tower symbols found on the Inset map and MFD maps and charts. Obstacle symbols appear in the perspective view with relative height above terrain and distance from the aircraft. When employing a TAWS-B system, unlike the Inset map and MFD moving map display, obstacles on the synthetic terrain display do not change colors to warn of potential conflict with the aircraft’s flight path until the obstacle is associated with an actual FLTA alert. Obstacles greater than 1000 feet below the aircraft altitude are not shown. Obstacles are shown behind the airspeed and altitude displays. As with terrain alerting on a TAWS-A system, obstacle alerting is limited to the synthetic terrain display on the PFD and the TAWS-A Page on the MFD. Obstacle Annunciation Obstacle Warning Potential Impact Point Figure 8-11 Obstacle 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 559 ADDITIONAL FEATURES FIELD OF VIEW The PFD field of view can be represented on the MFD Navigation Map Page. Two dashed lines forming a V‑shape in front of the aircraft symbol on the map, represent the forward viewing area shown on the PFD. Configuring field of view: 1) While viewing the Navigation Map Page, press the MENU Key to display the PAGE MENU. 2) Turn the large FMS Knob to highlight Map Setup and press the ENT Key. Field of View Navigation Map Page OPTIONS Menu Map Setup Menu, Map Group, Field of View Option Figure 8-12 Option Menus 3) Turn the FMS Knob to select the Map Group and press the ENT Key. 4) Turn the large FMS Knob to scroll through the Map Group options to FIELD OF VIEW. 5) Turn the small FMS Knob to select On or Off. 6) Press the FMS Knob to return to the Navigation Map Page. 560 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES The following figure compares the PFD forward looking depiction with the MFD plan view and FIELD OF VIEW turned on. Lines Depict PFD Field of View SVT View on the PFD Field of View on the MFD Figure 8-13 PFD and MFD Field of View Comparison 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 561 ADDITIONAL FEATURES 8.2 SAFETAXI The SafeTaxi feature gives greater map detail when viewing airports at close range. The maximum map ranges for enhanced detail are pilot configurable. When viewing at ranges close enough to show the airport detail, the map reveals taxiways with identifying letters/numbers, airport Hot Spots, and airport landmarks including ramps, buildings, control towers, and other prominent features. Resolution is greater at lower map ranges. When the MFD display is within the SafeTaxi ranges, the airplane symbol on the airport provides enhanced position awareness. Designated Hot Spots are recognized at airports with many intersecting taxiways and runways, and/or complex ramp areas. Airport Hot Spots are outlined to caution pilots of areas on an airport surface where positional awareness confusion or runway incursions happen most often. Hot Spots are defined with a magenta circle or outline around the region of possible confusion. Any map page that displays the navigation view can also show the SafeTaxi airport layout within the maximum configured range. The following is a list of pages where the SafeTaxi feature can be seen: • Navigation Map Page • VOR Information Page • Inset Map (PFD) • User Waypoint Information Page • Weather Datalink Page • Trip Planning Page • Airport Information Page • Nearest Pages • Intersection Information Page • Active and Stored Flight Plan Pages • NDB Information Page 562 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES During ground operations the aircraft’s position is displayed in reference to taxiways, runways, and airport features. In the example shown, the aircraft is on taxiway Bravo inside the High Alert Intersection boundary on KSFO airport. Airport Hot Spots are outlined in magenta. When panning over the airport, features such as runway holding lines and taxiways are shown at the cursor. Taxiway Identification Aircraft Position Airport Hot Spot Outline Airport Features Figure 8-14 SafeTaxi Depiction on the Navigation Map Page DCLTR Softkey Removes Taxiway Markings The DCLTR Softkey (declutter) label advances to DCLTR-1, DCLTR -2, and DCLTR-3 each time the softkey is selected for easy recognition of decluttering level. Selecting the DCLTR Softkey removes the taxiway markings and airport feature labels. Selecting the DCLTR-1 Softkey removes VOR station ID, the VOR symbol, and intersection names if within the airport plan view. Selecting the DCLTR-2 Softkey removes the airport runway layout, unless the airport in view is part of an active route structure. Selecting the DCLTR-3 Softkey cycles back to the original map detail. Refer to Map Declutter Levels in the Flight Management Section. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 563 ADDITIONAL FEATURES Configuring SafeTaxi range: 1) While viewing the Navigation Map Page, press the MENU Key to display the PAGE MENU. 2) Turn the large FMS Knob to highlight the Map Setup Menu Option and press the ENT Key. Figure 8-15 Navigation Map PAGE MENU, Map Setup Option 3) Turn the FMS Knob to select the Aviation Group and press the ENT Key. 4) Turn the large FMS Knob to scroll through the Aviation Group options to SAFETAXI. 5) Turn the small FMS Knob to display the range of distances. 6) Turn either FMS Knob to select the desired distance for maximum SafeTaxi display range. 7) Press the ENT Key to complete the selection. 8) Press the FMS Knob to return to the Navigation Map Page. SAFETAXI Option SafeTaxi Range Options Figure 8-16 MAP SETUP Menu, Aviation Group, SAFETAXI Range Options 564 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES SAFETAXI DATABASE CYCLE NUMBER AND REVISION SafeTaxi database is revised every 56 days. SafeTaxi is always available for use after the expiration date. When turning on the system, the Power-up Page indicates whether the databases are current, out of date, or not available. SafeTaxi Database Figure 8-17 Power-up Page, SafeTaxi Database Power-up Page Display Definition Normal operation. SafeTaxi database is valid and within current cycle. SafeTaxi database has expired. Database card contains no SafeTaxi data. Table 8-1 SafeTaxi Annunciation Definitions The SafeTaxi Region, Version, Cycle, Effective date and Expires date of the database cycle can also be found on the AUX - System Status page, as seen in Figure 8-18. Select the MFD1 DB Softkey to place the cursor in the DATABASE window. Scroll through the listed information by turning the FMS Knob or pressing the ENT Key until the SafeTaxi database information is shown. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 565 ADDITIONAL FEATURES The SafeTaxi database cycle number shown in Figure 8-18, 14S3, is deciphered as follows: 14 – Indicates the year 2014 S – Indicates the data is for SafeTaxi 3 – Indicates the third issue of the SafeTaxi database for the year The SafeTaxi EFFECTIVE date 07–MAY–14 is the beginning date for the current database cycle. SafeTaxi EXPIRES date 02–JUL–14 is the revision date for the next database cycle. SafeTaxi Data Figure 8-18 AUX – System Status Page, SafeTaxi Current Information SafeTaxi information appears in blue and yellow text. The EFFECTIVE date appears in blue when data is current and in yellow when the current date is before the effective date. The EXPIRES date appears in blue when data is current and in yellow when expired (Figures 8‑18 and 8-19). NOT AVAILABLE appears in blue in the REGION field if SafeTaxi data is not available on the database card (Figure 8‑19). An expired SafeTaxi database is not disabled and will continue to function indefinitely. Select the MFD1 DB Softkey a second time. The softkey label will change to PFD1 DB. The DATABASE window will now be displaying database information for PFD1. As before, scroll through the listed information by turning the FMS Knob or pressing the ENT Key until the SafeTaxi database information is shown. Select the PFD1 DB Softkey. The softkey label will change to PFD2 DB. The DATABASE window will now display database information for PFD2. Again, scroll through the listed information by turning the FMS Knob or pressing the ENT Key until the SafeTaxi database information is shown. Refer to Updating Garmin Databases in Appendix B for instructions on revising the SafeTaxi database. 566 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Figure 8-19 illustrates possible SafeTaxi database conditions that may appear on the AUX - System Status Page. The EFFECTIVE date is the beginning date for this database cycle. If the present date is before the effective date, the EFFECTIVE date appears in yellow and the EXPIRES date appears in blue. The EXPIRES date is the revision date for the next database cycle. NOT AVAILABLE indicates that SafeTaxi is not available on the database card or no database card is inserted. Current Date is before Effective Date SafeTaxi Database has Expired SafeTaxi Database Not Installed Figure 8-19 AUX – System Status Page, SafeTaxi Database Status 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 567 ADDITIONAL FEATURES 8.3 CHARTVIEW ChartView resembles the paper version of Jeppesen terminal procedures charts. The charts are displayed in full color with high-resolution. The MFD depiction shows the aircraft position on the moving map in the planview of approach charts and on airport diagrams. Airport Hot Spots are outlined in magenta. The geo-referenced aircraft position is indicated by an aircraft symbol displayed on the chart when the current position is within the boundaries of the chart. Inset boxes (Figure 8-20) are not considered within the chart boundaries. Therefore, when the aircraft symbol reaches a chart boundary line, or inset box, the aircraft symbol is removed from the display. Figure 8-20 shows examples of off-scale areas, indicated by the grey shading. Note, the grey shading is for illustrative purposes only and will not appear on the published chart or MFD display. These off-scale areas appear on the chart to convey supplemental information. However, the depicted geographical position of this information, as it relates to the chart planview, is not the actual geographic position. Therefore, when the aircraft symbol appears within one of these areas, the aircraft position indicated is relative to the chart planview, not to the off-scale area. Off-Scale Area Off-Scale Areas Figure 8-20 Sample Chart Indicating Off-Scale Areas NOTE: Do not maneuver the aircraft based solely upon the geo-referenced aircraft symbol. The ChartView database subscription is available from Jeppesen, Inc. Available data includes: • Arrivals (STAR) • Airport Diagrams • Departure Procedures (DP) • NOTAMs • Approaches 568 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES CHARTVIEW SOFTKEYS ChartView functions are displayed on three levels of softkeys. While on the Navigation Map Page, Nearest Airports Page, or Flight Plan Page, selecting the SHW CHRT Softkey displays the available terminal chart and advances to the chart selection level of softkeys: CHRT OPT, CHRT, INFO, DP, STAR, APR, WX, NOTAM, and GO BACK. The chart selection softkeys shown below appear on the Airport Information Page. Selecting the GO BACK Softkey reverts to the top level softkeys and previous page. Selecting the CHRT OPT Softkey advances to the next level of softkeys: ALL, HEADER, PLAN, PROFILE, MINIMUMS, FIT WDTH, FULL SCN, and BACK. While viewing the CHRT OPT Softkeys, after 45 seconds of softkey inactivity, the system reverts to the chart selection softkeys. SHW CHRT CHRT OPT CHRT INFO-1 DP HEADER PLAN APR WX NOTAM GO BACK Selecting the GO BACK Softkey returns to the top-level softkeys and previous page. INFO-2 ALL STAR PROFILE MINIMUMS FIT WDTH FULL SCN BACK Selecting the BACK Softkey returns to the Chart Selection Softkeys. Figure 8-21 ChartView SHW CHRT, Chart Selection, and Chart Option Softkeys 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 569 ADDITIONAL FEATURES TERMINAL PROCEDURES CHARTS Selecting Terminal Procedures Charts: While viewing the Navigation Map Page, Nearest Airport Page, or Flight Plan Page, select the SHW CHRT Softkey. Or: 1) Press the MENU Key to display the PAGE MENU. 2) Turn the large FMS Knob to scroll through the OPTIONS Menu to Show Chart. 3) Press the ENT Key to display the chart. Navigation Map Page OPTIONS Menu Waypoint Airport Information Page OPTIONS Menu Figure 8-22 Option Menus When no terminal procedure chart is available for the nearest airport or the selected airport, the banner CHART NOT AVAILABLE appears on the screen. The CHART NOT AVAILABLE banner does not refer to the Jeppesen subscription, but rather the availability of a particular airport chart selection or procedure for a selected airport. Figure 8-23 Chart Not Available Banner If there is a problem in rendering the data (such as a data error or a failure of an individual chart), the banner UNABLE TO DISPLAY CHART is then displayed. Figure 8-24 Unable To Display Chart Banner 570 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES When a chart is not available by selecting the SHW CHRT Softkey or selecting a Page Menu Option, charts may be obtained for other airports from the WPT Pages or Flight Plan Pages. If a chart is available for the destination airport, or the airport selected in the active flight plan, the chart appears on the screen. When no flight plan is active, or when not flying to a direct-to destination, selecting the SHW CHRT Softkey displays the chart for the nearest airport, if available. The chart shown is the one associated with the WPT – Airport Information page. Usually this is the airport runway diagram. Where no runway diagram exists, but Take Off Minimums or Alternate Minimums are available, that page appears. If Airport Information pages are unavailable, the Approach Chart for the airport is shown. Selecting a chart: 1) While viewing the Navigation Map Page, Flight Plan Page, or Nearest Airports Page, select the SHW CHRT Softkey. The airport diagram or approach chart is displayed on the Airport Information Page. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to select either the Airport Identifier Box or the Approach Box. (Select the APR Softkey if the Approach Box is not currently shown). 4) Turn the small and large FMS Knob to enter the desired airport identifier. 5) Press the ENT Key to complete the airport selection. 6) Turn the large FMS Knob to select the Approach Box. 7) Turn the small FMS Knob to show the approach chart selection choices. 8) Turn either FMS Knob to scroll through the available charts. 9) Press the ENT Key to complete the chart selection. Chart Scale Select Desired Approach Chart from Menu Scroll Through Entire Chart With the Joystick Figure 8-25 Approach Information Page, Chart Selection 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 571 ADDITIONAL FEATURES While the APPROACH Box is selected using the FMS Knob, the softkeys are blank. Once the desired chart is selected, the chart scale can be changed and the chart page can be scrolled using the Joystick. Pressing the Joystick centers the chart on the screen. The aircraft symbol is shown on the chart only if the chart is to scale and the aircraft position is within the boundaries of the chart. The aircraft symbol is not displayed when the Aircraft Not Shown Icon appears (Figure 8‑29). If the Chart Scale Box displays a banner NOT TO SCALE, the aircraft symbol is not shown. The Aircraft Not Shown Icon may appear at certain times, even if the chart is displayed to scale. Selecting the CHRT Softkey switches between the ChartView diagram and the associated map in the WPT page group. In the example shown, the CHRT Softkey switches between the DeKalb Peachtree (KPDK) Airport Diagram and the navigation map on the WPT – Airport Information page. Press CHRT Softkey to Switch Between ChartView and WPT Airport Information Page Figure 8-26 CHRT Softkey, Airport Information Page 572 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Pressing the INFO-1 or INFO-2 Softkey returns to the airport diagram chart when the view is on a terminal procedure chart. If the displayed chart is the airport diagram chart, pressing the INFO-1 or INFO-2 Softkey returns to the Airport Information Page. The aircraft position is shown in magenta on the ChartView diagrams when the location of the aircraft is within the chart boundaries. In the example shown, the aircraft is turning onto Taxiway Bravo on the Charlotte, NC (KCLT) airport. Another source for additional airport information is from the INFO Box above the chart for certain airports. This information source is not related to the INFO-1 or INFO-2 Softkey. When the INFO Box is selected using the FMS Knob, the softkeys are blank. The Charlotte, NC airport has five additional charts offering information; the Airport Diagram, Take-off Minimums, Class B Airspace, Airline Parking Gate Coordinates, and Airline Parking Gate Location. (The numbers in parentheses after the chart name are Jeppesen designators.) Figure 8-27 Airport Information Page, INFO View, Full Screen Width 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 573 ADDITIONAL FEATURES In the example shown in Figure 8-27, the Class B Chart is selected. Pressing the ENT Key displays the Charlotte Class B Airspace Chart (Figure 8-28). Figure 8-28 Airport Information Page, Class B Chart Selected from INFO View Selecting the DP Softkey displays the Departure Procedure Chart if available. Chart Not To Scale Aircraft Not Shown Icon Figure 8-29 Departure Information Page 574 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Selecting the STAR Softkey displays the Standard Terminal Arrival Chart if available. Chart Not To Scale Change Range and Scroll Through the Chart With the Joystick Aircraft Not Shown Icon Figure 8-30 Arrival Information Page Selecting the APR Softkey displays the approach chart for the airport if available. Figure 8-31 Approach Information Page 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 575 ADDITIONAL FEATURES Selecting the WX Softkey shows the airport weather frequency information, and includes weather data such as METAR and TAF from the XM Data Link Receiver, when available. Weather information is available only when an XM Data Link Receiver is installed and the SiriusXM Weather subscription is current. WX Info When Available WX Softkey Selected Figure 8-32 Weather Information Page NOTE: A subdued softkey label indicates the function is disabled. Recent NOTAMS applicable to the current ChartView cycle are included in the ChartView database. Selecting the NOTAM Softkey shows the local NOTAM information for selected airports, when available. When NOTAMS are not available, the NOTAM Softkey label appears subdued and is disabled. The NOTAM Softkey may appear on the Airport Information Page and all of the chart page selections. 576 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Figure 8-33 NOTAM Softkey Enabled NOTAM Softkey Appears When NOTAMS are Available for Selected Airport Local NOTAM on Selected Airport NOTAM Softkey Selected Figure 8-34 Airport Information Page, Local NOTAMs Selecting the NOTAM Softkey again removes the NOTAMS information. Selecting the GO BACK Softkey reverts to the previous page (Navigation Map Page, Nearest Pages, or Flight Plan Page). 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 577 ADDITIONAL FEATURES CHART OPTIONS Selecting the CHRT OPT Softkey displays the next level of softkeys, the chart options level (Figure 8-21). Selecting the ALL Softkey shows the entire approach chart on the screen. Entire Chart Shown Figure 8-35 Approach Information Page, ALL View Selecting the HEADER Softkey shows the header view (approach chart briefing strip) on the screen. Approach Chart Briefing Strip Figure 8-36 Approach Information Page, Header View 578 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Selecting the PLAN Softkey shows the approach chart two dimensional plan view. Approach Chart Plan View Figure 8-37 Approach Information Page, Plan View Selecting the PROFILE Softkey displays the approach chart descent profile strip. Approach Chart Descent Profile Strip Figure 8-38 Approach Information Page, Profile View, Full Screen Width 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 579 ADDITIONAL FEATURES Selecting the MINIMUMS Softkey displays the minimum descent altitude/visibility strip at the bottom of the approach chart. Minimum Descent Altitude/ Visibility Strip Figure 8-39 Approach Information Page, Minimums View, Full Screen Width 580 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES If the chart scale has been adjusted to view a small area of the chart, selecting the FIT WIDTH Softkey changes the chart size to fit the available screen width. Select FIT WDTH Softkey to Show Full Chart Width Figure 8-40 Airport Information Page, FIT WDTH Softkey Selected Selecting the FULL SCN Softkey alternates between removing and replacing the data window to the right. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 581 ADDITIONAL FEATURES Selecting Additional Information: 1) While viewing the Airport Taxi Diagram, select the FULL SCN Softkey to display the information windows (AIRPORT, INFO). 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the AIRPORT, INFO, RUNWAYS, or FREQUENCIES Box (INFO Box shown). 4) Turn the small FMS Knob to select the INFO Box choices. If multiple choices are available, scroll to the desired choice with the large FMS Knob and press the ENT Key to complete the selection. 5) Press the FMS Knob again to deactivate the cursor. Available Information Select FULL SCN Softkey to Switch Between Full Screen and Chart with Info Window Figure 8-41 Airport Information Page, Full Screen and Info Window Selecting the BACK Softkey, or waiting for 45 seconds reverts to the chart selection softkeys. The full screen view can also be selected by using the page menu option. 582 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Selecting full screen On or Off: 1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS. 2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key. 3) Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options. 4) Turn the small FMS Knob to choose between the On and Off Full Screen Options. Chart Setup Option Full Screen On/Off Selection Figure 8-42 Page Menus 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 583 ADDITIONAL FEATURES DAY/NIGHT VIEW ChartView can be displayed on a white or black background for day or night viewing. The Day View offers a better presentation in a bright environment. The Night View gives a better presentation for viewing in a dark environment. When the CHART SETUP Box is selected the softkeys are blank. Selecting Day, Night, or Automatic View: 1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS. 2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key. Figure 8-43 Waypoint Information Page, OPTIONS Menu 3) Turn the large FMS Knob to move to the COLOR SCHEME Option (Figure 8‑44). 4) Turn the small FMS Knob to choose between Day, Auto, and Night Options. 5) If Auto Mode is selected, turn the large FMS Knob to select the percentage field. Use the small FMS Knob to change the percentage value. The percentage value is the day/night crossover point based on the percentage of backlighting intensity. For example, if the value is set to 15%, the day/night display changes when the display backlight reaches 15% of full brightness. The display must be changed in order for the new setting to become active. This may be accomplished by selecting another page or changing the display range. 6) Press the FMS Knob when finished to remove the Chart Setup Menu. 584 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Figure 8-44 Arrival Information Page, Day View Figure 8-45 Arrival Information Page, Night View 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 585 ADDITIONAL FEATURES CHARTVIEW CYCLE NUMBER AND EXPIRATION DATE The ChartView database is revised every 14 days. Charts are still viewable during a period that extends from the cycle expiration date to the disables date. ChartView is disabled 70 days after the expiration date and is no longer available for viewing. After the expiration date, the ChartView database is no longer current, however, data displayed on the actual charts may still be current. When viewing charts after the ChartView database has expired, ensure the displayed chart is current before using. When turning on the system, the Power-up Page displays the current status of the ChartView database. See the table below for the various ChartView Power-up Page displays and the definition of each. ChartView Database Figure 8-46 Power-up Page, ChartView Database Power-up Page Display Definition Blank Line. system is not configured for ChartView. Contact a Garminauthorized service center for configuration. System is configured for ChartView but no chart database is installed. Contact Jeppesen for a ChartView database. Normal operation. ChartView database is valid and within current cycle. ChartView database is within 1 week after expiration date. A new cycle is available for update. ChartView database is beyond 1 week after expiration date, but still within the 70 day viewing period. ChartView database has timed out. Database is beyond 70 days after expiration date. ChartView database is no longer available for viewing. System time is not available. GPS satellite data is unknown or the system has not yet locked onto satellites. Check database cycle number for effectivity. System is verifying chart database when new cycle is installed for the first time. After verifying, chart database is found to be corrupt. ChartView is not available. Table 8-2 ChartView Power-up Page Annunciations and Definitions 586 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES The ChartView time critical information can also be found on the AUX - System Status page. The database CYCLE number, EXPIRES, and DISABLES dates of the ChartView subscription appear in either blue or yellow text. When the ChartView EXPIRES date is reached, ChartView becomes inoperative 70 days later. This is shown as the DISABLES date. When the DISABLES date is reached, charts are no longer available for viewing. The SHW CHRT Softkey label then appears subdued and is disabled until a revised issue of ChartView is installed. NOTE: A subdued softkey label indicates the function is disabled. Select the MFD1 DB Softkey to place the cursor in the DATABASE window. Scroll through the listed information by turning the FMS Knob or pressing the ENT Key until the ChartView database information is shown. The ChartView database cycle number shown in the figure, 1404, is deciphered as follows: 14 – Indicates the year 2014 04 – Indicates the fourth issue of the ChartView database for the year The EXPIRES date 06–MAR–14 is the date that this database should be replaced with the next issue. The DISABLES date 15–MAY–14 is the date that this database becomes inoperative. ChartView Data Figure 8-47 AUX – System Status Page, ChartView Current and Available The ChartView database is obtained directly from Jeppesen. Refer to Updating Jeppesen Databases in Appendix B for instructions on revising the ChartView database. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 587 ADDITIONAL FEATURES Other possible AUX - System Status page conditions are shown in Figure 8-48. The EXPIRES date, in yellow, is the revision date for the next database cycle. The DISABLES date, in yellow, is the date that this database cycle is no longer viewable. CYCLE NOT AVAILABLE in blue, indicates no ChartView data is available on the database card or no database card is inserted. ChartView has Expired, but is not Disabled ChartView Database is Disabled ChartView Database is Not Available Figure 8-48 AUX – System Status Page, ChartView Database Status 588 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES 8.4 FLITECHARTS FliteCharts resemble the paper version of AeroNav Services terminal procedures charts. The charts are displayed with high-resolution and in color for applicable charts. The MFD depiction shows the aircraft position on the moving map in the planview of approach charts. The geo-referenced aircraft position is indicated by an aircraft symbol displayed on the chart when the current position is within the boundaries of the chart. An aircraft symbol may be displayed within an off-scale area depicted on some charts. Figure 8-49 shows examples of off-scale areas, indicated by the grey shading. Note, these areas are not shaded on the published chart. These off-scale areas appear on the chart to convey supplemental information. However, the depicted geographical position of this information, as it relates to the chart planview, is not the actual geographic position. Therefore, when the aircraft symbol appears within one of these areas, the aircraft position indicated is relative to the chart planview, not to the off-scale area. NOTE: Do not maneuver the aircraft based solely upon the geo-referenced aircraft symbol. Off-Scale Areas Off-Scale Area Off-Scale Areas Off-Scale Area Figure 8-49 Sample Chart Indicating Off-Scale Areas 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 589 ADDITIONAL FEATURES The FliteCharts database subscription is available from Garmin. Available data includes: • Arrivals (STAR) • Approaches • Departure Procedures (DP) • Airport Diagrams FLITECHARTS SOFTKEYS FliteCharts functions are displayed on three levels of softkeys. While on the Navigation Map Page, Nearest Airports Page, or Flight Plan Page, selecting the SHW CHRT Softkey displays the available terminal chart and advances to the chart selection level of softkeys: CHRT OPT, CHRT, INFO, DP, STAR, APR, WX, and GO BACK. The chart selection softkeys appear on the Airport Information Page. Selecting the GO BACK Softkey reverts to the top level softkeys and previous page. Selecting the CHRT OPT Softkey displays the available terminal chart and advances to the next level of softkeys: ALL, FIT WDTH, FULL SCN, and BACK. While viewing the CHRT OPT Softkeys, after 45 seconds of softkey inactivity, the system reverts to the chart selection softkeys. NOTAMs are not available with FliteCharts. The NOTAM Softkey label appears subdued and is disabled. SHW CHRT CHRT OPT CHRT INFO-1 INFO-2 ALL DP STAR WX APR GO BACK Selecting the GO BACK Softkey returns to the top-level softkeys and previous page. FIT WDTH FULL SCN BACK Selecting the BACK Softkey returns to the Chart Selection Softkeys. Figure 8-50 FliteCharts SHW CHRT, Chart Selection, and Chart Option Softkeys 590 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES TERMINAL PROCEDURES CHARTS Selecting Terminal Procedures Charts: While viewing the Navigation Map Page, Nearest Airport Page, or Flight Plan Page, select the SHW CHRT Softkey. Or: 1) Press the MENU Key to display the PAGE MENU. 2) Turn the large FMS Knob to scroll through the OPTIONS Menu to Show Chart. 3) Press the ENT Key to display the chart. Navigation Map Page OPTIONS Menu Waypoint Airport Information Page OPTIONS Menu Figure 8-51 Option Menus When no terminal procedure chart is available, the banner CHART NOT AVAILABLE appears on the screen. The CHART NOT AVAILABLE banner does not refer to the FliteCharts subscription, but rather the availability of a particular airport chart selection or procedure for a selected airport. Figure 8-52 Chart Not Available Banner If there is a problem in rendering the data (such as a data error or a failure of an individual chart), the banner UNABLE TO DISPLAY CHART is then displayed. Figure 8-53 Unable To Display Chart Banner 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 591 ADDITIONAL FEATURES When a chart is not available by selecting the SHW CHRT Softkey or selecting a Page Menu Option, charts may be obtained for other airports from the WPT Pages or Flight Plan Pages. If a chart is available for the destination airport, or the airport selected in the active flight plan, the chart appears on the screen. When no flight plan is active, or when not flying to a direct-to destination, selecting the SHW CHRT Softkey displays the chart for the nearest airport, if available. The chart shown is one associated with the WPT – Airport Information page. Usually this is the airport runway diagram. Where no runway diagram exists, but Take Off Minimums or Alternate Minimums are available, that page appears. If Airport Information pages are unavailable, the Approach Chart for the airport is shown. Selecting a chart: 1) While viewing the Navigation Map Page, Flight Plan Page, or Nearest Airports Page, select the SHW CHRT Softkey. The airport diagram or approach chart is displayed on the Airport Information Page. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to select either the Airport Identifier Box or the Approach Box. (Select the APR Softkey if the Approach Box is not currently shown). 4) Turn the small and large FMS Knob to enter the desired airport identifier. 5) Press the ENT Key to complete the airport selection. 6) Turn the large FMS Knob to select the Approach Box. 7) Turn the small FMS Knob to show the approach chart selection choices. 8) Turn either FMS Knob to scroll through the available charts. 9) Press the ENT Key to complete the chart selection. Chart Not To Scale Select Desired Approach Chart from Menu Pan Entire Chart With the Joystick Aircraft Not Shown Icon Figure 8-54 Approach Information Page, Chart Selection 592 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES While the APPROACH Box is selected using the FMS Knob, the softkeys are blank. Once the desired chart is selected, the chart scale can be changed and the chart can be panned using the Joystick. Pressing the Joystick centers the chart on the screen. The Chart Scale Box displays a banner NOT TO SCALE. Selecting the CHRT Softkey switches between the FliteCharts diagram and the associated map in the WPT page group. In the example shown, the CHRT Softkey switches between the Charlotte, NC (KCLT) Airport Diagram and the navigation map on the WPT – Airport Information page. Select CHRT Softkey to Switch Between FliteCharts and WPT Airport Information Page Figure 8-55 CHRT Softkey, Airport Information Page 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 593 ADDITIONAL FEATURES Pressing the INFO-1 or INFO-2 Softkey returns to the airport diagram chart when the view is on a terminal procedure chart. If the displayed chart is the airport diagram chart, pressing the INFO-1 or INFO-2 Softkey returns to the Airport Information Page. Another source for additional airport information is from the INFO Box above the chart (Figure 8-55) or to the right of the chart (Figure 8-56) for certain airports. This information source is not related to the INFO-1 or INFO-2 Softkey. When the INFO Box is selected using the FMS Knob, the softkeys are blank. The Charlotte, NC airport has three additional charts offering information; the Airport Diagram, Alternate Minimums, and Take-off Minimums. Info Box Selected Figure 8-56 Airport Information Page, INFO View with Airport Information 594 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES In the example shown in Figure 8-56, TAKE OFF MINIMUMS is selected. Pressing the ENT Key displays the IFR Alternate Minimums Chart (Figure 8-57). Figure 8-57 Airport Information Page, ALTERNATE MINIMUMS Selected from INFO View Selecting the DP Softkey displays the Departure Procedure Chart if available. Figure 8-58 Departure Information Page 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 595 ADDITIONAL FEATURES Selecting the STAR Softkey displays the Standard Terminal Arrival Chart if available. Figure 8-59 Arrival Information Page Pressing the APR Softkey displays the approach chart for the airport if available. The aircraft symbol is shown on the chart only if the chart is to scale and the aircraft position is within the boundaries of the chart. The aircraft symbol is not displayed when the Aircraft Not Shown Icon appears. If the Chart Scale Box displays a banner NOT TO SCALE, the aircraft symbol is not shown. Figure 8-60 Approach Information Page 596 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Selecting the WX Softkey shows the airport weather frequency information, when available, and includes weather data such as METAR and TAF from the XM Data Link Receiver. Weather information is available only when an XM Data Link Receiver is installed and the SiriusXM Weather subscription is current. Selecting Additional Information: 1) While viewing the Airport Taxi Diagram, select the WX Softkey to display the information windows (AIRPORT, INFO). 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the INFO Box. 4) Turn the small FMS Knob to select the INFO Box choices. When the INFO Box is selected the softkeys are blank. If multiple choices are available, scroll to the desired choice with the large FMS Knob and press the ENT Key to complete the selection. 5) Press the FMS Knob again to deactivate the cursor. Info Available on This Airport WX Info When Available Chart Not To Scale Softkeys are Blank during Info Box Selection Figure 8-61 Weather Information Page, WX Softkey Selected WX Softkey Selected Selecting the GO BACK Softkey reverts to the previous page (Navigation Map Page or Flight Plan Page). 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 597 ADDITIONAL FEATURES CHART OPTIONS Selecting the CHRT OPT Softkey displays the next level of softkeys, the chart options level (Figure 8-50). Selecting the ALL Softkey shows the entire chart on the screen. Entire Chart Shown Figure 8-62 Airport Information Page, ALL View Selected 598 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Selecting the FIT WIDTH Softkey fits the width of the chart in the display viewing area. In the example shown, the chart at close range is replaced with the full width chart. Select FIT WDTH Softkey to Show Full Chart Width Figure 8-63 Approach Information Page, FIT WDTH Softkey Selected 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 599 ADDITIONAL FEATURES Selecting the FULL SCN Softkey alternates between removing and replacing the data window to the right. Select FULL SCN Softkey to Switch Between Full Screen Chart and Chart with Info Window Figure 8-64 Airport Information Page, Full Screen and Info Window Selecting the BACK Softkey, or waiting for 45 seconds reverts to the chart selection softkeys. The full screen view can also be selected by using the page menu option. 600 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Selecting full screen On or Off: 1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS. 2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key. 3) Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options. 4) Turn the small FMS Knob to choose between the On and Off Full Screen Options. Chart Setup Option Full Screen On/Off Selection Figure 8-65 Page Menus 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 601 ADDITIONAL FEATURES DAY/NIGHT VIEW FliteCharts can be displayed on a white or black background for day or night viewing. The Day View offers a better presentation in a bright environment. The Night View gives a better presentation for viewing in a dark environment. When the CHART SETUP Box is selected the softkeys are blank. Selecting Day, Night, or Automatic View: 1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS. 2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key. Figure 8-66 Waypoint Information Page, OPTIONS Menu 3) Turn the large FMS Knob to move to the COLOR SCHEME Option (Figure 8‑67). 4) Turn the small FMS Knob to choose between Day, Auto, and Night Options. 5) If Auto Mode is selected, turn the large FMS Knob to select the percentage field. Use the small FMS Knob to change the percentage value. The percentage value is the day/night crossover point based on the percentage of backlighting intensity. For example, if the value is set to 15%, the day/night display changes when the display backlight reaches 15% of full brightness. The display must be changed in order for the new setting to become active. This may be accomplished by selecting another page or changing the display range. 6) Press the FMS Knob when finished to remove the Chart Setup Menu. 602 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Figure 8-67 Approach Information Page, Day View Figure 8-68 Approach Information Page, Night View 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 603 ADDITIONAL FEATURES FLITECHARTS CYCLE NUMBER AND EXPIRATION DATE FliteCharts data is revised every 28 days. Charts are still viewable during a period that extends from the cycle expiration date to the disables date. FliteCharts is disabled 180 days after the expiration date and are no longer available for viewing upon reaching the disables date. After the expiration date, the FliteCharts database is no longer current, however, data displayed on the actual charts may still be current. When viewing charts after the FliteCharts database has expired, ensure the displayed chart is current before using. When turning on the system, the Power-up Page displays the current status of the FliteCharts database. See the table below for the various FliteCharts Power-up Page displays and the definition of each. FliteCharts Database Figure 8-69 Power-up Page, FliteCharts Database Power-up Page Display Definition Blank Line. system is not configured for FliteCharts. Contact a Garminauthorized service center for configuration. System is configured for FliteCharts but no chart database is installed. Refer to Updating Garmin Databases in Appendix B for the FliteCharts database Normal operation. FliteCharts database is valid and within current cycle. FliteCharts database is beyond the expiration date, but still within the 180 day viewing period. FliteCharts database has timed out. Database is beyond 180 days after expiration date. FliteCharts database is no longer available for viewing. Table 8-3 FliteCharts Power-up Page Annunciations and Definitions Other possible AUX - System Status page conditions are shown in Figure 8-70. ‘FliteCharts Expires’ plus a date in white, indicates the chart database is current. ‘Chart data is out of date!’ in yellow, indicates charts are still viewable, but approaching the disable date. 604 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES When the 180 day grace period has expired, ‘Chart data is disabled.’ in yellow indicates that the FliteCharts database has expired and is no longer viewable. ‘Chart Data: N/A’ appears in white if no FliteCharts data is available on the database card or no database card is inserted. FliteCharts time critical information can also be found on the AUX - System Status page. The FliteCharts database REGION, CYCLE number, EFFECTIVE, EXPIRES, and DISABLES dates of the subscription appear in either blue or yellow text. Dates shown in blue are current data. Dates shown in yellow indicate the data is not within the current subscription period. FliteCharts becomes inoperative 180 days after the FliteCharts EXPIRES date is reached, and is no longer available for viewing. This date is shown as the DISABLES date. After the disable date the SHW CHRT Softkey label appears subdued and is unavailable until a revised issue of FliteCharts is installed. NOTE: A subdued softkey label indicates the function is disabled. Select the MFD1 DB Softkey to place the cursor in the DATABASE window. Scroll through the listed information by turning the FMS Knob or pressing the ENT Key until the FliteCharts database information is shown. The FliteCharts database cycle number shown in the figure, 1405, is deciphered as follows: 14 – Indicates the year 2014 05 – Indicates the fifth issue of the FliteCharts database for the year The FliteCharts EFFECTIVE date 07–MAY–14 is the first date that this database is current. The FliteCharts EXPIRES date 04–JUN–14 is the last date that this database is current. The DISABLES date 01–DEC–14 is the date that this database becomes inoperative. FliteCharts Data Figure 8-70 AUX – System Status Page, FliteCharts Current and Available 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 605 ADDITIONAL FEATURES The FliteCharts database is provided from Garmin. Refer to Updating Garmin Databases in Appendix B for instructions on revising the FliteCharts database. The other four possible AUX - System Status page conditions are shown here. The EFFECTIVE date, in yellow, indicates the current date precedes the date the FliteCharts database becomes effective. The EXPIRES date, in yellow, is the revision date for the next database cycle. The DISABLES date, in yellow, is the date that this database cycle is no longer viewable. NOT AVAILABLE in blue, indicate the FliteCharts database is not available on the database card or no database card is inserted. Current Date is Before Effective Date FliteCharts Expired, but is not Disabled FliteCharts Database is Disabled FliteCharts Database is Not Available Figure 8-71 AUX – System Status Page, FliteCharts Datbase Status 606 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES 8.5 AIRPORT DIRECTORY The Aircraft Owners and Pilots Association (AOPA) and optional AC-U-KWIK Airport Directory databases offer detailed information regarding services, hours of operation, lodging options, and more. This information is viewed on the Airport Information Page by selecting the INFO Softkey until INFO-2 is displayed as shown in Figure 8-72. Both Airport Directories are available for downloading at flygarmin.com. However, copy only one of the databases to the Supplemental Data Card. The system cannot recognize both databases simultaneously. Selecting the Airport Directory Page: 1) Turn the large FMS Knob to select the ‘WPT’ page group. 2) Turn the small FMS Knob to select the AIRPORT INFORMATION Page. Initially, information for the airport closest to the aircraft’s present position is displayed. 3) If necessary, select the INFO softkey until INFO-2 is displayed. Figure 8-72 Airport Directory Information on the Airport Information Page 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 607 ADDITIONAL FEATURES AIRPORT DIRECTORY DATABASE CYCLE NUMBER AND REVISION The Airport Directory databases are revised every 56 days. Check fly.garmin.com for the current database. The Airport Directory is always available for use after the expiration date. When turning on the system, the Power-up Page indicates whether the databases are current, out of date, or not available. Airport Directory Database Figure 8-73 Power-up Page, Airport Directory Database Power-up Page Display Definition Normal operation. Airport Directory database is valid and within current cycle. Airport Directory database has expired. Database card contains no Airport Directory data. Table 8-4 Airport Directory Annunciation Definitions 608 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES The Airport Directory Region, Version, Cycle, Effective date and Expires date of the database cycle can also be found on the AUX - System Status page, as seen in Figure 8-74. Select the MFD1 DB Softkey to place the cursor in the DATABASE window. Scroll through the listed information by turning the FMS Knob or pressing the ENT Key until the Airport Directory database information is shown. The Airport Directory database cycle number shown in the figure, 14D2, is deciphered as follows: 14 – Indicates the year 2014 D – Indicates the data is for Airport Directory 2 – Indicates the second issue of the Airport Directory database for the year The Airport Directory EFFECTIVE date 15–APR–14 is the beginning date for the current database cycle. The Airport Directory EXPIRES date 14–JUL–14 is the revision date for the next database cycle. Airport Directory Data Figure 8-74 AUX – System Status Page, Airport Directory Current Information Airport Directory information appears in blue and yellow text. The EFFECTIVE date appears in blue when data is current and in yellow when the current date is before the effective date. The EXPIRES date appears in blue when data is current and in yellow when expired (Table 8-4). NOT AVAILABLE appears in blue in the REGION field if Airport Directory data is not available on the database card. An expired Airport Directory database is not disabled and will continue to function indefinitely. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 609 ADDITIONAL FEATURES 8.6 SATELLITE TELEPHONE AND SMS MESSAGING NOTE: Separate accounts must be established to access the Iridium satellite network for voice and Garmin Connext for data transmission of maintenance reports. Up to two optional GSR 56 Iridium Transceivers provide Iridium Satellite Telephone service and SMS text messaging. Iridium telephone and text messaging are available to the flight crew through the Multi-function Display, audio panel and headset. The system provides a telephone handset interface to be used for voice communication between the aircraft cabin and the cockpit and for Iridium telephone service in the aircraft cabin. Operation of these features in the cockpit is accomplished through the AUX-TELEPHONE and AUX-TEXT MESSAGING Pages. For operation using the cabin handset, consult the instructions provided with the handset. REGISTERING WITH GARMIN CONNEXT A subscriber account must be established prior to using the Iridium Satellite System. Before setting up an Iridium account, obtain the serial number of the Iridium Transceiver (GSR1) and the System ID by selecting the AUX- SYSTEM STATUS Page as shown in Figure 8-75. Contact Connext at 1-866-739-5687 in the United States or 913-397-8200, ext. 1135. Iridium Transceiver Serial Number System ID Number Figure 8-75 Identification Needed for Iridium Registration 610 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES TELEPHONE COMMUNICATION The pilot or copilot can place and answer calls on the Iridium satellite network as well as to or from the telephone handset in the cabin. Calls can also be answered or made from the cabin phone, however, only actions initiated from the cockpit phone will be discussed here. See the cabin handset user guide for more information. Control and monitoring of telephone functions are accomplished through the AUX-TELEPHONE Page. Viewing the Telephone Page: 1) Turn the large FMS Knob on the MFD to select the AUX page group. 2) Turn the small FMS Knob to select SATELLITE PHONE. 3) If necessary, select the TEL Softkey to display the AUX-TELEPHONE Page. The PHONE STATUS display, as shown in Figure 8-76, gives a graphical representation of the current disposition of voice and/or data transmissions. Table 8-5 describes symbology used on Phone Status display. Satellite Signal Strength External Phone Internal Phones Figure 8-76 Phone Status Display 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 611 ADDITIONAL FEATURES Internal Phone External Phone Description Phone is Idle Phone is ringing Phone has a dial tone (off hook) or connected to another phone Phone dialed is busy Phone is dialing another phone Phone has failed Phone status not known Phone is disabled Phone is reserved for data transmission Calling other phone or incoming call from other phone Other phone is on hold Phones are connected Table 8-5 Telephone Symbols 612 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES ENABLE/DISABLE THE IRIDIUM TELEPHONE SYSTEM The Iridium Satellite Telephone System may be turned on or off by using the page menu. Figure 8-77 Enable Iridium Telephone System To enable the Iridium telephone system: 1) With the AUX-TELEPHONE Page displayed, select the MENU Key on the MFD to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Enable Iridium Transmission’. 3) Press the ENT Key. To disable the Iridium telephone system: 1) With the AUX-TELEPHONE Page displayed, select the MENU Key on the MFD to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Disable Iridium Transmission’. 3) Press the ENT Key. INCOMING CALLS When viewing MFD pages other than the AUX-TELEPHONE Page, a pop-up alert similar to Figure 8-78 will be displayed and an aural alert “Incoming Call” will be heard. If the call is from the cabin, CABIN will be displayed as seen in Figure 8-78. If the incoming call is an Iridium network call, IRIDIUM will be displayed. The pop-up alert may be inhibited at times, such as during takeoff. In addition to the pop-up alert, a ringing phone symbol will be displayed to the right of the MFD page title as shown in Figure 8-78. Also, the voice alert “Incoming Call” will be heard on the selected cockpit audio. Incoming Call Pop-up Incoming Call Symbol on MFD Page Figure 8-78 Incoming Call 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 613 ADDITIONAL FEATURES Answering an incoming call in the cockpit: 1) Press the TEL Key on the appropriate audio panel. 2) Select the ANSWER Softkey on the MFD. Or: While viewing the AUX-TELEPHONE Page: NOTE: The Push-to-Talk switch is not utilized for telephone communication. The microphone is active after selecting the ANSWER Softkey, and stays active until the call is terminated. 1) Press the TEL Key on the appropriate audio panel. 2) Press the MENU Key to display the Page Menu. 3) Turn either FMS Knob to place the cursor on ‘Answer Incoming Call’. 4) Press the ENT Key. Selecting the IGNORE Softkey will extinguish the pop-up window and leave the current call unanswered. Selecting the IGNR ALL Softkey will extinguish the pop-up window for the current and all future incoming calls and leave the current call unanswered. Selecting the TEL Softkey will display the AUX-TELEPHONE Page allowing additional call information to be viewed before answering. Disabling incoming call alerts: 1) With the AUX-TELEPHONE Page displayed, press the MENU Key on the MFD to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Disable Incoming Call Alerts’. 3) Press the ENT Key. The voice and pop-up alert will not be displayed now when an incoming call is received. 614 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES OUTGOING CALLS Voice calls can be made from the cockpit to the handset in the cabin, or to an external phone through the Iridium Satellite Network. Making a call to the cabin: 1) Press the TEL Key on the appropriate audio panel. 2) Select the DIAL Softkey on the MFD. A display similar to Figure 8-79 will be shown. Figure 8-79 Initiating a Cabin Call 3) Press the ENT Key. The cursor will move from ‘CABIN’ to ‘OK’. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 615 ADDITIONAL FEATURES 4) Press the ENT Key again. The cabin phone will now ring as seen in Figure 8-80. Figure 8-80 Cabin Phone Ringing When the cabin phone is answered, the connection is established as shown in Figure 8-81. To exit the call, select the HANGUP Softkey. Figure 8-81 Cabin Phone Answered 616 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Making an external call from the cockpit using the Iridium satellite network: 1) Press the TEL Key on the appropriate audio panel. 2) Select the DIAL Softkey on the MFD. A display similar to Figure 8-82 will be shown. Figure 8-82 Initiating an External Call 3) Turn the small FMS Knob to select ‘IRIDIUM’ as seen in Figure 8-83. Figure 8-83 Selecting the Iridium Satellite System 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 617 ADDITIONAL FEATURES 4) Press the ENT Key. The cursor has now moved to the phone number entry field as shown in Figure 8-84. Figure 8-84 Enter Phone Number 5) Enter the desired telephone number by selecting the number softkeys on the MFD or by pressing the numeric keys on the MFD Control Unit. The International dialing sequence is necessary to place a call from the cockpit to an external phone: Country Code + City/Area Code (if any) + Telephone Number. The following country codes may be used when calling other satellite telephone systems. Satellite System Inmarsat ICO Ellipso Iridium Globalstar 618 Embraer Prodigy® Flight Deck 100 Pilot’s Guide Country Code 870 8810 or 8811 8812 or 8813 8816 or 8817 8818 or 8819 190-00728-06 Rev. A ADDITIONAL FEATURES 6) Press the ENT Key. ‘OK’ is highlighted as in Figure 8-85. Figure 8-85 Make the Call 7) Press the ENT Key. The system will begin calling the number, as in Figure 8-86. Figure 8-86 System is Making the Connection 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 619 ADDITIONAL FEATURES When the phone is answered, the connection is established as shown in Figure 8-87. To exit the call, select the HANGUP Softkey. When numeric entries are required while a call is connected, such as selecting menu items like “dial zero to get an operator”, select the KEYPAD Softkey to access the numeric softkeys. Figure 8-87 Phone is Answered, Connection Complete 620 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES PLACING THE COCKPIT PHONE ON HOLD Placing a call on hold: Select the HOLD Softkey on the MFD. Or: 1) Press the MENU Key to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Put Current Call On Hold’. 3) Press the ENT Key. The cockpit phone is now isolated from the call as seen in Figure 8-88. This figure illustrates a conference call between the cockpit, cabin, and an external phone in which the cockpit phone has been put on hold. Select the HOLD Softkey again to resume the call. Figure 8-88 Cockpit Phone on Hold 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 621 ADDITIONAL FEATURES TRANSFERRING A CALL FROM THE COCKPIT From the cockpit phone, an external call can be transferred to the cabin phone, or a call with the cabin phone can be transferred to an external phone, or (when two Iridium Transceivers are installed) an external call can be transferred to another external phone. Transferring a call: 1) Select the TRANS Softkey on the MFD. Or: a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Transfer Current Call’. c) Press the ENT Key. A window similar to that shown in Figure 8-89 will be displayed. In this example, an active call to the cabin is transferred to an external number. Therefore, the window shows the ‘Iridium’ option. If the active call is with an external phone, ‘CABIN’ would be the option. Figure 8-89 Enter Phone Number to Receive Transferred Call 2) Press the ENT Key. The cursor now highlights the phone number entry field. 3) Enter the phone number to which the call is being transferred, as discussed earlier for making an external call on the Iridium satellite network. 4) Press the ENT Key. ‘OK’ is now highlighted. 622 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES 5) Press the ENT Key again to place the call as shown in Figure 8-90. Figure 8-90 Call Transfer to an External Phone When the external phone is answered, the call connection is indicated as in Figure 8-91. Figure 8-91 Call Transfer Complete 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 623 ADDITIONAL FEATURES MAKING A CONFERENCE CALL FROM THE COCKPIT The cabin or an external phone (two external phones if two Iridium Transceivers are installed) can be added to a call already in progress. Adding another phone to an active call: 1) Select the CONF Softkey on the MFD. Or: a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Conference Current Call’. c) Press the ENT Key. A window similar to that shown in Figure 8-92 will be displayed. In this example, an external phone will be added to an active call to the cabin. Therefore, the window shows the ‘IRIDIUM’ option. If the active call is with an external phone, ‘CABIN’ would be the option. Figure 8-92 Initiate a Conference Call 2) Press the ENT Key. The cursor now highlights the phone number entry field. 3) Enter the phone number to be added to the call, as discussed earlier for making an external call on the Iridium satellite network. 4) Press the ENT Key. ‘OK’ is now highlighted. 624 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES 5) Press the ENT Key again to place the call as shown in Figure 8-93. Figure 8-93 Conference in External Phone When the external phone is answered, the call connection is indicated as in Figure 8-94. Figure 8-94 External Phone Added 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 625 ADDITIONAL FEATURES TEXT MESSAGING (SMS) The pilot or copilot can send and receive text messages on the Iridium satellite network. Messages may be sent to an email address or text message capable cellular telephone. Message length is limited to 160 characters, including the email address. The text messaging user interface is mainly through the AUX-TEXT MESSAGING Page. Viewing the Text Messaging Page: 1) Turn the large FMS Knob on the MFD to select the AUX page group. 2) Turn the small FMS Knob to select the SATELLITE PHONE. 3) If necessary, select the SMS Softkey to display the AUX-TEXT MESSAGING Page as shown in Figure 8-95. Figure 8-95 Text Messaging Page 626 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Message Symbol Description Received text message that has not been opened Received text message that has been opened Saved text message, draft not sent System is sending text message Text message has been sent System failed to send text message Predefined text message Table 8-6 Text Message Symbols 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 627 ADDITIONAL FEATURES VIEWING A TEXT MESSAGE WHEN RECEIVED When viewing MFD pages other than the AUX-TEXT MESSAGING Page, a pop-up alert similar to Figure 8-96 will be displayed when a new text message is received. New Text Message Pop-up New Text Message Symbol on MFD Page Figure 8-96 New Text Message Received Select the VIEW Softkey to view the message (Figure 8-97). Selecting the IGNORE Softkey will extinguish the pop-up window and leave the text message unopened. Selecting the IGNR ALL Softkey will extinguish the pop-window and ignore all future incoming text messages. Selecting the SMS Softkey will display the AUX-TEXT MESSAGING Page. Figure 8-97 Text Message Displayed from Pop-Up Alert The pop-up alerts may be enabled or disabled through the Page Menu. 628 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Enabling/disabling incoming text message pop-up alerts: 1) With the AUX-TEXT MESSAGING Page displayed, press the MENU Key on the MFD to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Disable New Message Popups’ or ‘Enable New Message Popups’. 3) Press the ENT Key. The pop-up alert will not be displayed when an incoming text message is received. Figure 8-98 Disabling New Text Message Pop-Ups REPLY TO A TEXT MESSAGE After reading a text message, a reply may be sent. Replying to a text message: While viewing the text message, select the REPLY Softkey. Or: 1) Press the MENU Key to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Reply To Message’. 3) Press the ENT Key. SENDING A TEXT MESSAGE Text messages may be sent from the AUX-TEXT MESSAGING Page. Sending a new text message: 1) While viewing the AUX-TEXT MESSAGING Page, select the NEW Softkey. Or: 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 629 ADDITIONAL FEATURES a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Draft New Message’. c) Press the ENT Key. Figure 8-99 Composing a New Text Message 2) The TEXT MESSAGE DRAFT Window is now displayed with the cursor in the ‘TO’ field. Enter the desired telephone number or email address. Entry can be accomplished through the alphanumeric keys on the MFD Controller, or combination of the FMS Knob on the controller and softkeys on the MFD. The FMS Knob is used to enter letters and numbers, or numbers can be entered from the MFD by selecting the NUMBERS Softkey. Select the CAP LOCK Softkey to create upper and lower case alpha characters. Special characters can be accessed by selecting the SYMBOLS Softkey. See Figure 8-99. 3) Press the ENT Key. The cursor is now displayed in the ‘MESSAGE’ field. 4) Enter the desired message using any combination of entry methods as described in step 2. 5) Press the ENT Key. 6) Select the SEND Softkey to send the message immediately, or select the SAVE Softkey to save the message in the Outbox for sending at a later time. Select the CANCEL Softkey to delete the message. 630 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES PREDEFINED TEXT MESSAGES Time and effort can be saved in typing text messages that are used repeatedly by saving these messages as a predefined message. Creating a predefined text message: 1) While viewing the AUX-TEXT MESSAGING Page, press the MENU Key to display the Page Menu. Figure 8-100 Creating/Editing Predefined Messages 2) Turn either FMS Knob to select ‘Edit Predefined Messages’ as shown in Figure 8-100. 3) Press the ENT Key. The PREDEFINED MESSAGES view is now displayed. 4) Select the NEW Softkey. Or: a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Draft New Predefined Message’. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 631 ADDITIONAL FEATURES c) Press the ENT Key. The PREDEFINED SMS TEXT MESSAGE Window is now displayed as shown in Figure 8-101. Figure 8-101 Composing a Predefined Message 5) The cursor is displayed in the ‘TITLE’ field. Enter the desired message title. Entry can be accomplished through the alphanumeric keys on the MFD Controller, or combination of the FMS Knob on the controller and softkeys on the MFD. The FMS Knob is used to enter letters and numbers, or numbers can be entered from the MFD by selecting the NUMBERS Softkey. Select the CAP LOCK Softkey to create upper and lower case alpha characters. Special characters can be accessed by selecting the SYMBOLS Softkey. 6) Press the ENT Key. The cursor is now displayed in the ‘MESSAGE’ field. 7) Enter the desired message using any combination of entry methods as described in step 5. 8) Press the ENT Key. 9) Select the SAVE Softkey. The new predefined message is now shown in the displayed list. Selecting the CANCEL Softkey will delete the message without saving. 10) Press the MENU Key to display the Page Menu. 11) Turn either FMS Knob to place the cursor on ‘Stop Editing Predefined Message’. 12) Press the ENT Key. Sending a predefined text message: 1) While viewing the AUX-TEXT MESSAGING Page, select the NEW Softkey. 2) The TEXT MESSAGE DRAFT Window is now displayed with the cursor in the ‘TO’ field. Enter the desired telephone number or email address. Entry can be accomplished through the alphanumeric keys on the MFD Controller, or combination of the FMS Knob on the controller and softkeys on the MFD. The FMS Knob is used to enter letters and numbers, or numbers can be entered from the MFD by selecting the NUMBERS Softkey. Select the CAP LOCK Softkey to create upper and lower case alpha characters. Special characters can be accessed by selecting the SYMBOLS Softkey. See Figure 8-102. 632 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES 3) Press the ENT Key. The cursor is now displayed in the ‘MESSAGE’ field (Figure 8-102). Figure 8-102 Composing a New Text Message 4) Select the PREDEFD Softkey. The PREDEFINED MESSAGE MENU Window is displayed as seen in Figure 8-103. Figure 8-103 Predefined Message List 5) Turn either FMS Knob to select the desired predefined message. 6) Press the ENT Key. The predefined message text is inserted into the message field. If desired, the message can be edited by using the FMS Knobs. 7) Press the ENT Key. 8) Select the SEND Softkey to transmit the message. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 633 ADDITIONAL FEATURES TEXT MESSAGE BOXES Received text messages reside in the Inbox as ‘Read’ or ‘Unread’ messages. The Outbox contains ‘Sent” and ‘Unsent’ text messages. Saved messages that are meant to be sent later are stored as Drafts. Each text message box may be viewed separately, or together in any combination. Show Inbox messages: While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE Softkey, then select the INBOX Softkey (Figure 8-104). Or: 1) Press the MENU Key to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Show Inbox Messages’. 3) Press the ENT Key. The message box selected for viewing is indicated at the bottom left of the list window. Figure 8-104 Text Message Inbox Show Outbox messages: While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE Softkey, then select the OUTBOX Softkey. Or: 1) Press the MENU Key to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Show Outbox Messages’. 3) Press the ENT Key. The message box selected for viewing is indicated at the bottom left of the list window. 634 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Show Draft messages: While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE Softkey, then select the DRAFTS Softkey. Or: 1) Press the MENU Key to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Show Draft Messages’. 3) Press the ENT Key. The message box selected for viewing is indicated at the bottom left of the list window. MANAGING TEXT MESSAGES The viewed messages may be listed according to the date/time the message was sent or received, the type of message (read, unread, sent, unsent, etc.), or by message address. Viewing messages sorted by message date/time: While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE Softkey, then select the TIME Softkey (Figure 8-104). Or: 1) Press the MENU Key to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Sort By Date/Time’. 3) Press the ENT Key. The sorting selection is indicated at the bottom center of the list window (Figure 8-104). Viewing messages sorted by message type: While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE Softkey, then select the TYPE Softkey. Or: 1) Press the MENU Key to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Sort By Type’. 3) Press the ENT Key. The sorting selection is indicated at the bottom center of the list window. Viewing messages sorted by address: While viewing the AUX-TEXT MESSAGING Page, select the ARRANGE Softkey, then select the ADDRESS Softkey. Or: 1) Press the MENU Key to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Sort By Address’. 3) Press the ENT Key. The sorting selection is indicated at the bottom center of the list window. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 635 ADDITIONAL FEATURES Viewing the content of a text message: 1) While viewing the AUX-TEXT MESSAGING Page, select the desired message box. 2) Press the FMS Knob to activate the cursor. 3) Turn either FMS Knob to select the desired message. 4) Select the VIEW Softkey. Or: Press the ENT Key. Or: a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘View Selected Message’. c) Press the ENT Key. Message content is displayed as shown in Figure 8-105. Figure 8-105 Viewing Message Content 5) To close the text message, select the CLOSE Softkey. Or: a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Close Message’. c) Press the ENT Key. 636 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Marking selected message as read: 1) While viewing the Inbox on the AUX-TEXT MESSAGING Page, press the FMS Knob to activate the cursor. 2) Turn either FMS Knob to select the desired message. 3) Select the MRK READ Softkey. Or: a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Mark Selected Message As Read’. c) Press the ENT Key. The message symbol now indicates the message has been opened. Marking all messages as read: 1) While viewing the Inbox on the AUX-TEXT MESSAGING Page, press the MENU Key to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Mark All New Messages As Read’. 3) Press the ENT Key. A confirmation window is displayed. 4) With cursor highlighting ‘YES’, press the ENT Key. The message symbols now indicate all the message have been opened. Delete a message: 1) While viewing the Inbox on the AUX-TEXT MESSAGING Page, press the FMS Knob to activate the cursor. 2) Turn either FMS Knob to select the desired message. 3) Select the DELETE Softkey. Or: a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Delete Selected Message’. c) Press the ENT Key. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 637 ADDITIONAL FEATURES 8.7 WI-FI CONNECTIONS The optional GDL 59 Data Link provides a Wi-Fi data link between the aircraft and a ground computer network. Wi-Fi connections are used for transferring maintenance log data to the aircraft manufacturer. The system can connect to a IEEE 802.11g compatible network provided the aircraft is on the ground and located within range of a network. The system is capable of WEP64, WEP128,WPA-PSK, and WPA2-PSK encryption formats. WPAEnterprise and WPA2-Enterprise are not supported. Connections that require web proxies, captive portals, or other elements that require user credentials, including a username and password or a redemption or access code; or require action such as accepting a user agreement, are not supported. Control and monitoring of Wi-Fi functions are accomplished through the AUX-WI-FI SETUP Page. Viewing the Wi-Fi Setup Page: 1) Turn the large FMS Knob on the MFD to select the AUX page group. 2) Turn the small FMS Knob to select DATA LINK. The AUX-WI-FI SETUP Page is now displayed. Setting up a new Wi-Fi connection: 1) Select the AVAIL Softkey on the MFD. A list of available networks will be displayed in the AVAILABLE NETWORKS window as shown in Figure 8-106. Signal strength is shown for each network, as well as security methods and whether the network has been saved in the system’s memory. Figure 8-106 Available Wi-Fi Networks 2) If necessary, select the RESCAN Softkey to have the system scan again for available networks. Or: a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Rescan Available Networks’. c) Press the ENT Key. 638 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES 3) Press the FMS Knob to place the cursor in the list of networks. 4) Turn either FMS Knob to select the desired network. See Figure 8-107. Figure 8-107 Desired Network Selected 5) Select the CONNECT Softkey. Or: a) Press the MENU Key to display the Page Menu. b) Turn either FMS Knob to place the cursor on ‘Connect To Selected Network’. c) Press the ENT Key. 6) If the network is secured, a window similar to Figure 8-108 will be displayed in order to enter the necessary passcode. Use the FMS Knobs to enter the desired alpha numeric characters. Select the CAP LOCK Softkey to enter upper case letters. If there is no security associated with the network, proceed to step 9. Figure 8-108 Enter Security Code 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 639 ADDITIONAL FEATURES 7) Press the ENT Key. ‘OK’ will be highlighted. 8) Press the ENT Key again. 9) The SAVE SETTINGS window is now displayed with the cursor highlighting ‘SAVE CONNECTION’. Figure 8-109 Save Option 10) The selected network can be saved to system memory to make re-connection easier at a later time. Connecting the selected network without saving: a) Turn the large FMS Knob to move the cursor to highlight ‘CONNECT’. b) Press the ENT Key. Saving and connecting the selected network: a) Press the ENT Key. A checkmark is placed in the checkbox and the cursor moves to the airport field as shown in Figure 8-110. b) Using the FMS Knobs, enter an airport identifier to be associated with the saved network. This aids in identifying the network later in the event of duplicate network names. c) Press the ENT Key. The cursor moves to ‘CONNECT’. d) Press the ENT Key again to connect to the selected network. Figure 8-110 Save Connection 640 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Editing a saved network: 1) While viewing list of saved networks, press the FMS Knob to activate the cursor as seen in Figure 8-111. 2) Turn either FMS Knob to highlight the network to be edited. 3) Pressing the ENT Key at this point will check or uncheck the AUTO CONNECT checkbox. When a checkmark is present, the system will automatically connect to the network when within range. Figure 8-111 Select Network to be Edited 4) Select the EDIT Softkey. The cursor now appears in the CONNECTION SETTINGS window as shown in Figure 8-112. Figure 8-112 Select Attributes to Edit 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 641 ADDITIONAL FEATURES 5) Turn the large FMS Knob to select the network attribute to be edited. 6) Turn the small FMS Knob to begin editing the field. 7) When the entry is complete, press the ENT Key. 8) Turn the large FMS Knob or press the ENT Key until ‘SAVE’ is highlighted. 9) Press the ENT Key. Disconnecting a Wi-Fi network: Select the DISCNCT Softkey. Or: 1) Press the MENU Key to display the Page Menu. 2) Turn either FMS Knob to place the cursor on ‘Disconnect From Network’. 3) Press the ENT Key. Deleting a saved Wi-Fi network: 1) While viewing the list of saved networks, press the FMS Knob to activate the cursor. 2) Turn either FMS Knob to highlight the network to be deleted. 3) Select the DELETE Softkey. The selected network is removed from the list. 642 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES 8.8 MAINTENANCE LOGS The system provides recording of CAS, CMC, exceedances, and other critical aircraft data that occur while the aircraft is on the ground or in flight. This information may be used by aircraft maintenance personnel in determining specific maintenance requirements. The Maintenance Logs feature is accessible by entering a password. No pilot action is required. Viewing the Maintenance Logs Page: 1) Turn the large FMS Knob on the MFD to select the AUX page group. 2) Turn the small FMS Knob to select ‘MAINTENANCE LOG’, as seen in Figure 8-113. The AUX-MAINTENANCE LOGS Page is now displayed. Figure 8-113 Maintenance Logs Page 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 643 ADDITIONAL FEATURES 3) Select the PSWD Key to enter the password, as shown in Figure 8-114. 4) Enter the password. 5) Press the ENT Key to access the page. Figure 8-114 Maintenance Logs Page 644 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES 8.9 SIRIUSXM SATELLITE RADIO ENTERTAINMENT NOTE: Refer to the Hazard Avoidance Section for information about SiriusXM Weather products. The optional SiriusXM Satellite Radio entertainment feature of the GDL 69A Data Link Receiver is available for the pilot’s and passengers’ enjoyment. The GDL 69A can receive SiriusXM Satellite Radio entertainment services at any altitude throughout the Continental U.S. Entertainment audio is not available on the GDL 69 Data Link Receiver. SiriusXM Satellite Radio offers a variety of radio programming over long distances without having to constantly search for new stations. Based on signals from satellites, coverage far exceeds land-based transmissions. SiriusXM Satellite Radio services are subscription-based. For more information on specific service packages, visit www.siriusxm.com. ACTIVATING SIRIUSXM SATELLITE RADIO SERVICES The service is activated by providing SiriusXM Satellite Radio with either one or two coded IDs, depending on the equipment. Either the Audio Radio ID or the Data Radio ID, or both, must be provided to SiriusXM Satellite Radio to activate the entertainment subscription. It is not required to activate both the entertainment and weather service subscriptions with the GDL 69A. Either or both services can be activated. SiriusXM Satellite Radio uses one or both of the coded IDs to send an activation signal that, when received by the GDL 69A, allows it to play entertainment programming. These IDs are located: • On the label on the back of the Data Link Receiver • On the XM Information Page on the MFD (Figure 8-115) • On the XM Satellite Radio Activation Instructions included with the unit (available at www.garmin.com, P/N 190-00355-04) Contact the installer if the Data Radio ID and the Audio Radio ID cannot be located. NOTE: The LOCK Softkey on the XM Information Page (Auxiliary Page Group) is used to save GDL 69A activation data when the SiriusXM services are initially set up. It is not used during normal SiriusXM Satellite Radio operation, but there should be no adverse effects if inadvertently selected during flight. Refer to the GDL 69/69A XM Satellite Radio Activation Instructions (190-00355-04, Rev K or later) for further information. Activating the SiriusXM Satellite Radio services: 1) Contact SiriusXM Satellite Radio. Follow the instructions provided by SiriusXM Satellite Radio services. 2) Turn the large FMS Knob to select the AUX Page Group. 3) Turn the small FMS Knob to select XM RADIO. 4) Select the INFO Softkey to display the XM Information Page. 5) Verify that the desired services are activated. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 645 ADDITIONAL FEATURES 6) Select the LOCK Softkey. 7) Turn the large FMS Knob to highlight YES. 8) To complete activation, press the ENT Key. Data Radio ID Audio Radio ID Weather Products Window LOCK Softkey is Used to Save Activation Data During Initial Setup RADIO and INFO Softkeys Figure 8-115 XM Information Page If SiriusXM Weather services have not been activated, the weather product boxes will appear empty on the XM Information Page and a yellow Activation Required message is displayed in the center of the Weather Data Link Page (Map Page Group). The Service Class refers to the groupings of weather products available for subscription. 646 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES USING SIRIUSXM SATELLITE RADIO The XM Radio Page provides information and control of the audio entertainment features of the SiriusXM Satellite Radio. Selecting the XM Radio Page: 1) Turn the large FMS Knob to select the AUX Page Group. 2) Turn the small FMS Knob to select XM RADIO. 3) Select the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled. Active Channels Channel List Categories Field Figure 8-116 XM Radio Page ACTIVE CHANNEL AND CHANNEL LIST The Active Channel Box on the XM Radio Page displays the currently selected channel that the SiriusXM Radio is using. The Channels List Box of the XM Radio Page shows a list of the available channels for the selected category. Channels can be stepped through one at a time or may be selected directly by channel number. Selecting a channel from the channel list: 1) While on the XM Radio Page, select the CHNL Softkey. 2) Select the CH + Softkey to go up through the list in the Channel Box, or move down the list with the CH – Softkey. Or: 1) Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels. 2) Press the ENT Key to activate the selected channel. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 647 ADDITIONAL FEATURES Selecting a channel directly: 1) While on the XM Radio Page, select the CHNL Softkey. 2) Select the DIR CH Softkey. The channel number in the Active Channel Box is highlighted. 3) Select the numbered softkeys located on the bottom of the display to directly select the desired channel number. 4) Press the ENT Key to activate the selected channel. CATEGORY The Category Box of the XM Radio Page displays the currently selected category of audio. Categories of channels such as jazz, rock, or news can be selected to list the available channels for a type of music or other contents. One of the optional categories is PRESETS to view channels that have been programmed. Selecting a category: 1) Select the CATGRY Softkey on the XM Radio Page. 2) Select the CAT + and CAT - Softkeys to cycle through the categories. Or: Turn the small FMS Knob to display the Categories list. Highlight the desired category with the small FMS Knob and press the ENT Key. Selecting All Categories places all channels in the list. Figure 8-117 Categories List PRESETS Up to 15 channels from any category can be assigned a preset number. The preset channels are selected by selecting the PRESETS and MORE Softkeys. Then the preset channel can be selected directly and added to the channel list for the Presets category. 648 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Setting a preset channel number: 1) On the XM Radio Page, while listening to an Active Channel that is wanted for a preset, select the PRESETS Softkey to access the first five preset channels (PS1 - PS5). 2) Select the MORE Softkey to access the next five channels (PS6 – PS10), and again to access the last five channels (PS11 – PS15). Selecting the MORE Softkey repeatedly cycles through the preset channels. 3) Select any one of the (PS1 - PS15) softkeys to assign a number to the active channel. 4) Select the SET Softkey on the desired channel number to save the channel as a preset. Press PRESETS to Access the Preset Channels Softkeys Press MORE to Cycle Through the Preset Channels Press SET to Save Each Preset Channel Figure 8-118 Accessing and Selecting Preset SiriusXM Channels Selecting the BACK Softkey, or 45 seconds of softkey inactivity, returns the system to the top level softkeys. VOLUME Radio volume is shown as a percentage. Volume level is controlled by selecting the VOL Softkey, which brings up the MUTE Softkey and the volume increase and decrease softkeys. Adjusting the volume: 1) With the XM Radio Page displayed, press the VOL Softkey. 2) Press the VOL – Softkey to reduce volume or press the VOL + Softkey to increase volume. (Once the VOL Softkey is pressed, the volume can also be adjusted using the small FMS Knob.) Figure 8-119 Volume Control Radio volume may also be adjusted at each passenger station. Mute SiriusXM audio: 1) Select the XM Radio Page or XM Information Page. 2) Press the MUTE Softkey to mute the audio. Press the MUTE Softkey again to unmute the audio. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 649 ADDITIONAL FEATURES 8.10 SCHEDULER The Scheduler feature can be used to enter and display reminder messages (e.g., Hot Section Inspection or Phase 1 Maintenance Check) in the Messages Window on the PFD. Messages can be set to display based on a specific date and time (event), once the message timer reaches zero (one-time; default setting), or recurrently whenever the message timer reaches zero (periodic). Message timers set to periodic alerting automatically reset to the original timer value once the message is displayed. When power is cycled, all messages are retained until deleted, and message timer countdown is resumed. Figure 8-120 Scheduler (Utility Page) Entering a scheduler message: 1) Select the AUX - Utility Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the first empty scheduler message naming field. 4) Use the FMS Knob to enter the message text to be displayed in the Messages Window and press the ENT Key. 5) Press the ENT Key again or use the large FMS Knob to move the cursor to the field next to Type. 6) Turn the small FMS Knob to select the message type: • Event—Message issued at the specified date/time • One-time—Message issued when the message timer reaches zero (default setting) • Periodic—Message issued each time the message timer reaches zero 7) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field. 8) For periodic and one-time message, use the FMS Knob to enter the timer value (HH:MM:SS) from which to countdown and press the ENT Key. 650 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES 9) For event-based messages: a) Use the FMS Knob to enter the desired date (DD-MM-YY) and press the ENT Key. b) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field. c) Use the FMS Knob to enter the desired time (HH:MM) and press the ENT Key. 10) Press the ENT Key again or use the large FMS Knob to move the cursor to enter the next message. Deleting a scheduler message: 1) Select the AUX - Utility Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the name field of the scheduler message to be deleted. 4) Press the CLR Key to clear the message text. If the CLR Key is pressed again, the message is restored. 5) Press the ENT Key while the message line is cleared to clear the message text. Scheduler messages appear in the Messages Window on the PFD. When a scheduler message is waiting, the MSG Softkey label flashes. Selecting the MSG Softkey opens the Messages Window and acknowledges the scheduler message. Selecting the MSG Softkey again removes the Messages Window from the display, and the scheduler message is deleted from the message queue. Figure 8-121 PFD Messages Window 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 651 ADDITIONAL FEATURES 8.11 ELECTRONIC CHECKLISTS NOTE: The optional checklists presented here are for example only and may differ from checklists available for the Phenom 100. The information described in this section is not intended to replace the checklist information described in the POH. NOTE: Garmin is not responsible for the content of checklists. Checklists are created by the aircraft manufacturer. Modifications or updates to the checklists are coordinated through the aircraft manufacturer. The user cannot edit these checklists. The optional checklist functions are displayed on two levels of softkeys that are available on any MFD page. (Optional) SYSTEM CPDLC SYSTEM CPDLC MAP DCLTR SHW CHRT CHKLIST EXIT CHECK EMERGCY The CHECK Softkey label changes to UNCHECK when the checklist item is already checked. Figure 8-122 Checklist Softkeys The MFD is able to display optional electronic checklists which allow the pilot to quickly find the proper procedure on the ground and during each phase of flight. The system accesses the checklists from an SD card inserted into the top card slot of the MFD. If the SD card contains an invalid checklist file or no checklist, the Power-up Page messages display ‘Checklist File: Invalid’ or ‘Checklist File: N/A’ (not available) and the CHKLIST Softkey is not available. The following colors are used for checklist items: • Light Blue - Items not selected or checked • White - Item is selected • Green - Item has been checked • Gray - General notes • Yellow - Caution notes • Red - Warning notes Accessing and navigating checklists: 1) From any page on the MFD, select the CHKLIST Softkey or turn the large FMS Knob to select the Checklist Page. 2) Turn the large FMS Knob to select the ‘GROUP’ field. 3) Turn the small FMS Knob to select the desired procedure and press the ENT Key. 4) Turn the large FMS Knob to select the ‘CHECKLIST’ field. 5) Turn the small FMS Knob to select the desired checklist and press the ENT Key. The selected checklist item is indicated with white text surrounded by a white box. 6) Press the ENT Key or select the CHECK Softkey to check the selected checklist item. The line item turns green and a checkmark is placed in the associated box. The next line item is automatically selected for checking. Either FMS Knob can be used to scroll through the checklist and select the desired checklist item. 652 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES Press the CLR Key or select the UNCHECK Softkey to remove a check mark from an item. 7) When all checklist items have been checked, ‘*Checklist Finished*’ is displayed in green text at the bottom left of the checklist window and ‘GO TO NEXT CHECKLIST?’ is highlighted. If ‘GO TO NEXT CHECKLIST?’ is selected prior to checking all the checklist items, ‘*CHECKLIST NOT FINISHED*’ will be displayed in yellow text. 8) Press the ENT Key. If ‘GO TO NEXT CHECKLIST?’ is displayed when pressing the ENT Key, the next checklist in the group will be displayed. If ‘EXIT CHECKLISTS?’ is displayed when pressing the ENT Key, the system will exit the Checklist Page. 9) Select the EXIT Softkey to exit the Checklist Page and return to the page last viewed. When returning to the Checklist Page after pressing the EXIT Softkey, the system will return to the last selected checklist item. Figure 8-123 Sample Checklist Accessing emergency procedures: 1) From any page on the MFD, select the CHKLIST Softkey or turn the large FMS Knob to select the Checklist Page. 2) Select the EMERGCY Softkey. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 653 ADDITIONAL FEATURES 3) Turn the FMS Knob to select the desired emergency checklist and press the ENT Key. 4) Press the ENT Key or select the CHECK Softkey to check the selected emergency checklist item. The line item turns green and a checkmark is placed in the box next to it. The next line item is automatically highlighted for checking. Either FMS Knob can be used to scroll through the checklist and select the desired checklist item. Press the CLR Key or select the UNCHECK Softkey to remove a check mark from an item. 5) When all checklist items have been checked, ‘*Checklist Finished*’ is displayed in green text at the bottom left of the checklist window and ‘GO TO NEXT CHECKLIST?’ is highlighted. If ‘GO TO NEXT CHECKLIST?’ is selected prior to checking all the checklist items, ‘*CHECKLIST NOT FINISHED*’ will be displayed in yellow text. 6) Press the ENT Key to advance to the next checklist. 7) Select the RETURN Softkey to return to the previous checklist. 8) Select the EXIT Softkey to exit the Checklist Page and return to the page last viewed. Figure 8-124 Emergency Checklist Page Example 654 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES 8.12 ABNORMAL OPERATION SVT TROUBLESHOOTING SVT is intended to be used with traditional attitude, heading, obstacle, terrain, and traffic inputs. SVT is disabled when valid attitude or heading data is not available for the display. In case of invalid SVT data, the PFD display reverts to the standard blue-over-brown attitude display. SVT becomes disabled without the following data resources: • Attitude data • Heading data • GPS position data • 9 Arc-second Terrain data • Obstacle data • TAWS function is not available, in test mode, or failed • The position of the aircraft exceeds the range of the terrain database. REVERSIONARY MODE SVT can be displayed on the Multifunction Display (MFD) in Reversionary Mode. If it is enabled when switching to Reversionary Mode, SVT will take up to 30 seconds to be displayed. The standard, non-SVT PFD display will be shown in the interim. Figure 8-125 SVT Reversionary Mode 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 655 ADDITIONAL FEATURES UNUSUAL ATTITUDES Unusual attitudes are displayed with red chevrons overlaid on the display indicating the direction to fly to correct the unusual attitude condition. The display shows either a brown or blue colored bar at the top or bottom of the screen to represent earth or sky. This is intended to prevent losing sight of the horizon during extreme pitch attitudes. Figure 8-126 Unusual Attitude Display The blue colored bar is also displayed when terrain gradient is great enough to completely fill the display. Blue Band Terrain Completely Fills Display Figure 8-127 Blue Sky Bar with Full Display Terrain 656 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A ADDITIONAL FEATURES GDL 69/69A DATA LINK RECEIVER TROUBLESHOOTING Some quick troubleshooting steps listed below can be performed to find the possible cause of a failure. • Ensure the owner/operator of the aircraft in which the Data Link Receiver is installed has subscribed to SiriusXM Satellite Radio • Ensure the SiriusXM subscription has been activated • Perform a quick check of the circuit breakers to ensure that power is applied to the Data Link Receiver • Ensure that nothing is plugged into the Music jack(s) because this would prevent SiriusXM Satellite Radio from being heard For troubleshooting purposes, check the LRU Information Box on the AUX - System Status Page for Data Link Receiver (GDL 69/69A) status, serial number, and software version number. If a failure has been detected in the GDL 69/69A the status is marked with a red X. Selecting the System Status Page: 1) Turn the large FMS Knob to select the AUX Page Group. 2) Turn the small FMS Knob to select the System Status Page (the last page in the AUX Page Group). Figure 8-128 LRU Information Window on System Status Page 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 657 ADDITIONAL FEATURES If a failure still exists, the following messages may provide insight as to the possible problem: Message Message Location CHECK ANTENNA XM Information Page (MFD) UPDATING XM Information Page (MFD)) NO SIGNAL XM Information Page Weather Datalink Page Loss of signal; signal strength too low for (MFD) receiver LOADING XM Radio Page (MFD) Acquiring channel audio or information OFF AIR XM Radio Page (MFD) Channel not in service -------- XM Radio Page (MFD) WEATHER DATA LINK FAILED Weather Datalink Page (MFD) ACTIVATION REQUIRED XM Information Page (MFD) Missing channel information No communication from Data Link Receiver within last 5 minutes SiriusXM subscription is not activated DETECTING ACTIVATION Weather Datalink Page (MFD) WAITING FOR DATA... 658 Description Data Link Receiver antenna error; service required Data Link Receiver updating encryption code SiriusXM subscription is activating. SiriusXM subscription confirmed downloading Weather Datalink Page (MFD) weather data. Table 8-7 GDL 69/69A Data Link Receiver Messages Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX A ANNUNCIATIONS AND ALERTS CAS MESSAGES WARNING MESSAGES See the Airplane Flight Manual (AFM) for recommended pilot actions. Accompanied by a triple chime tone which repeats until acknowledged. Message CAB ALTITUDE HI DOOR EMER OPEN DOOR PAX OPEN E1 FIRE E2 FIRE E1 OIL LO PRES E2 OIL LO PRES ELEC EMERGENCY ELEC XFR FAIL LG LEVER DISAG NO TO CONFIG Description Cabin altitude pressure altitude high Emergency door open Passenger door open Fire in engine 1 Fire in engine 2 Low oil pressure in engine 1 Low oil pressure in engine 2 Generators offline Generators offline and electrical emergency transfer has failed Landing gear position and control lever disagreement No takeoff configuration CAUTION MESSAGES See the Airplane Flight Manual (AFM) for recommended pilot actions. Accompanied by a single chime tone which repeats until acknowledged. Message ADS 1 FAIL ADS 2 FAIL ADS 1 HTR FAIL ADS 2 HTR FAIL AHRS 1 FAIL AHRS 2 FAIL A-I E1 FAIL A-I E2 FAIL ANTI-SKID FAIL AP FAIL AP PITCH MISTRIM AP ROLL MISTRIM AUDIO PNL 1 FAIL AUDIO PNL 2 FAIL AURAL WRN FAIL AUTO PTRIM FAIL BATT DISCHARGE BATT 1 OFF BUS 190-00728-06 Rev. A Description ADS 1 offline or failed ADS 2 offline or failed Pitot heater 1 offline or heater element failed Pitot heater 2 offline or heater element failed AHRS 1 failure AHRS 2 failure Anti-ice system failue in engine 1 Anti-ice system failue in engine 2 Anti-skid function lost; main brake still available Loss of AP function Airplane mistrimmed in pitch axis when AP is engaged Airplane mistrimmed in roll axis when AP is engaged Audio panel 1 is offline Audio panel 2 is offline Aural warning system failure due to non-communicating LRUs Auto pitch trim failure; other pitch trim functions still available Battery discharging under normal operation Battery 1 offline Embraer Prodigy® Flight Deck 100 Pilot’s Guide 659 APPENDIX A Message Description BATT 2 OFF BUS Battery 2 offline BATT EXCEEDANCE Battery voltage has exceeded 29 VDC Bleed 1 system not under control BLEED 1 FAIL Bleed 2 system not under control BLEED 2 FAIL Bleed 1 hot air leakage at some region of the ducting BLEED 1 LEAK Bleed 2 hot air leakage at some region of the ducting BLEED 2 LEAK Main brake system lost BRK FAIL CAB DELTA-P FAIL Excessive cabin pressure differential CLUTCH PIT FAIL Slip clutch maintenance test failed CLUTCH ROL FAIL Slip clutch maintenance test failed CLUTCH YAW FAIL Slip clutch maintenance test failed CONFIG MDL FAIL Master Configuration Module failed or non-communicative D-I WINGSTB FAIL Deice system in wings and tail failure DOORBAG AFT OPEN Crew baggage door open DOORBAG FWD OPEN Forward baggage door open DUCT 1 OVERTEMP Duct 1 temperature over specified safe value DUCT 2 OVERTEMP Duct 2 temperature over specified safe value E1 CTRL FAULT Engine 1 responds slowly or not at all to thrust commands E2 CTRL FAULT Engine 2 responds slowly or not at all to thrust commands Uncommanded shutdown detected for engine 1 E1 FAIL Uncommanded shutdown detected for engine 2 E2 FAIL E1 FIRE DET FAIL Fire detection system failure in engine 1 E2 FIRE DET FAIL Fire detection system failure in engine 2 Fire extinguisher failure in engine 1 E1 FIREX FAIL Fire extinguisher failure in engine 2 E2 FIREX FAIL E1 FUEL IMP BYP Fuel filter impending bypass condition for engine 1 E2 FUEL IMP BYP Fuel filter impending bypass condition for engine 2 Thrust Lever Angle failure for engine 1 E1 TLA FAIL Thrust Lever Angle failure for engine 2 E2 TLA FAIL E1 TT0 HTR FAIL Heater failure in engine 1 E2 TT0 HTR FAIL Heater failure in engine 2 E1 TT0 PROBE ICE Engine 1 probe frozen E2 TT0 PROBE ICE Engine 2 probe frozen Electrical bay over temperature EBAY OVHT EMER BRK LO PRES Emergency accumulator pressure below 1800 psi. Few emergency brake functions available. ENG NO TO DATA No takeoff data entered Loss of flaps deployment or retraction FLAP FAIL FUEL 1 LO LEVEL Low fuel level in tank 1 FUEL 2 LO LEVEL Low fuel level in tank 2 FUEL 1 LO PRES Fuel pressure low in engine 1 feed line FUEL 2 LO PRES Fuel pressure low in engine 2 feed line FUEL 1 SOV FAIL Fuel feed SOV 1 closed or unavilable FUEL 2 SOV FAIL Fuel feed SOV 2 closed or unavilable FUEL IMBALANCE Fuel is imbalanced between the tanks 660 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX A Message FUEL OVERFILL FUEL XFR FAIL GEN 1 OFF BUS GEN 2 OFF BUS GEN OVLD GEN START FAULT GIA 1 FAIL GIA 2 FAIL GIA 1 OVHT GIA 2 OVHT HYD HI TEMP HYD LO PRES ICE CONDITION* LG WOW SYS FAIL MFD CONFIG MFD FAULT MFD OVHT OXY LO PRES PARK BRK NOT REL PAX OXY NO PRES PFD 1 CONFIG PFD 2 CONFIG PFD 1 FAULT PFD 2 FAULT PFD 1 OVHT PFD 2 OVHT PRESN AUTO FAIL PTRIM BKP FAIL PTRIM DISCONNECT PTRIM NML FAIL PUSHER FAIL PUSHER OFF STBY HTR FAIL SWPS FAIL SWPS FAULT SWPS HTR 1 FAIL SWPS HTR 2 FAIL SWPS UNTESTED TCAS FAIL* WSHLD 1 HTR FAIL WSHLD 2 HTR FAIL YD FAIL YD MISTRIM Description Fuel tank overfilled Fuel transfer failure Generator 1 offline Generator 2 offline Generator(s) overload Generator start fault Failure of GIA 1 Failure of GIA 2 GIA 1 over temperature GIA 2 over temperature Hydraulic temperature high Hydraulic pressure low Icing condition detected Landing gear weight-on-wheels system failure MFD configuration error Fault with the MFD MFD over temperature Oxygen system pressure low Parking brake not released Cabin altitude high and passenger oxygen system pressure low PFD 1 configuration error PFD 2 configuration error Fault with PFD 1 Fault with PFD 2 PFD 1 over temperature PFD 2 over temperature Pressurization controller failure Loss of backup pitch trim actuator Pitch trim disconnected Loss of normally-operating pitch trim actuator Stall Warning & Protection System pusher has failed Stall Warning Pusher is off Failure of standby heater Stall Warning & Protection System inoperative Stall Warning & Protection System activation angles anticipated to conservative settings Stall Warning & Protection System heater 1 failure Stall Warning & Protection System heater 2 failure Stall Warning & Protection System has not been tested TCAS I or TCAS II is unavailable Windshield 1 heater failure Windshield 2 heater failure Loss of yaw damper function Airplane mistrimmed in yaw axis when YD is engaged * Optional 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 661 APPENDIX A ADVISORY MESSAGES See the Airplane Flight Manual (AFM) for recommended pilot actions. Message A-I E1 ON A-I E2 ON ADS 1 HTR FAULT ADS 2 HTR FAULT ADS-AOA HTR ON AHRS 1 FAULT AHRS 2 FAULT AUDIO PNL1 FAULT AUDIO PNL2 FAULT AURAL WRN FAULT ATC DLK FAIL* AVNX FAN FAIL BLEED 1 OFF BLEED 2 OFF CLUTCH PIT PASS CLUTCH PIT PROG CLUTCH ROL PASS CLUTCH ROL PROG CLUTCH YAW PASS CLUTCH YAW PROG DC BUS 1 OFF DC BUS 2 OFF D-I WINGSTB ON E1 CHIP DETECTED E2 CHIP DETECTED E1 FADEC FAULT E2 FADEC FAULT ELEC SYS FAULT EMER BUS OFF ENG EXCEEDANCE ENG FIREX DISCH ENG NO DISPATCH FLAP NOT AVAIL FUEL EQUAL FUEL1 FEED FAULT FUEL2 FEED FAULT FUEL 1 PSW FAIL FUEL 2 PSW FAIL FUEL PUMP 1 FAIL 662 Description De-ice system on in engine 1 De-ice system on in engine 2 Fault in ADS 1 heater Fault in ADS 2 heater ADS-AOA probe switch is on Fault with AHRS 1 Fault with AHRS 2 Fault with audio panel 1 Fault with audio panel 2 Partial loss of aural warning function CPDLC system has failed Avionics fan failure Bleed pressure regulator 1 and shut-off valve closed Bleed pressure regulator 2 and shut-off valve closed Pitch slip clutch maintenance test passed Pitch slip clutch maintenance test in progress Roll slip clutch maintenance test passed Roll slip clutch maintenance test in progress Yaw slip clutch maintenance test passed Yaw slip clutch maintenance test in progress DC bus 1 offline DC bus 2 offline Deice system in wings and tail ON Chip detected by engine 1 oil chip detector Chip detected by engine 2 oil chip detector FADEC fault in engine 1 FADEC fault in engine 2 Electrical system fault Emergency bus OFF Limit exceeded in engine(s) during flight Engine fire extinguisher discharge FADEC detected no dispatch fault condition in engine(s) Flaps not available Fuel quantity asymmetry corrected; XFEED SOV is open DC pump on due to low fuel pressure DC pump on due to low fuel pressure Fuel pressure switch stuck in “high” position Fuel pressure switch stuck in “high” position Fuel pump 1 failure Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX A Message FUEL PUMP 2 FAIL GEA 1 FAIL GEA 2 FAIL GEA 3 FAIL GND SPLR OPEN* GPU CONNECTED GSD FAIL HSDB FAULT HSDB SW REV POS ICE DET FAIL* MFD FAN FAIL OXY SW NOT AUTO PFD 1 FAN FAIL PFD 2 FAN FAIL PTRIM SW1 FAIL PTRIM SW2 FAIL RALT FAIL* RAM AIR FAIL SHED BUS OFF SPDBRK SW DISAG* SPOILER FAULT* SWPS ICE SPEED Description Fuel pump 2 failure Failure of GEA 1 Failure of GEA 2 Failure of GEA 3 The spoiler panels are open in flight without any command for doing so Ground power unit connected to the aircraft GSD non-communicative An LRU has stopped communicating over an HSDB HSDB switch in reversionary position Failure of the ice detection system Failure of MFD fan Oxygen system switch in manual mode Failure of PFD 1 fan Failure of PFD 2 fan Failure of pilot pitch trim switch Failure of copilot pitch trim switch Radar altitude failure Ram air valve failure Shed bus off Speed brake switch is in "OPEN" in an unauthorized flight condition Ground Spoiler arm logic failed Ground Spoiler command disagree Spoiler position disagree Ground Spoiler Control Valve failed Speed brake command failed Speed brake command inhibit failed Stall Warning System activation angles anticipated due to ice conditions * Optional COMPARATOR ANNUNCIATIONS The Comparator monitors critical values generated by redundant sensors. If differences in the sensors exceed a specified amount, this discrepancy will be annunciated in the Comparator Window as a ‘MISCOMP’ (miscompare) as seen in Figure A-1. Note that operating the system in the vicinity of metal buildings or other metal structures can cause sensor differences that may result in nuisance miscompare annunciations during start up, shut down, or while taxiing. If one or both of the sensed values are unavailable, it will be annunciated as a ‘NO COMP’ (no compare). The following is a list of the possible annunciations: 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 663 APPENDIX A Comparator Window Figure A-1 Sensor Comparator Window Comparator Window Text Condition Difference in altitude sensors is > 200 ft. ALT MISCOMP If both airspeed sensors detect < 35 kts, this is inhibited. IAS MISCOMP If either airspeed sensor detects > 35 kts, and the difference in sensors is > 15 kts. If either airspeed sensor detects > 80 kts, and the difference in sensors is > 10 kts. HDG MISCOMP Difference in heading sensors is > 10º. PIT MISCOMP Difference in pitch sensors is > 5º. ROL MISCOMP Difference in roll sensors is > 6º. ALT NO COMP No data from one or both altitude sensors. IAS NO COMP No data from one or both airspeed sensors. HDG NO COMP No data from one or both heading sensors. PIT NO COMP No data from one or both pitch sensors. ROL NO COMP No data from one or both roll sensors.. REVERSIONARY SENSOR ANNUNCIATIONS Reversionary sensor selection is annunciated in the Reversionary Sensor Window, as shown in Figure A-2. These annunciations reflect reversionary sensors selected on one or both PFDs. Pressing the SENSOR Softkey gives access to ADC1, ADC2, ADCSTBY, AHRS1, AHRS2, and ATTSTBY Softkeys. These softkeys allow manual switching of sensors. In the case of certain types of sensor failures, the system may make some sensor selections automatically. The GPS sensor cannot be switched manually. 664 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX A Reversionary Sensor Window Figure A-2 Reversionary Sensor Windows Reversionary Sensor Window Text BOTH ON ADC1 BOTH ON ADC2 BOTH ON ADCSTBY BOTH ON AHRS1 BOTH ON AHRS2 BOTH ON ATTSTBY BOTH ON GPS1 BOTH ON GPS2 USING ADC1 USING ADC2 USING ADCSTBY USING AHRS1 USING AHRS2 USING ATTSTBY USING GPS1 USING GPS2 Condition Both PFDs are displaying data from the #1 Air Data Computer. Both PFDs are displaying data from the #2 Air Data Computer. Both PFDs are displaying data from the standby air data input. Both PFDs are displaying data from the #1 AHRS. Both PFDs are displaying data from the #2 AHRS. Both PFDs are displaying data from the standby attitude and heading reference input. Both PFDs are displaying data from the #1 GPS receiver. Both PFDs are displaying data from the #2 GPS receiver. PFD2 is displaying data from the #1 Air Data Computer. PFD1 is displaying data from the #2 Air Data Computer. PFD1 or PFD2 is displaying data from the standby air data input. PFD2 is displaying data from the #1 AHRS. PFD1 is displaying data from the #2 AHRS. PFD1 or PFD2 is displaying data from the standby attitude and heading reference input. PFD2 is displaying data from the #1 GPS. PFD1 is displaying data from the #2 GPS. PRODIGY® SYSTEM ANNUNCIATIONS When a new message is issued, the MSG Softkey will flash to alert the flight crew of a new message. It will continue to flash until acknowledged by pressing the softkey. Active messages are displayed in white text. Messages that have become inactive will change to gray text. The MSG Softkey will flash if the state of a displayed message changes or a new message is displayed. The inactive messages can be removed from the Message Window by pressing the flashing MSG Softkey. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 665 APPENDIX A Messages are conveyed to the flight crew regarding problems with the system. Typically, a large red “X” appears in a window when a related LRU fails or detects invalid data. When an LRU or an LRU function fails, a large red “X” is typically displayed on windows associated with the failed data. The following section describes various system annunciations. Refer to the AFM for additional information regarding pilot responses to these annunciations. NOTE: Upon power-up of the system, certain windows remain invalid as equipment begins to initialize. All windows should be operational within one minute of power-up. Should any window continue to remain flagged, the system should be serviced by a Garmin-authorized repair facility. System Annunciation Red ‘X’ Messages Window Figure A-3 System Messages 666 Message Softkey Annunciation Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX A GIA 63W Integrated Avionics Units GIA 63W Integrated Avionics Units GDC 74B Air Data Computer FADEC GRS 77 AHRS Or GMU 44 Magnetometer GEA 71 Engine Airframe Unit KRA 405B Radar Altimeter or GIA 63W Integrated Avionics Units Pressure Controller GEA 71 Engine Airframe Unit & GSD 71 Data Concentrator GIA 63W Integrated Avionics Units & GEA 71 Engine Airframe Unit GIA 63W Integrated Avionics Units FADEC GTX 33/D Transponder Or GIA 63W Integrated Avionics Units GDC 74B Air Data Computer Figure A-4 System Failure Annunciations System Annunciation Comment Attitude and Heading Reference System is aligning. Display system is not receiving attitude information from the AHRS. Indicates a configuration module failure. Display system is not receiving airspeed input from air data computer. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 667 APPENDIX A System Annunciation Comment Display system is not receiving valid heading input from AHRS. System is not receiving valid heading input from GMU, but is receiving GPS-derived track information. Display system is not receiving altitude input from the air data computer. Display system is not receiving vertical speed input from the air data computer. Display system is not receiving valid transponder information. GPS information is either not present or is invalid for navigation use. Note that AHRS utilizes GPS inputs during normal operation. AHRS operation may be degraded if GPS signals are not present (see AFM). Other Various Red X Indications 668 A red “X” through any other display field (such as engine instrumentation display) indicates that the field is not receiving valid data. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX A PRODIGY® SYSTEM MESSAGE ADVISORIES NOTE: This Section provides information regarding message advisories that may be displayed by the system. Knowledge of the aircraft, systems, flight conditions, and other existing operational priorities must be considered when responding to a message. Always use sound pilot judgment. The Phenom 100 Airplane Flight Manual (AFM) takes precedence over any conflicting guidance found in this section. This section describes various system message advisories. Certain messages are issued due to an LRU or an LRU function failure. Such messages are normally accompanied by a corresponding red “X” annunciation as shown previously in the Prodigy® System Annunciation section. MFD & PFD MESSAGE ADVISORIES Message DATA LOST – Pilot stored data was lost. Recheck settings. XTALK ERROR – A flight display crosstalk error has occurred. PFD1 SERVICE – PFD1 needs service. Return unit for repair. PFD2 SERVICE – PFD2 needs service. Return unit for repair. MFD1 SERVICE – MFD1 needs service. Return unit for repair. MANIFEST – PFD1 software mismatch, communication halted. MANIFEST – PFD2 software mismatch, communication halted. MANIFEST – MFD1 software mismatch, communication halted. PFD1 CONFIG – PFD1 config error. Config service req’d. PFD2 CONFIG – PFD2 config error. Config service req’d. MFD1 CONFIG – MFD1 config error. Config service req’d. SW MISMATCH – GDU software version mismatch. Xtalk is off. PFD1 COOLING – PFD1 has poor cooling. Reducing power usage. PFD2 COOLING – PFD2 has poor cooling. Reducing power usage. MFD1 COOLING – MFD1 has poor cooling. Reducing power usage. 190-00728-06 Rev. A Comments The pilot profile data was lost. System reverts to default pilot profile and settings. The pilot may reconfigure the MFD & PFDs with preferred settings, if desired. The MFD and PFDs are not communicating with each other. The system should be serviced. The PFD and/or MFD self-test has detected a problem. The system should be serviced. The PFD and/or MFD has incorrect software installed. The system should be serviced. The PFD configuration settings do not match backup configuration memory. The system should be serviced. The MFD configuration settings do not match backup configuration memory. The system should be serviced. The MFD and PFDs have different software versions installed. The system should be serviced. The PFD and/or MFD is overheating and is reducing power consumption by dimming the display. If problem persists, the system should be serviced. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 669 APPENDIX A Message PFD1 KEYSTK – PFD1 [key name] Key is stuck. PFD2 KEYSTK – PFD2 [key name] Key is stuck. MFD1 KEYSTK – MFD [key name] Key is stuck. CNFG MODULE – PFD1 configuration module is inoperative. PFD1 VOLTAGE – PFD1 has low voltage. Reducing power usage PFD2 VOLTAGE – PFD2 has low voltage. Reducing power usage MFD1 VOLTAGE – MFD1 has low voltage. Reducing power usage Comments A key is stuck on the PFD and/or MFD bezel. Attempt to free the stuck key by pressing it several times. The system should be serviced if the problem persists. The PFD1 configuration module backup memory has failed. The system should be serviced. The PFD1 voltage is low. The system should be serviced. The PFD2 voltage is low. The system should be serviced. The MFD voltage is low. The system should be serviced. DATABASE MESSAGE ADVISORIES Message MFD1 DB ERR – MFD1 navigation database error exists. PFD1 DB ERR – PFD1 navigation database error exists. PFD2 DB ERR – PFD2 navigation database error exists. MFD1 DB ERR – MFD1 navigation database error exists. PFD1 DB ERR – PFD1 navigation database error exists. PFD2 DB ERR – PFD2 navigation database error exists. MFD1 DB ERR – MFD1 basemap database error exists. PFD1 DB ERR – PFD1 basemap database error exists. PFD2 DB ERR – PFD2 basemap database error exists. MFD1 DB ERR – MFD1 navigation database error exists. PFD1 DB ERR – PFD1 navigation database error exists. PFD2 DB ERR – PFD2 navigation database error exists. 670 Comments The MFD and/or PFD detected a failure in the navigation database. Attempt to reload the navigation database. If problem persists, the system should be serviced. The MFD and/or PFD detected a failure in the navigation database. Attempt to reload the navigation database. If problem persists, the system should be serviced. The MFD and/or PFD detected a failure in the basemap database. The MFD and/or PFD detected a failure in the navigation database. Attempt to reload the navigation database. If problem persists, the system should be serviced. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX A Message MFD1 DB ERR – MFD1 basemap database error exists. PFD1 DB ERR – PFD1 basemap database error exists. PFD2 DB ERR – PFD2 basemap database error exists. MFD1 DB ERR – MFD1 obstacle database missing. PFD1 DB ERR – PFD1 obstacle database missing. PFD2 DB ERR – PFD2 obstacle database missing. MFD1 DB ERR – MFD1 airport terrain database error exists. PFD1 DB ERR – PFD1 airport terrain database error exists. PFD2 DB ERR – PFD2 airport terrain database error exists. MFD1 DB ERR – MFD1 airport terrain database missing. PFD1 DB ERR – PFD1 airport terrain database missing. PFD2 DB ERR – PFD2 airport terrain database missing. MFD1 DB ERR – MFD1 Safe Taxi database error exists. PFD1 DB ERR – PFD1 Safe Taxi database error exists. PFD2 DB ERR – PFD2 Safe Taxi database error exists. MFD1 DB ERR – MFD1 Chartview database error exists. MFD1 DB ERR – MFD1 FliteCharts database error exists. MFD1 DB ERR – MFD1 Airport Directory database error exists. DB MISMATCH – Navigation database mismatch. Xtalk is off. DB MISMATCH – Standby Navigation database mismatch. 190-00728-06 Rev. A Comments The MFD and/or PFD detected a failure in the basemap database. The obstacle database is present on another LRU, but is missing on the specified LRU. The MFD and/or PFD detected a failure in the airport terrain database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced. The airport terrain database is present on another LRU, but is missing on the specified LRU. The MFD and/or PFD detected a failure in the Safe Taxi database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced. The MFD detected a failure in the ChartView database (optional feature). Ensure the data card is properly inserted. Replace data card. If problem persists, system should be serviced. The MFD detected a failure in the FliteCharts database (optional feature). Ensure the data card is properly inserted. Replace data card. If problem persists, system should be serviced. The MFD detected a failure in the Airport Directory database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the system should be serviced. The PFDs and MFD have different navigation database versions or types (Americas, European, etc.) installed. Crossfill is off. Install correct navigation database version or type in all displays. The PFDs and MFD have different standby navigation database versions or types (Americas, European, etc.) installed. Install correct standby navigation database version or type in all displays. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 671 APPENDIX A Message DB MISMATCH – Terrain database mismatch. DB MISMATCH – Obstacle database mismatch. DB MISMATCH – Airport Terrain database mismatch. NAV DB UPDATED – Active navigation database updated. TERRAIN DSP – [PFD1, PFD2 or MFD1] Terrain awareness display unavailable. Comments The PFDs and MFD have different terrain database versions or types installed. Install correct terrain database version or type in all displays. The PFDs and MFD have different obstacle database installed. Install correct obstacle database in all displays. The PFDs and MFD have different airport terrrain databases installed. Install correct airport terrain database in all displays. System has updated the active navigation database from the standby navigation database. One of the terrain, airport terrain, or obstacle databases required for TAWS in the specified PFD or MFD is missing or invalid. GMA 1347D MESSAGE ADVISORIES Message GMA1 FAIL – GMA1 is inoperative. GMA2 FAIL – GMA2 is inoperative. GMA XTALK – GMA crosstalk error has occurred. GMA1 CONFIG – GMA1 config error. Config service req’d. GMA2 CONFIG – GMA2 config error. Config service req’d. MANIFEST – GMA1 software mismatch, communication halted. MANIFEST – GMA2 software mismatch, communication halted. GMA1 SERVICE – GMA1 needs service. Return unit for repair. GMA2 SERVICE – GMA2 needs service. Return unit for repair. Comments The audio panel self-test has detected a failure. The audio panel is unavailable. The system should be serviced. An error has occurred in transferring data between the two GMAs. The system should be serviced. The audio panel configuration settings do not match backup configuration memory. The system should be serviced. The audio panel has incorrect software installed. The system should be serviced. The audio panel self-test has detected a problem in the unit. Certain audio functions may still be available, and the audio panel may still be usable. The system should be serviced when possible. GIA 63W MESSAGE ADVISORIES Message GIA1 CONFIG – GIA1 config error. Config service req’d. GIA2 CONFIG – GIA2 config error. Config service req’d. GIA1 CONFIG – GIA1 audio config error. Config service req’d. GIA2 CONFIG – GIA2 audio config error. Config service req’d. 672 Comments The GIA1 and/or GIA2 configuration settings do not match backup configuration memory. The system should be serviced. The GIA1 and/or GIA2 have an error in the audio configuration. The system should be serviced. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX A Message GIA1 COOLING – GIA1 temperature too low. GIA2 COOLING – GIA2 temperature too low. GIA1 COOLING – GIA1 over temperature. GIA2 COOLING – GIA2 over temperature. GIA1 SERVICE – GIA1 needs service. Return the unit for repair. GIA2 SERVICE – GIA2 needs service. Return the unit for repair. HW MISMATCH – GIA hardware mismatch. GIA1 communication halted. HW MISMATCH – GIA hardware mismatch. GIA2 communication halted. MANIFEST – GIA1 software mismatch, communication halted. MANIFEST – GIA2 software mismatch, communication halted. MANIFEST – GFC software mismatch, communication halted. COM1 TEMP – COM1 over temp. Reducing transmitter power. COM2 TEMP – COM2 over temp. Reducing transmitter power. COM1 SERVICE – COM1 needs service. Return unit for repair. COM2 SERVICE – COM2 needs service. Return unit for repair. COM1 PTT – COM1 push-to-talk key is stuck. COM2 PTT – COM2 push-to-talk key is stuck. COM1 RMT XFR – COM1 remote transfer key is stuck. COM2 RMT XFR – COM2 remote transfer key is stuck. LOI – GPS integrity lost. Crosscheck with other NAVS. 190-00728-06 Rev. A Comments The GIA1 and/or GIA2 temperature is too low to operate correctly. Allow units to warm up to operating temperature. The GIA1 and/or GIA2 temperature is too high. If problem persists, the system should be serviced. The GIA1 and/or GIA2 self-test has detected a problem in the unit. The system should be serviced. A GIA mismatch has been detected, where only one is SBAS capable. The GIA1 and/or GIA 2 has incorrect software installed. The system should be serviced. Incorrect servo software is installed, or gain settings are incorrect. The system has detected an over temperature condition in COM1 and/or COM2. The transmitter is operating at reduced power. If the problem persists, the system should be serviced. The system has detected a failure in COM1 and/or COM2. COM1 and/or COM2 may still be usable. The system should be serviced when possible. The COM1 and/or COM2 external push-to-talk switch is stuck in the enable (or “pressed”) position. Press the PTT switch again to cycle its operation. If the problem persists, the system should be serviced. The COM1 and/or COM2 transfer switch is stuck in the enabled (or “pressed”) position. Press the transfer switch again to cycle its operation. If the problem persists, the system should be serviced. GPS integrity is insufficient for the current phase of flight. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 673 APPENDIX A Message GPS NAV LOST – Loss of GPS navigation. Insufficient satellites. GPS NAV LOST – Loss of GPS navigation. Position error. GPS NAV LOST – Loss of GPS navigation. GPS fail. ABORT APR – Loss of GPS navigation. Abort approach. APR DWNGRADE – Approach downgraded. TRUE APR – True north approach. Change HDG reference to TRUE. GPS1 SERVICE – GPS1 needs service. Return unit for repair. GPS2 SERVICE – GPS2 needs service. Return unit for repair. NAV1 SERVICE – NAV1 needs service. Return unit for repair. NAV2 SERVICE – NAV2 needs service. Return unit for repair. NAV1 RMT XFR – NAV1 remote transfer key is stuck. NAV2 RMT XFR – NAV2 remote transfer key is stuck. G/S1 FAIL – G/S1 is inoperative. Comments Loss of GPS navigation due to insufficient satellites. Loss of GPS navigation due to position error. Loss of GPS navigation due to GPS failure. Abort approach due to loss of GPS navigation. Vertical guidance generated by SBAS is unavailable, use LNAV only minimums. Displayed after passing the first waypoint of a true north approach when the nav angle is set to ‘AUTO’. A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver may still be available. The system should be serviced. A failure has been detected in the NAV1 and/or NAV2 receiver. The receiver may still be available. The system should be serviced. The remote NAV1 and/or NAV2 transfer switch is stuck in the enabled (or “pressed”) state. Press the transfer switch again to cycle its operation. If the problem persists, the system should be serviced. A failure has been detected in glideslope receiver 1 and/or receiver 2. The system should be serviced. G/S2 FAIL – G/S2 is inoperative. G/S1 SERVICE – G/S1 needs service. Return unit for repair. G/S2 SERVICE – G/S2 needs service. Return unit for repair. A failure has been detected in glideslope receiver 1 and/or receiver 2. The receiver may still be available. The system should be serviced when possible. GSD 41 MESSAGE ADVISORIES Message GSD1 CONFIG – GSD1 config error. Config service req’d. GSD1 COOLING – GSD1 temperature too low. GSD1 COOLING – GSD1 over temperature. 674 Comments GSD1 and the CDU have different copies of the GSD1 configuration. GSD1 is reporting a low temperature condition. GSD1 is reporting an over-temperature condition. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX A GSD1 SERVICE – GSD1 needs service. Return unit for repair. GSD1 is reporting an internal error condition. The GSD may still be usable. MANIFEST – GSD1 software mismatch. Communication halted. GSD1 has incorrect software installed. The system should be serviced. GEA 71 MESSAGE ADVISORIES Message GEA1 CONFIG – GEA1 config error. Config service req’d. GEA2 CONFIG – GEA2 config error. Config service req’d. GEA3 CONFIG – GEA3 config error. Config service req’d. MANIFEST – GEA1 software mismatch, communication halted. MANIFEST – GEA2 software mismatch, communication halted. MANIFEST – GEA3 software mismatch, communication halted. Comments The GEA1 configuration settings do not match those of backup configuration memory. The system should be serviced. The GEA2 configuration settings do not match those of backup configuration memory. The system should be serviced. The GEA3 configuration settings do not match those of backup configuration memory. The system should be serviced. The #1 GEA 71 has incorrect software installed. The system should be serviced. The #2 GEA 71 has incorrect software installed. The system should be serviced. The #3 GEA 71 has incorrect software installed. The system should be serviced. GTX 33 MESSAGE ADVISORIES Message XPDR1 CONFIG – XPDR1 config error. Config service req’d. XPDR2 CONFIG – XPDR2 config error. Config service req’d. MANIFEST – GTX1 software mismatch, communication halted. MANIFEST – GTX2 software mismatch, communication halted. XPDR1 SRVC – XPDR1 needs service. Return unit for repair. XPDR2 SRVC – XPDR2 needs service. Return unit for repair. XPDR1 FAIL – XPDR1 is inoperative. XPDR2 FAIL – XPDR2 is inoperative. XPDR1 ADS-B FAIL – XPDR1 is unable to transmit ADS-B messages. XPDR2 ADS-B FAIL – XPDR2 is unable to transmit ADS-B messages. 190-00728-06 Rev. A Comments The transponder configuration settings do not match those of backup configuration memory. The system should be serviced. The transponder configuration settings do not match those of backup configuration memory. The system should be serviced. The transponder has incorrect software installed. The system should be serviced. The transponder has incorrect software installed. The system should be serviced. The #1 transponder should be serviced when possible. The #2 transponder should be serviced when possible. There is no communication with the #1 transponder. There is no communication with the #2 transponder. ADS-B is inoperative. The transponder may not be receiving a valid GPS position. Other transponder functions may be available. Service when possible. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 675 APPENDIX A GRS 77 MESSAGE ADVISORIES Message AHRS1 TAS – AHRS1 not receiving airspeed. AHRS2 TAS – AHRS2 not receiving airspeed. AHRS1 GPS – AHRS1 using backup GPS source. AHRS2 GPS – AHRS2 using backup GPS source. AHRS1 GPS – AHRS1 not receiving any GPS information. AHRS2 GPS – AHRS2 not receiving any GPS information. AHRS1 GPS – AHRS1 not receiving backup GPS information. AHRS2 GPS – AHRS2 not receiving backup GPS information. AHRS1 GPS – AHRS1 operating exclusively in no-GPS mode. AHRS2 GPS – AHRS2 operating exclusively in no-GPS mode. AHRS MAG DB – AHRS magnetic model database version mismatch. AHRS1 SRVC – AHRS1 Magneticfield model needs update. AHRS2 SRVC – AHRS2 Magneticfield model needs update. GEO LIMITS – AHRS1 too far North/South, no magnetic compass. GEO LIMITS – AHRS2 too far North/South, no magnetic compass. MANIFEST – GRS1 software mismatch, communication halted. MANIFEST – GRS2 software mismatch, communication halted. Comments The #1 AHRS is not receiving true airspeed from the air data computer. The AHRS relies on GPS information to augment the lack of airspeed. The system should be serviced. The #2 AHRS is not receiving true airspeed from the air data computer. The AHRS relies on GPS information to augment the lack of airspeed. The system should be serviced. The #1 AHRS is using the backup GPS path. Primary GPS path has failed. The system should be serviced when possible. The #2 AHRS is using the backup GPS path. Primary GPS path has failed. The system should be serviced when possible. The #1 AHRS is not receiving any or any useful GPS information. Check AFMS limitations. The system should be serviced. The #2 AHRS is not receiving any or any useful GPS information. Check AFMS limitations. The system should be serviced. The #1 AHRS is not receiving backup GPS information. The system should be serviced. The #2 AHRS is not receiving backup GPS information. The system should be serviced. The #1 AHRS is operating exclusively in no-GPS mode. The system should be serviced. The #2 AHRS is operating exclusively in no-GPS mode. The system should be serviced. The #1 AHRS and #2 AHRS magnetic model database versions do not match. The #1 AHRS earth magnetic field model is out of date. Update magnetic field model when practical. The #2 AHRS earth magnetic field model is out of date. Update magnetic field model when practical. The aircraft is outside geographical limits for approved AHRS operation. Heading is flagged as invalid. The #1 AHRS has incorrect software installed. The system should be serviced. The #2 AHRS has incorrect software installed. The system should be serviced. GMU 44 MESSAGE ADVISORIES Message HDG FAULT – AHRS1 magnetometer fault has occurred. 676 Comments A fault has occurred in the #1 GMU 44. Heading is flagged as invalid. The AHRS uses GPS for backup mode operation. The system should be serviced. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX A Message HDG FAULT – AHRS2 magnetometer fault has occurred. MANIFEST – GMU1 software mismatch, communication halted. MANIFEST – GMU2 software mismatch, communication halted. Comments A fault has occurred in the #2 GMU 44. Heading is flagged as invalid. The AHRS uses GPS for backup mode operation. The system should be serviced. The GMU 44 has incorrect software installed. The system should be serviced. GSR 56 MESSAGE ADVISORIES Message GSR1 FAIL – GSR1 has failed. GSR2 FAIL – GSR2 has failed. Comments A failure has been detected in the #1 GSR 56. The system should be serviced. A failure has been detected in the #2 GSR 56. The system should be serviced. GDL 59 MESSAGE ADVISORIES Message GDL59 CONFIG – GDL 59 config error. Config service req’d. GDL59 FAIL – GDL 59 has failed. GDL59 SERVICE – GDL 59 needs service. Return unit for repair. GDL59 RTR FAIL – The GDL 59 router has failed. REGISTER GFDS – Data services are inoperative, register w/GFDS. MANIFEST – GDL software mismatch, communication halted. Comments GDL 59 configuration settings do not match those of backup configuration memory. The system should be serviced. A failure has been detected in the GDL 59. The receiver is unavailable. The system should be serviced. A failure has been detected in the GDL 59. The system should be serviced. A failure has been detected in the GDL 59 router. The system should be serviced. The GDL 59 is not registered with Garmin Flight Data Services, or its current registration data has failed authentication. The GDL 59 has incorrect software installed. The system should be serviced. GDL 69A MESSAGE ADVISORIES Message GDL69 CONFIG – GDL 69 config error. Config service req’d. GDL69 FAIL – GDL 69 has failed. MANIFEST – GDL software mismatch, communication halted. Comments GDL 69 configuration settings do not match those of backup configuration memory. The system should be serviced. A failure has been detected in the GDL 69. The receiver is unavailable. The system should be serviced The GDL 69 has incorrect software installed. The system should be serviced. GWX 68 ALERT MESSAGES Message GWX CONFIG – GWX config error. Config service req’d. 190-00728-06 Rev. A Comments GWX 68 configuration settings do not match those of the GDU configuration. The system should be serviced. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 677 APPENDIX A Message GWX FAIL – GWX is inoperative. Comments The GDU is not receiving status packet from the GWX 68 or the GWX 68 is reporting a fault. The GWX 68 radar system should be serviced. GWX SERVICE – GWX needs service. Return unit for repair. MANIFEST – GWX software mismatch, communication halted. WX ALERT – Possible severe weather ahead. A failure has been detected in the GWX 68. The GWX 68 may still be usable. The GWX 68 has incorrect software installed. The system should be serviced. Possible severe weather detected within +/- 10 degrees of the aircraft heading at a range of 80 to 320 nm. GDC 74B MESSAGE ADVISORIES Message ADC1 ALT EC – ADC1 altitude error correction is unavailable. ADC2 ALT EC – ADC2 altitude error correction is unavailable. ADC1 AS EC – ADC1 airspeed error correction is unavailable. ADC2 AS EC – ADC2 airspeed error correction is unavailable. MANIFEST – GDC1 software mismatch, communication halted. MANIFEST – GDC2 software mismatch, communication halted. Comments GDC1 or GDC2 is reporting that the altitude error correction is unavailable. GDC1 or GDC2 is reporting that the airspeed error correction is unavailable. The GDC 74B has incorrect software installed. The system should be serviced. GCU 475 MESSAGE ADVISORIES Message GCU CNFG – GCU Config error. Config service req’d. GCU FAIL – GCU is inoperative. MANIFEST – GCU software mismatch, communication halted. GCU KEYSTK – GCU [key name] Key is stuck. Comments GCU 475 configuration settings do not match those of backup configuration memory. The system should be serviced. A failure has been detected in the GCU 475. The GCU 475 is unavailable. The GCU 475 has incorrect software installed. The system should be serviced. A key is stuck on the GCU 475 bezel. Attempt to free the stuck key by pressing it several times. The system should be serviced if the problem persists. GMC 715 MESSAGE ADVISORIES Message GMC CONFIG – GMC Config error. Config service req’d. GMC FAIL – GMC is inoperative. MANIFEST – GMC software mismatch. Communication halted. GMC KEYSTK – GMC [key name] Key is stuck. 678 Comments Error in the configuration of the GMC 715. A failure has been detected in the GMC 715. The GMC 715 is unavailable. The GMC 715 has incorrect software installed. The system should be serviced. A key is stuck on the GMC 715 bezel. Attempt to free the stuck key by pressing it several times. The system should be serviced if the problem persists. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX A GTS 850 MESSAGE ADVISORIES Message GTS CONFIG – GTS config error. Config service req’d. Comments The GTS and GDU have incompatible configurations. This alert is also set when the GTS has an invalid mode S address configured or the mode S address does not match both XPDR mode S addresses. MANIFEST – GTS software mismatch, communication halted. The GTS has incorrect software installed. The system should be serviced. GDR 66 VHF DATA LINK TRANSCEIVER SYSTEM MESSAGES System Message CPDLC – CPDLC facility logon failed. CPDLC – CPDLC session terminated. GDR TEMP – GDR over temp. Reducing transmitter power. GDR FAIL – GDR is inoperative. GDR TX FAIL – GDR transmitter is inoperative. GDR PTT – GDR push-to-talk key is stuck. GDR RMT XFR – GDR remote transfer key is stuck. GDR SERVICE – GDR needs service. Return unit for repair. GDR CONFIG – GDR config error. Config service req’d. GDR MANIFEST – GDR software mismatch, communication halted. GDR AUX MANIFEST – GDR AUX software mismatch, communication halted. 190-00728-06 Rev. A Comments Logon failed. Check pertinent entries for accuracy. The currently active CPDLC session has been terminated. The system has detected an over temperature condition in the GDR. The transmitter operates at reduced power. If the problem persists, the system should be serviced. A failure has been detected in the GDR. The system should be serviced. The system should be serviced. The GDR push-to-talk switch is stuck in the enable (or “pressed”) position. Press the PTT switch again to cycle its operation. If the problem persists, the system should be serviced. The GDR transfer switch is stuck in the enabled (or “pressed”) position. Press the transfer switch again to cycle its operation. If the problem persists, the system should be serviced. The GDR should be serviced when possible. GDR configuration settings do not match those of backup configuration memory. The system should be serviced. The GDR has incorrect software installed. The system should be serviced. The GDR secondary processor has incorrect software installed. The system should be serviced. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 679 APPENDIX A MISCELLANEOUS MESSAGE ADVISORIES Message FPL WPT LOCK – Flight plan waypoint is locked. FPL WPT MOVE – Flight plan waypoint moved. TIMER EXPIRD – Timer has expired. DB CHANGE – Database changed. Verify user modified procedures. DB CHANGE – Database changed. Verify stored airways. FPL TRUNC – Flight plan has been truncated. LOCKED FPL – Cannot navigate locked flight plan. WPT ARRIVAL – Arriving at waypoint -[xxxx] STEEP TURN – Steep turn ahead. INSIDE ARSPC – Inside airspace. ARSPC AHEAD – Airspace ahead less than 10 minutes. ARSPC NEAR – Airspace near and ahead. ARSPC NEAR – Airspace near – less than 2 nm. APR INACTV – Approach is not active. SLCT FREQ – Select appropriate frequency for approach. SLCT NAV – Select NAV on CDI for approach. PTK FAIL – Parallel track unavailable: bad geometry. PTK FAIL – Parallel track unavailable: past IAF. 680 Comments Upon power-up, the system detects that a stored flight plan waypoint is locked. This occurs when an navigation database update eliminates an obsolete waypoint. The flight plan cannot find the specified waypoint and flags this message. This can also occur with user waypoints in a flight plan that is deleted. Remove the waypoint from the flight plan if it no longer exists in any database, Or update the waypoint name/identifier to reflect the new information. The system has detected that a waypoint coordinate has changed due to a new navigation database update. Verify that stored flight plans contain correct waypoint locations. The system notifies the pilot that the timer has expired. This occurs when a stored flight plan contains procedures that have been manually edited. This alert is issued only after an navigation database update. Verify that the user-modified procedures in stored flight plans are correct and up to date. This occurs when a stored flight plan contains an airway that is no longer consistent with the navigation database. This alert is issued only after an navigation database update. Verify use of airways in stored flight plans and reload airways as needed. This occurs when a newly installed navigation database eliminates an obsolete approach or arrival used by a stored flight plan. The obsolete procedure is removed from the flight plan. Update flight plan with current arrival or approach. This occurs when the pilot attempts to activate a stored flight plan that contains locked waypoint. Remove locked waypoint from flight plan. Update flight plan with current waypoint. Arriving at waypoint [xxxx], where [xxxx] is the waypoint name. A steep turn is 15 seconds ahead. Prepare to turn. The aircraft is inside the airspace. Special use airspace is ahead of aircraft. The aircraft will penetrate the airspace within 10 minutes. Special use airspace is near and ahead of the aircraft position. Special use airspace is within 2 nm of the aircraft position. The system notifies the pilot that the loaded approach is not active. Activate approach when required. The system notifies the pilot to load the approach frequency for the appropriate NAV receiver. Select the correct frequency for the approach. The system notifies the pilot to set the CDI to the correct NAV receiver. Set the CDI to the correct NAV receiver. Bad parallel track geometry. IAF waypoint for parallel offset has been passed. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX A Message PTK FAIL – Parallel track unavailable: past IAF. UNABLE V WPT – Can’t reach current vertical waypoint. VNV – Unavailable. Unsupported leg type in flight plan. VNV – Unavailable. Excessive track angle error. VNV – Unavailable. Excessive crosstrack error. VNV – Unavailable. Parallel course selected. NON WGS84 WPT – Do not use GPS navigation to [xxxx]. TRAFFIC FAIL – Traffic device has failed. FAILED PATH – A data path has failed. MAG VAR WARN – Large magnetic variance. Verify all course angles. SVS – SVS DISABLED: Out of available terrain region. SVS – SVS DISABLED: Terrain DB resolution too low. SCHEDULER [#] – . CHECK CRS – Database course for LOC1 / [LOC ID] is [CRS]°. CHECK CRS – Database course for LOC2 / [LOC ID] is [CRS]°. [PFD1, PFD2, or MFD1] CARD 1 REM – Card 1 was removed. Reinsert card. [PFD1, PFD2, or MFD1] CARD 2 REM – Card 2 was removed. Reinsert card. [PFD1, PFD2, or MFD1] CARD 1 ERR – Card 1 is invalid. [PFD1, PFD2, or MFD1] CARD 2 ERR – Card 2 is invalid. 190-00728-06 Rev. A Comments IAF waypoint for parallel offset has been passed. The current vertical waypoint can not be reached within the maximum flight path angle and vertical speed constraints. The system automatically transitions to the next vertical waypoint. The lateral flight plan contains a procedure turn, vector, or other unsupported leg type prior to the active vertical waypoint. This prevents vertical guidance to the active vertical waypoint. The current track angle error exceeds the limit, causing the vertical deviation to go invalid. The current crosstrack exceeds the limit, causing vertical deviation to go invalid. A parallel course has been selected, causing the vertical deviation to go invalid. The position of the selected waypoint [xxxx] is not calculated based on the WGS84 map reference datum and may be positioned in error as displayed. Do not use GPS to navigate to the selected non-WGS84 waypoint. The system is no longer receiving data from the traffic system. The traffic device should be serviced. A data path connected to the GDU, GSD 41, or the GIA 63/W has failed. The GDU’s internal model cannot determine the exact magnetic variance for geographic locations near the magnetic poles. Displayed magnetic course angles may differ from the actual magnetic heading by more than 2°. Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database. Synthetic Vision is disabled because a terrain database of sufficient resolution (9 arcsecond or better) is not currently installed. Message criteria entered by the user. Selected course for LOC1 differs from published localizer course by more than 10 degrees. Selected course for LOC2 differs from published localizer course by more than 10 degrees. The SD card was removed from the top card slot of the specified PFD or MFD. The SD card needs to be reinserted. The SD card was removed from the bottom card slot of the specified PFD or MFD. The SD card needs to be reinserted. The SD card in the top card slot of the specified PFD or MFD contains invalid data. The SD card in the bottom card slot of the specified PFD or MFD contains invalid data. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 681 APPENDIX A TAWS-A ALERTS PFD/MFD TAWS-A Page Annunciation Alert Type MFD Map Page Pop-Up Alert Aural Message Reduced Required Terrain Clearance Warning (RTC) Imminent Terrain Impact Warning (ITI) “Terrain, Terrain; Pull Up, Pull Up” “Terrain, Terrain; Pull Up, Pull Up” Reduced Required Obstacle Clearance Warning (ROC) Imminent Obstacle Impact Warning (IOI) “Obstacle, Obstacle; Pull Up, Pull Up” “Obstacle, Obstacle; Pull Up, Pull Up” Excessive Descent Rate Warning (EDR) “ Pull Up” Excessive Closure Rate Warning (ECR) “ Pull Up” Reduced Required Terrain Clearance Caution (RTC) Imminent Terrain Impact Caution (ITI) “Caution, Terrain; Caution, Terrain” Reduced Required Obstacle Clearance Caution (ROC) “Caution, Obstacle; Caution, Obstacle” Imminent Obstacle Impact Caution (IOI) “Caution, Obstacle; Caution, Obstacle” Premature Descent Alert Caution (PDA) “Too Low, Terrain” Excessive Descent Rate Caution (EDR) “Sink Rate” Excessive Closure Rate Caution (ECR) “Terrain, Terrain” Negative Climb Rate Caution (NCR) “Don’t Sink” Flight Into Terrain High Speed Caution (FIT) “Too Low, Terrain” Flight Into Terrain Gear Caution (FIT) “Too Low, Gear” Flight Into Terrain Flaps Caution (FIT) “Too Low, Flaps” Flight Into Terrain Takeoff Caution (FIT) “Too Low, Terrain” Glide Slope/Glide Path Deviation Caution (GSD) (depends on approach type) Altitude Voice Callout (VCO) 682 “Caution, Terrain; Caution, Terrain” or or None None Embraer Prodigy® Flight Deck 100 Pilot’s Guide “Glide Slope” or “Glide Path” “Five-Hundred” “Four-Hundred” “Three-Hundred” “Two-Hundred” “One-Hundred” 190-00728-06 Rev. A APPENDIX A TAWS-A SYSTEM STATUS ANNUNCIATIONS PFD/MFD TAWS-A Page Annunciation Additional TAWS-A Page Annunciation Aural Message TAWS System Fail, Terrain or Obstacle database unavailable or invalid, invalid software configuration, system audio fault GPWS System Fail TAWS FAIL “TAWS System Failure” None “GPWS System Failure” System Test in progress TAWS TEST None None None “TAWS System Test OK” None TERRAIN DATABASE FAILURE None None “GPWS System Failure” NO GPS POSITION “TAWS Not Available” None “TAWS Not Available” None “TAWS Not Available” “TAWS Available” when aircraft enters database coverage area. Alert Type System Test pass MFD Terrain or Obstacle database unavailable or invalid. TAWS operating with PFD Terrain or Obstacle databases GPWS System Fail, Radar Altimeter invalid, Altitude or Vertical Speed unavailable No GPS position Excessively degraded GPS signal, Out of database coverage area Out of database coverage area TAWS-A ALERT AVAILABILITY TAWS-A Alert Type Available TAWS-A Status RTC ITI ROC IOI PDA EDR ECR NCR Annunciation Displayed * FIT GSD VCO No No No No No No No No No No No No No No No No Yes Yes Yes Yes *No **Yes No No No No No Yes Yes Yes Yes Yes **Yes No No No No No Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes No No No No No **Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes No Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes No Yes Yes Yes Yes Yes Yes Yes Yes Yes #Yes Yes Yes GSD alert will be available if a valid ILS is being used for navigation, even if no valid GPS signal is being received. ** VCO alerts are not issued if both TAWS and GPWS systems have failed or are not available. # 190-00728-06 Rev. A Only the portions of FIT Alerting based on flap position are disabled when FLAP OVR annunciation is displayed. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 683 APPENDIX A TAWS-B ALERTS Annunciations appear on the PFD and MFD. Pop-up alerts appear only on the MFD. PFD/MFD TAWS Page Annunciation Alert Type MFD Map Page Pop-Up Alert Aural Message Excessive Descent Rate Warning (EDR) “Pull Up” Reduced Required Terrain Clearance Warning (RTC) Imminent Terrain Impact Warning (ITI) “Terrain, Terrain; Pull Up, Pull Up” “Terrain, Terrain; Pull Up, Pull Up” Reduced Required Obstacle Clearance Warning (ROC) Imminent Obstacle Impact Warning (IOI) “Obstacle, Obstacle; Pull Up, Pull Up” “Obstacle, Obstacle; Pull Up, Pull Up” Reduced Required Terrain Clearance Caution (RTC) Imminent Terrain Impact Caution (ITI) “Caution, Terrain; Caution, Terrain” “Caution, Terrain; Caution, Terrain” Reduced Required Obstacle Clearance Caution (ROC) Imminent Obstacle Impact Caution (IOI) “Caution, Obstacle; Caution, Obstacle” “Caution, Obstacle; Caution, Obstacle” Premature Descent Alert Caution (PDA) Altitude Callout “500” Excessive Descent Rate Caution (EDR) “Too Low, Terrain” None “Five-Hundred” “Sink Rate” None Negative Climb Rate Caution (NCR) “Don’t Sink” TAWS-B SYSTEM STATUS ANNUNCIATIONS PFD/MFD Alert Annunciation Alert Type System Test in Progress System Test Pass TAWS Alerting is disabled None MFD Terrain or Obstacle database unavailable or invalid. TAWS operating with PFD Terrain or Obstacle databases TAWS-B System Test Fail, Terrain or Obstacle database unavailable or invalid, invalid software configuration, system audio fault None No GPS position Excessively degraded GPS signal, Out of database coverage area Sufficient GPS signal received after loss 684 None TAWS-B Page Annunciation Aural Message TAWS TEST None None “TAWS System Test OK” None None TERRAIN DATABASE FAILURE None TAWS FAIL “TAWS System Failure” NO GPS POSITION “TAWS Not Available” None “TAWS Not Available” None “TAWS Available” Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX A TCAS I ALERTS AND ANNUNCIATIONS Mode Traffic Mode Annunciation (Traffic Map Page) TCAS I Self-test Initiated TEST (also shown in white in center of page) OPERATING TCAS I Operating TCAS I Standby Traffic Display Status Icon (Other Maps) STANDBY (also shown in white in center of page) FAIL TCAS I Failed TCAS I Modes Traffic Map Page Annunciation Description NO DATA Data is not being received from the TCAS I unit DATA FAILED Data is being received from the TCAS I unit, but the unit is self-reporting a failure FAILED Incorrect data format received from the TCAS I unit TCAS I Failure Annunciations Traffic Status Banner Annunciation TA OFF SCALE TA X.X ± XX ↕ TRFC FAIL NO TCAS DATA Description A Traffic Advisory is outside the selected display range*. Annunciation is removed when traffic comes within the selected display range. System cannot determine bearing of Traffic Advisory**. Annunciation indicates distance in nm, altitude separation in hundreds of feet, and altitude trend arrow (climbing/descending). TCAS I unit has failed (unit is self-reporting a failure or sending incorrectly formatted data) Data is not being received from the TCAS I unit *Shown as symbol on Traffic Map Page **Shown in center of Traffic Map Page TCAS I Traffic Status Annunciations 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 685 APPENDIX A TCAS II ALERTS AND ANNUNCIATIONS PFD Mode Annunciation Mode TCAS II Self-test Initiated (TEST) None Traffic Advisory and Resolution Advisory (TA/RA) None MFD Traffic Map Page Mode Annunciation TEST (‘TEST MODE’ also shown in white on top center of page) Traffic Display Status Icon (Other Maps) TA/RA Traffic Advisory Only (TA ONLY) TA ONLY TCAS II Standby (TFC STBY) * STANDBY (also shown in white in center of page when aircraft on ground, yellow in air) FAIL TCAS II Failed * Annunciation appears white when aircraft is on the ground and yellow while in the air. TCAS II Modes Traffic Map Page Annunciation NO DATA DATA FAILED FAILED Description Data is not being received from the TCAS II unit Data is being received from the TCAS II unit, but the unit is self-reporting a failure Incorrect data format received from the TCAS II unit TCAS II Failure Annunciations Traffic Status Banner Annunciation RA OFF SCALE TA OFF SCALE RA X.X ± XX ↕ TA X.X ± XX ↕ TRFC FAIL NO TCAS DATA Description A Resolution Advisory is outside the selected display range*. Annunciation is removed when traffic comes within the selected display range A Traffic Advisory is outside the selected display range*. Annunciation is removed when traffic comes within the selected display range. System cannot determine bearing of Resolution Advisory**. Annunciation indicates distance in nm, altitude separation in hundreds of feet, and altitude trend arrow (climbing/descending). System cannot determine bearing of Traffic Advisory**. Annunciation indicates distance in nm, altitude separation in hundreds of feet, and altitude trend arrow (climbing/descending). TCAS II unit has failed (unit is self-reporting a failure or sending incorrectly formatted data) Data is not being received from the TCAS II unit *Shown as symbol on Traffic Map Page **Shown in center of Traffic Map Page TCAS II Traffic Status Annunciations 686 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX A CPDLC ATC ALERT The following PFD alert informs the flight crew of a received CPDLC message from ATC. When the message is received, the alert flashes five times, then stays illuminated until the required action is accomplished. Figure A-5 CPDLC Alert on the PFD OTHER PRODIGY® AURAL ALERTS Message Priority Warning – Autopilot is disengaged Single alert for manual AP disengagement Continuous alert for automatic AP disengagement; cancelled with AP DISC Switch High cabin altitude Engine fire Flight director has reverted to pitch or roll default mode Maximum operating speed exceeded “Autopilot” “Cabin” “Fire, Fire” “Flight Director” “High Speed” "Increase Speed, Increase Speed" “Landing Gear” “Minimums, minimums” “No Takeoff Brake” “No Takeoff Flaps” “No Takeoff Trim” “No Takeoff Spoilers” “Stall, Stall” “Timer Expired” "Message ATC" “Altitude” “Traffic” “Trim Trim Trim” “Vertical track” “Aural Warning OK” “Aural Warning One Channel” “Incoming Call “SelCal” “Takeoff OK” “TIS not available” 190-00728-06 Rev. A Description Warning Airplane is in a low airspeed and high angle of attack configuration Gear up in landing condition The aircraft has descended below the preset barometric minimum descent altitude. No Takeoff Configuration due to brake status No Takeoff Configuration due to flap status No Takeoff Configuration due to trim status No Takeoff Configuration due to spoiler status Airplane in stall condition Countdown timer on the PFD has reached zero New ATC data link message received Aircraft has deviated ±200 feet of the selected altitude The Traffic Information Service (TIS) has issued a Traffic Advisory alert. Advisory Trim switch malfunction The aircraft is one minute from Top of Descent. Issued only when vertical navigation is enabled. Aural warning system test passes Aural warning system test detects failure in one channel Satellite telephone is receiving a call Status Incoming communication through the HF radio Takeoff configuration test passed The aircraft is outside the Traffic Information Service (TIS) coverage area. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 687 APPENDIX A FLIGHT PLAN IMPORT/EXPORT MESSAGES In some circumstances, some messages may appear in conjunction with others. Flight Plan Import/Export Results ‘Flight plan successfully imported.’ ‘File contained user waypoints only. User waypoints imported successfully. No stored flight plan data was modified.’ ‘No flight plan files found to import.’ ‘Flight plan import failed.’ ‘Flight plan partially imported.’ ‘File contained user waypoints only.’ ‘Too many points. Flight plan truncated.’ ‘Some waypoints not loaded. Waypoints locked.’ ‘User waypoint database full. Not all loaded.’ ‘One or more user waypoints renamed.’ ‘Flight plan successfully exported.’ ‘Flight plan export failed.’ Description A flight plan file stored on the SD card was successfully imported as a stored flight plan. The file stored on the SD card did not contain a flight plan, only user waypoints. These waypoints have been saved to the system user waypoints. No flight plans stored in the system have been modified. The SD card contains no flight plan data. Flight plan data was not successfully imported from the SD card. Some flight plan waypoints were successfully imported from the SD card, however others had errors and were not imported. A partial stored flight plan now exists in the system. The file stored on the SD card did not contain a flight plan, only user waypoints. One or more of these waypoints did not import successfully. The flight plan on the SD card contains more waypoints than the system can support. The flight plan was imported with as many waypoints as possible. The flight plan on the SD card contains one or more waypoints that the system cannot find in the navigation database. The flight plan has been imported, but must be edited within the system before it can be activated for use. The flight plan file on the SD card contains user waypoints. The quantity of stored user waypoints has exceeded system capacity, therefore not all the user waypoints on the SD card have been imported. Any flight plan user waypoints that were not imported are locked in the flight plan. The flight plan must be edited within the system before it can be activated for use. One or more imported user waypoints were renamed when imported due to naming conflicts with waypoints already existing in the system. The stored flight plan was successfully exported to the SD card. The stored flight plan was not successfully exported to the SD card. The SD card may not have sufficient available memory or the card may have been removed prematurely. PILOT PROFILE IMPORT/EXPORT MESSAGES Pilot Profile Import/Export Results ‘No pilot profile plan files found to import.’ ‘Overwrite existing profile?’ ‘Profile name invalid. Enter a different profile name.’ ‘All available pilot profiles in use. Delete a profile before importing another.’ ‘Pilot profile import failed.’ ‘Pilot profile import succeeded.’ ‘Overwrite existing file?’ ‘Pilot profile export failed.’ ‘Pilot profile export succeeded.’ 688 Description Displayed if the SD card does not have one or more valid pilot profile filenames. Displayed if the profile name matches the name of existing profile. Displayed if the profile name is invalid. Displayed if the maximum number for pilot profiles has been reached. Displayed if the importing operation fails for any other reason. Displayed if the importing operation succeeds. Displayed if the filename matches the name of an existing file on the SD card. Displayed if the export operation fails. Displayed if the export operation succeeds. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX B DATABASE MANAGEMENT CAUTION: Never disconnect power to the system when loading a database. Power interuption during the database loading process could result in maintenance being required to reboot the system. The system uses Secure Digital (SD) cards to load and store various types of data. For basic flight operations, SD cards are required for database storage as well as Jeppesen navigation and ChartView database updates. Not all SD cards are compatible with the Prodigy® system. Use only SD cards supplied by Garmin or the aircraft manufacturer. CAUTION: When downloading updates to the Jeppesen Navigation Database, copy the data to an SD card other than a Garmin Supplemental Data Card. Otherwise, data corruption can occur. NOTE: When loading database updates, the ‘DB Mismatch’ message will be displayed until database synchronization is complete, followed by turning system power off, then on. Synchronization can be monitored on the AUX-SYSTEM STATUS Page. NOTE: Loading a database in the system prior to its effective date will result in the expiration date on the power-up screen and the effective date on the AUX-System Status Page being displayed in yellow. NOTE: Garmin requests the flight crew report any observed discrepancies related to database information. These discrepancies could come in the form of an incorrect procedure; incorrectly identified terrain, obstacles and fixes; or any other displayed item used for navigation or communication in the air or on the ground. Go to FlyGarmin.com and select “Aviation Data Error Report”. NOTE: The FAA has asked Garmin to remind pilots who fly with Garmin database-dependent avionics of the following: • It is the pilot’s responsibility to remain familiar with all FAA regulatory and advisory guidance and information related to the use of databases in the National Airspace System. • Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen. Databases obtained from Garmin or Jeppesen are assured compliance with all data quality requirements (DQRs) by virtue of a Type 2 Letter of Authorization (LOA) from the FAA. A copy of the Type 2 LOA is available for each database and can be viewed at http://fly.garmin.com by selecting ‘Type 2 LOA Status.’ • Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with established FAA regulatory guidance, but does not constitute authorization to fly any and all terminal procedures that may be presented by the system. It is the pilot’s responsibility to operate in accordance with established AFM(S) and regulatory guidance or limitations as applicable to the pilot, the aircraft, and installed equipment. NOTE: The pilot/operator must review and be familiar with Garmin’s database exclusion list as discussed in SAIB CE-14-04 to determine what data may be incomplete. The database exclusion list can be viewed at www.flygarmin.com by selecting ‘Database Exclusions List.’ 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 689 APPENDIX B NOTE: The pilot/operator must have access to Garmin and Jeppesen database alerts and consider their impact on the intended aircraft operation. The database alerts can be viewed at www.flygarmin.com by selecting ‘Aviation Database Alerts.’ NOTE: If the pilot/operator wants or needs to adjust the database, contact Garmin Product Support to coordinate the revised DQRs. NOTE: Garmin requests the flight crew report any observed discrepancies related to database information. These discrepancies could come in the form of an incorrect procedure; incorrectly identified terrain, obstacles and fixes; or any other displayed item used for navigation or communication in the air or on the ground. Go to FlyGarmin.com and select ‘Report An Aviation Data Error Report.’ JEPPESEN DATABASES The Jeppesen navigation database is updated on a 28-day cycle. The ChartView database is updated on a 14day cycle. If the ChartView database is not updated within 70 days of the expiration date, ChartView will no longer function. Both of these databases are provided directly from Jeppesen. NOTE: The Jeppesen aviation navigation database is now referred to as the ‘navigation database’. Previously this database had been referred to as the ‘aviation database’. The ChartView database should be copied to the Garmin supplied Supplemental Data Card which will reside in the bottom card slot on the MFD. The navigation database must be installed from the Jeppesen or user supplied SD data card. Contact Jeppesen (www.jeppesen.com) for subscription and update information. NOTE: After the navigation database is installed, the card may be removed. Updating the active Jeppesen navigation database (not using the Dual Navigation Database or Automatic Database Synchronization Features): 1) With the system OFF, insert the SD card containing the new navigation database version into the top card slot of the display (PFD1, PFD2 or MFD) to be updated (label of SD card facing left). 2) Turn the system ON. A prompt similar to the following is displayed in the upper left corner of the display: Figure B-1 Standby Navigation Database Prompt 690 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX B 3) Press the NO Softkey to proceed to loading the active database. 4) A prompt similar to the following is displayed, press the YES Softkey to update the active navigation database. Figure B-2 Database Update Confirmation 5) After the update completes, the display starts in normal mode. Do not remove power while the display is starting. 6) Turn the system OFF and remove the SD card from the top card slot. 7) Repeat steps 1 through 6 for the other displays (PFD1, PFD2 or MFD). Remove the SD card when finished. 8) Apply power to the system and press the ENT Key to acknowledge the startup screen. 9) Turn the large FMS Knob to select the AUX Page group on the MFD. 10) Turn the small FMS Knob to select the System Status Page. 11) Press the Display Database Selection Softkey to show active navigation database information for each display (MFD1 DB, PFD1 DB, PFD2 DB). Verify the correct active navigation database cycle information is shown for each display. DUAL NAVIGATION DATABASE FEATURE The dual navigation database feature allows each display to store an upcoming navigation database on the bottom SD card so that the system can automatically load it to replace the active database when the new database becomes effective (the next cycle becomes available seven days prior to its effective date). If a navigation database loader card is inserted into the top SD card slot of a display, and an SD card is in the bottom slot, the system will prompt the user (upon on-ground power up) as to whether the database should be stored on the bottom SD card as the standby database. If the user responds affirmatively, the system will copy the navigation database from the top SD card to the bottom SD card. As long as the bottom SD card remains in the card slot, this standby navigation database will be available for the system to use as the active database as soon as it becomes effective. The system checks the active and standby databases upon (on-ground only) power-up. If the standby database is current and the active database is out of date, the display will upload the standby database into the active internal database location. Loading the standby database to the active location takes approximately 45-55 seconds. During the loading process ‘Please Wait. Navigation Database Update in Progress. Do Not Remove Power from Displays’ will be displayed on screen. After startup is complete, the pilot is alerted that the update is complete by a system alert message, ‘NAV DB UPDATED’. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 691 APPENDIX B In some situations, such as an overnight flight in which departure date is prior to the effective date of the standby database and arrival date is after the effective date, it may be desired to force the loaded standby database into active service earlier than the system would otherwise make the change. This can be accomplished by selecting the STBY DB Softkey on the AUX-System Status Page. Turn system power off, then on to complete the database change. Loading a standby navigation database: 1) With the system OFF, insert the SD card containing the new navigation database version into the top card slot of the MFD. 2) Verify that an SD card is inserted in the bottom slot of each PFD and the MFD. 3) Turn the system ON. A prompt similar to the following is displayed. Figure B-3 Standby Navigation Database Prompt 4) Press the YES Softkey. The navigation database is copied to the SD card in the bottom card slot of the MFD. 5) After the navigation database files are copied to the bottom SD card, the display will appear as shown in Figure B-4. Figure B-4 Standby Navigation Database Update Complete 692 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX B 6) As instructed on the display, press any key to continue. The display will now appear as shown in Figure B-5. Figure B-5 Navigation Database Verification Prompt 7) Press any key to continue. The display will now appear as shown in Figure B-6. Figure B-6 Active Navigation Database Prompt 8) Press the NO Softkey. The display now starts in normal mode. Since the database effective date is not yet valid, it should not be loaded as the active database. The display now starts in normal mode. Do not remove power while the display is starting. 9) Press the ENT Key to acknowledge the startup screen. 10) Turn the large FMS Knob to select the AUX Page group on the MFD. 11) Turn the small FMS Knob to select the System Status Page. 12) The new database is copied to the SD card in the bottom card slot of each PFD. Progress can be monitored in the SYNC STATUS field. When copying is finished, ‘Complete’ is displayed. 13) Turn system power OFF. 14) Remove the SD card from the top card slot of the MFD. 15) Turn system power ON. 16) Press the ENT Key to acknowledge the startup screen. 17) Turn the large FMS Knob to select the AUX Page group on the MFD. 18) Turn the small FMS Knob to select the System Status Page. 19) Press the Display Database Selection Softkey to show standby navigation database information for each display (MFD1 DB, PFD1 DB, PFD2 DB). Verify the correct standby navigation database cycle information is shown for each display. GARMIN DATABASES The following databases are stored on Supplemental Data Cards provided by Garmin: • Expanded basemap • Airport terrain • SafeTaxi • Terrain • Obstacle • FliteCharts 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide • Airport Directory (AOPA or AC-UKWIK) 693 APPENDIX B After subscribing to the desired database product, these database products will be downloaded and ultimately stored on three Supplemental Data Cards (with the exception of FliteCharts, which is loaded on only one card). Each Supplemental Data Card resides in the bottom card of each display as shown in Figure B-7. These cards must not be removed except to update the databases stored on each card. PFD1 MFD PFD2 Figure B-7 Correct Database Locations Since these databases are not stored internally in the displays, a Supplemental Data Card containing identical database versions must be kept in each display unit. The basemap database contains data for the topography and land features, such as rivers, lakes, and towns. It is updated only periodically, with no set schedule. There is no expiration date. The terrain database contains the terrain mapping data. The airport terrain database contains increased resolution terrain data around airports. These databases are updated periodically and have no expiration date. The obstacle database contains data for obstacles, such as towers, that pose a potential hazard to aircraft. Obstacles 200 feet and higher are included in the obstacle database. It is very important to note that not all obstacles are necessarily charted and therefore may not be contained in the obstacle database. This database is updated on a 56-day cycle. NOTE: The data contained in the terrain and obstacle databases comes from government agencies. Garmin accurately processes and cross-validates the data, but cannot guarantee the accuracy and completeness of the data. The AOPA or AC-U-KWIK Airport Directory provides data on airports and heliports throughout the U.S., and offers detailed information for over 5,300 U. S. airports, along with the names and phone numbers of thousands of FBOs. These databases are updated every 56 days. The SafeTaxi database contains detailed airport diagrams for selected airports. These diagrams aid in following ground control instructions by accurately displaying the aircraft position on the map in relation to taxiways, ramps, runways, terminals, and services. This database is updated on a 56-day cycle. The FliteCharts database contains procedure charts for the United States only. This database is updated on a 28-day cycle. If not updated within 180 days of the expiration date, FliteCharts will no longer function. 694 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX B AUTOMATIC DATABASE SYNCHRONIZATION FEATURE The automatic database synchronization feature automatically transfers the database from a single SD database card to the SD cards on each PFD and the MFD to ensure that all databases are synchronized throughout the system. After power-up, the system compares all copies of each applicable database. If similar databases do not match, the most recent valid database is automatically copied to each card in the system that does not already contain that database. The following databases are checked and synchronized: Basemap, Safetaxi, Airport Terrain, Obstacle, Airport Directory (AOPA or AC-U-KWIK), and Terrain. This feature applies only to databases that are stored on the SD card that resides in the bottom slot of each display. This feature does not apply to the navigation database which is stored internally in each display, or to the charts databases (FliteCharts and ChartView) which are only required to be present on the MFD. The typical procedure would be to download new databases to the MFD card, then synchronize the data to the PFD(s). NOTE: The 9-arc second terrain database may take as long as 100 minutes to synchronize using this method. Therefore the user may want to transfer the data using a PC, or connect the system to a ground power source while performing the database synchronization. The synchronization progress may be monitored on the AUX-System Status Page in the Sync Status section of the Database Window (Figure B-8). This section shows the synchronization status of each applicable database, including the percent complete, time remaining, and to which displays the databases are being copied. When the synchronization is complete, the status is listed as ‘Complete’, followed by the displays to which the databases were copied. This sub-section is only present when a sync is occurring or has occurred on the current power-up. An indication of ‘Complete’ still requires a power cycle before the synchronized databases will be used by the system. Figure B-8 AUX-System Status Page, Database Window The Display Database Softkey (Figure B-11) is used to place the cursor in the Database Window. Upon first press of the Display Database Softkey, the softkey will change to a selected state (black text on gray background) and the cursor will appear in the Database Window. At this point the user can scroll through 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 695 APPENDIX B all databases in the Database Window to view status information. If the Display Database Softkey is pressed repeatedly, the softkey will cycle through PFD1, PFD2, and MFD. Database status information in the Database Window will reflect the database of the selected PFD or MFD. After a successful sync and restart, verify that the proper databases are now in use on the AUX–System Status Page (Figure B-8). If an error occurs during the synchronization, an error message will be displayed, followed by the affected display in the Sync Status section of the Database Window (Figure B-9). If a synchronization completes on one display, but an error occurs on another, the error message will be displayed with the affected diaplay listed after it. When an error message (Table B-1) is displayed, the problem must be corrected before the synchronization can be completed. A power cycle is required to restart synchronization when ‘Card Full’ or ‘Err’ is shown. Database Synchronization Error Message Figure B-9 Synchronization Error Message Error Message Description Canceled Database synchronization has been canceled by removing the bottom SD card in display being updated Card Full SD card does not contain sufficient memory Err Displayed for all other errors that may cause the synchronization process to be halted Timeout System timed-out prior to the database transfer completing Table B-1 Database Synchronization Error Messages UPDATING GARMIN DATABASES The Garmin database updates can be obtained by following the instructions detailed in the ‘Aviation Databases’ section of the Garmin website (fly.garmin.com). Once the updated files have been downloaded from the website, a PC equipped with an appropriate SD card reader is used to unpack and program the new databases onto an existing Supplemental Data Card. Equipment required to perform the update is as follows: • Windows-compatible PC computer (running Windows XP, Vista, or Windows 7) • SD Card Reader: SanDisk SDDR-93, SanDisk SDDR-99, Verbatim #96504, or equivalent • Updated database obtained from the Garmin website • Existing Supplemental Database SD Cards (010-00330-42, or -43) from both PFDs and MFD 696 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX B In some cases it may be necessary to obtain an unlock code from Garmin in order to make the database product functional. It may also be necessary to have the system configured by a Garmin authorized service facility in order to use some database features. After the data has been copied to the appropriate data card, perform the following steps: 1) With system power OFF, remove the MFD database card from the bottom card slot of the MFD. 2) Update the Garmin databases on the MFD card. 3) Insert the MFD database card into the bottom card slot of the MFD. 4) Apply power to the system, check that the databases are initialized and displayed on the power-up screen (Figure B-10). When updating the terrain and FliteCharts databases, a ‘Verifying’ message may be seen. If this message is present, wait for the system to finish loading before proceeding to step 5. Figure B-10 Database Information on the Power-up Screen 5) Acknowledge the Power-up Page agreement by pressing the ENT Key or the right most softkey. 6) Turn the large FMS Knob to select the AUX Page group on the MFD. 7) Turn the small FMS Knob to select the System Status Page. 8) Monitor the Sync Status in the Database Window. Wait for all databases to complete synching, indicated by ‘Complete’ being displayed as seen in Figure B-9. 9) Remove and reapply power to the system. 10) Turn the large FMS Knob to select the AUX Page group on the MFD. 11) Turn the small FMS Knob to select the System Status Page. 12) Press the Display Database Selection Softkey to show database information for each display (MFD1 DB, PFD1 DB, PFD2 DB). Verify the correct database cycle information is shown for each database for each display. Unselected MFD1 DB Selected PFD1 DB Selected Figure B-11 Display Database Softkey 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 697 APPENDIX B MAGNETIC FIELD VARIATION DATABASE UPDATE A copy of the current magnetic field variation database (MV DB) is included with the navigation database. At startup, the system compares this version of the MV DB with that presently being used by each AHRS (GRS1 and GRS2). If the system determines the MV DB needs to be updated, a prompt is displayed on the Navigation Map Page, as shown in Figure B-12. Note, in the following example, GRS1 is the first AHRS to indicate an update is available. In actuality, this is dependent on which AHRS is the first to report status to the system. GRS2 may be displayed before GRS1. The order is not important, only that both AHRS be updated. Figure B-12 GRS1 Magnetic Field Variation Database Update Prompt Loading the magnetic field variation database update: 1) With ‘OK’ highlighted, as seen in Figure B-12, press the ENT Key on the MFD. A progress monitor is displayed as shown in Figure B-13. Figure B-13 Uploading Database to GRS1 2) When the upload is complete, the prompt for the next GRS upload is displayed, as seen in Figure B-14. Figure B-14 GRS2 Magnetic Field Variation Database Update Prompt 698 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX B 3) With ‘OK’ highlighted, press the ENT Key on the MFD. A progress monitor is displayed as shown in Figure B-15. When the upload is complete, the system is ready for use. Figure B-15 Uploading Database to GRS2 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 699 APPENDIX B Blank Page 700 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX C GLOSSARY ACC accuracy ACT, ACTV active, activate ADC air data computer ADF Automatic Direction Finder ADI Attitude Direction Indicator AF Arc to fix AFCS Automatic Flight Control System AFM Airplane Flight Manual AFMS Airplane Flight Manual Supplement AFRM airframe AGL Above Ground Level AHRS Attitude and Heading Reference System AIM Aeronautical Information Manual AIRMET Airman’s Meteorological Information ALRT alert ALT altitude ALT, ALTN alternator AMPS amperes ANNUNC annunciation ANT antenna AOPA Aircraft Owners & Pilots Association AP autopilot AP DISC autopilot disconnect APR approach APT airport, aerodrome ARINC Aeronautical Radio Incorporated ARSPC airspace ARTCC Air Route Traffic Control Center ARV arrival AS airspeed ASB Aviation Support Branch ASOS Automated Surface Observing System ATC Air Traffic Control ATCRBS ATC Radar Beacon System ATIS Automatic Terminal Information Service ATK along-track AUTOSEQ automatic sequence AUX auxiliary AWOS Automated Weather Observing System B ALT barometric altitude BARO barometric setting BATT battery BC backcourse Bearing The compass direction from the present position to a destination waypoint. BFO beat frequency oscillator BKSP backspace 190-00728-06 Rev. A BRG bearing C center runway ºC degrees Celsius CA Course to Altitude CALC calculator Calibrated Airspeed Indicated airspeed corrected for installation and instrument errors. CD Course to DME distance CDI Course Deviation Indicator CDU Control Display Unit CF Course to Fix CHT Cylinder Head Temperature CHKLIST checklist CHNL channel CI Course to Intercept CLD cloud CLR clear cm centimeter CNS Communication, Navigation, & Surveillance CO carbon monoxide COM communication radio CONFIG configuration COOL coolant COPLT co-pilot Course The line between two points to be followed by the aircraft. Course to Steer The recommended direction to steer in order to reduce course error or stay on course. Provides the most efficient heading to get back to the desired course and proceed along the flight plan. CR Course to Radial CRG Cockpit Reference Guide CRNT current Crosstrack Error The distance the aircraft is off a desired course in either direction, left or right. CRS course CRS Course to Steer CRSR cursor CTA Control Area CTRL control Cumulative The total of all legs in a flight plan. CVR Cockpit Voice Recorder CVRG coverage CWS control wheel steering CYL cylinder D ALT density altitude Embraer Prodigy® Flight Deck 100 Pilot’s Guide 701 APPENDIX C DB, DBASE database dBZ decibels ‘Z’ (radar return) DCLTR, DECLTR declutter DEC FUEL decrease fuel deg degree DEIC, DEICE de-icing DEP departure Desired Track The desired course between the active “from” and “to” waypoints. DEST destination DF Direct to Fix DFLT default DGRD degrade DH decision height Dilution of Precision A measure of GPS satellite geometry quality on a scale of one to ten (lower numbers equal better geometry, where higher numbers equal poorer geometry). DIR direction DIS distance Distance The ‘great circle’ distance from the present position to a destination waypoint. DME Distance Measuring Equipment DOP Dilution of Precision DP Departure Procedure DPRT departure DR dead reckoning DSBL disabled DTK Desired Track E ECU Efficiency empty, east Engine Control Unit A measure of fuel consumption, expressed in distance per unit of fuel. EGT Exhaust Gas Temperature EIS Engine Indication System EGNOS European Geostationary Navigation Overlay Service ELEV elevation ELEV elevator EMERGCY emergency EMI Electromagnetic Interference ENDUR endurance Endurance Flight endurance, or total possible flight time based on available fuel on board. ENG engine ENGD engaged ENR enroute 702 Enroute Safe Altitude The recommended minimum altitude within ten miles left or right of the desired course on an active flight plan or direct-to. ENT enter EPE Estimated Position Error EPU Estimated Position Uncertainty ERR error ESA Enroute Safe Altitude Estimated Position Error A measure of horizontal GPS position error derived by satellite geometry conditions and other factors. Estimated Time of Arrival The estimated time at which the aircraft should reach the destination waypoint, based upon current speed and track. Estimated Time Enroute The estimated time it takes to reach the destination waypoint from the present position, based upon current ground speed. ETA Estimated Time of Arrival ETE Estimated Time Enroute EXPIRD expired ºF degrees Fahrenheit FA Course From Fix to Altitude FAA Federal Aviation Administration FADEC Full Authority Digital Engine Control FAF Final Approach Fix FAIL failure FC Course From Fix to Distance FCC Federal Communication Commission FCST forecast FD Course From Fix to DME Distance FD flight director FDE Fault Detection and Exclusion FFLOW fuel flow FIS-B Flight Information Services-Broadcast FISDL Flight Information Service Data Link FL flight level FLC Flight Level Change FM Course From Fix to Manual Termination FMS Flight Management System FOB Fuel On Board FPL flight plan fpm feet per minute FREQ frequency FRZ freezing FSS Flight Service Station ft foot/feet Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX C Fuel Flow Fuel On Board The fuel flow rate, expressed in units of fuel per hour. The total amount of usable fuel on board the aircraft. G/S, GS glideslope GA go-around gal, gl gallon(s) GBOX gearbox GDC Garmin Air Data Computer GDL Garmin Satellite Data Link GDU Garmin Display Unit GEA Garmin Engine/Airframe Unit GEO geographic GFC Garmin Flight Control GIA Garmin Integrated Avionics Unit GLS Global Navigation Satellite Landing System GMA Garmin Audio Panel System GMC Garmin Mode Controller GMT Greenwich Mean Time GMU Garmin Magnetometer Unit GND ground gph gallons per hour GPS Global Positioning System Grid MORA Grid Minimum Off-Route Altitude; one degree latitude by one degree longitude in size and clears the highest elevation reference point in the grid by 1000 feet for all areas of the grid Groundspeed The velocity that the aircraft is travelling relative to a ground position. Ground Track see Track GRS Garmin Reference System GS Ground speed GTX Garmin Transponder HA Hold Terminating at Altitude HDG heading Heading The direction an aircraft is pointed, based upon indications from a magnetic compass or a properly set directional gyro. HF Hold Terminating at Fix HFOM Horizontal Figure of Merit Hg mercury HI high HI SENS High Sensitivity HM Hold with Manual Termination Horizontal Figure of Merit A measure of the uncertainty in the aircraft’s horizontal position. 190-00728-06 Rev. A hPa hectopascal HPL Horizontal Protection Level hr hour HSDB High-Speed Data Bus HSI Horizontal Situation Indicator HT heat HUL Horizontal Uncertainty Level Hz Hertz I Inner Marker IAF Initial Approach Fix IAT Indicated Air Temperature ICAO International Civil Aviation Organization ICS Intercom System ID Identification/Morse Code Identifier IDENT, IDNT identification IF Initial Fix IFR Instrument Flight Rules IG Imperial gallon ILS Instrument Landing System IMC Instrument Meteorological Conditions in inch INACTV inactive INC FUEL increase fuel IND indicated Indicated Information provided by properly calibrated and set instrumentation on the aircraft panel. INFO information in HG inches of mercury INT intersection(s) INTEG integrity (RAIM unavailable) IrDA, IRDA Infrared Data Association KEYSTK key stuck kg kilogram kHz kilohertz km kilometer kt knot L left, left runway LAT latitude LBL label lb pound LCD Liquid Crystal Display LCL local LED Light Emitting Diode Left Over Fuel On Board The amount of fuel remaining on board after the completion of one or more legs of a flight plan or direct-to. Embraer Prodigy® Flight Deck 100 Pilot’s Guide 703 APPENDIX C Left Over Fuel Reserve The amount of flight time remaining, based on the amount of fuel on board after the completion of one or more legs of a flight plan or direct-to, and a known consumption rate. Leg The portion of a flight plan between two waypoints. LIFR Low Instrument Flight Rules LNAV Lateral Navigation LO low LOC localizer LOI loss of integrity (GPS) LON longitude LPV Localizer Performance with Vertical guidance LRU Line Replacement Unit LT left LTNG lightning LVL level M Middle Marker m meter MAG Magnetic MAG VAR Magnetic Variation MAHP Missed Approach Hold Point MAN IN manifold pressure (inches Hg) MAN SQ Manual Squelch MAP Missed Approach Point MASQ Master Avionics Squelch MAX maximum MAXSPD maximum speed (overspeed) MDA barometric minimum descent altitude MET manual electric trim METAR Meteorological Aviation Routine MEPT manual electric pitch trim MFD Multi Function Display MGRS Military Grid Reference System MHz megahertz MIC microphone MIN minimum Minimum Safe Altitude Uses Grid MORAs to determine a safe altitude within ten miles of the aircraft present position. MKR marker beacon MOA Military Operations Area MOV movement mpm meters per minute MSA Minimum Safe Altitude MSAS Multi-functional Satellite Augmentation System MSG message 704 MSL Mean Sea Level MT meter mV millivolt(s) MV DB Magnetic Field Variation Database MVFR Marginal Visual Flight Rules N north NAV navigation NAVAID NAVigation AID NDB Non-directional Beacon NEXRAD Next Generation Radar nm nautical mile(s) NoPT No Procedure Turn Required (procedure shall not be executed without ATC clearance) NRST nearest O Outer Marker OAT Outside Air Temperature OBS Omni Bearing Selector OFST offset OXY oxygen P ALT pressure altitude PA Passenger Address PA Proximity Advisory PASS passenger(s) PC personal computer PFD Primary Flight Display PI Procedure Turn to Course Intercept PIT, PTCH pitch POSN position PPM parts per million P. POS Present Position PRES, PRESS pressure PROC procedure(s), procedure turn psi pounds per square inch PT Procedure Turn PTK parallel track PTT Push-to-Talk PWR power QTY quantity R right, right runway RAD radial RAIM Receiver Autonomous Monitoring RAM random access memory REF reference Embraer Prodigy® Flight Deck 100 Pilot’s Guide Integrity 190-00728-06 Rev. A APPENDIX C REM remaining (fuel remaining above Reserve) REQ required RES reserve (fuel reserve entered by pilot) REV reverse, revision, revise RF Constant Radius Turn to Fix RMI Radio Magnetic Indicator RMT remote RNG range RNWY runway ROL roll ROM read only memory rpm revolutions per minute RST FUEL reset fuel RSV reserve (fuel reserve entered by pilot) RT right RVRSNRY reversionary RX receive S south SA Selective Availability SAT Static Air Temperature SBAS Satellite-Based Augmentation System SCIT Storm Cell Identification and Tracking SD Secure Digital sec second(s) SEL, SLCT select SFC surface SIAP Standard Instrument Approach Procedures SID Standard Instrument Departure SIGMET Significant Meteorological Information Sim simulator SLP/SKD slip/skid SMBL symbol SPD speed SPI Special Position Identification SPKR speaker SQ squelch SRVC, SVC service STAL stall STAR Standard Terminal Arrival Route STATS statistics STBY standby STD standard SUA Special Use Airspace SUSP suspend SVS Synthetic Vision System SW software SYS system 190-00728-06 Rev. A T true TA Traffic Advisory TACAN Tactical Air Navigation System TAF Terminal Aerodrome Forecast TAS True Airspeed TAS Traffic Advisory System, true airspeed TAT Total Air Temperature TAWS Terrain Awareness and Warning System TCA Terminal Control Area TCAS Traffic Collision Avoidance System TEL telephone TEMP temperature TERM terminal TF Track Between Two Fixes TFR Temporary Flight Restriction T HDG True Heading TIS Traffic Information System TIT Turbine Inlet Temperature TKE Track Angle Error TMA Terminal Maneuvering Area TMR/REF Timer/Reference Topo topographic Track Direction of aircraft movement relative to a ground position; also ‘Ground Track’ Track Angle Error The angle difference between the desired track and the current track. TRG target TRK track TRSA Terminal Radar Service Area TRUNC truncated TTL total TURN procedure turn TX transmit UNAVAIL unavailable USR user UTC Coordinated Universal Time UTM/UPS Universal Transverse Mercator / Universal Polar Stereographic Grid V, Vspeed velocity (airspeed) VA Heading Vector to Altitude VAPP VOR approach VAR variation VD Heading Vector to DME Distance Vdc volts, direct current VERT vertical Embraer Prodigy® Flight Deck 100 Pilot’s Guide 705 APPENDIX C Vertical Figure of Merit A measure of the uncertainty in the aircraft’s vertical position. Vertical Speed Required The vertical speed necessary to descend/ climb from a current position and altitude to a defined target position and altitude, based upon current groundspeed. VFOM Vertical Figure of Merit VFR Visual Flight Rules VHF Very High Frequency VI Heading Vector to Intercept VLOC VOR/Localizer Receiver VM Heading Vector to Manual Termination VMC Visual Meteorological Conditions VNAV, VNV vertical navigation VOL volume VOR VHF Omni-directional Range VORTAC very high frequency omnidirectional range station and tactical air navigation VPL Vertical Protection Level VPROF VNV profile, vertical profile VPTH VNV path, vertical path VR Heading Vector to Radial VS vertical speed VSI Vertical Speed Indicator VSR Vertical Speed Required VTF vector to final W watt(s), west WAAS Wide Area Augmentation System WARN warning (GPS position error) WGS-84 World Geodetic System - 1984 WPT waypoint(s) WW world wide WX weather XFER, XFR transfer XPDR transponder XTALK cross-talk XTK cross-track 706 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX D FREQUENTLY ASKED QUESTIONS If a particular aspect of system operational capability is not addressed by these commonly asked questions or in the index, contact Garmin (see the copyright page or back cover for contact information) or a Garmin-authorized dealer. Garmin is dedicated to supporting its products and customers. What is SBAS? The Satellite Based Augmentation System (SBAS) uses a system of ground stations to correct any GPS signal errors. These ground stations correct for errors caused by ionospheric disturbances, timing, and satellite orbit errors. It also provides vital integrity information regarding the health of each GPS satellite. The signal correction is then broadcast through geostationary satellites. This correction information can then be received by any SBAS-enabled GPS receiver. SBAS is designed to provide the additional accuracy, availability, and integrity necessary to enable users to rely on GPS for all phases of flight. There are several SBAS systems serving different parts of the world. The Wide Area Augmentation System (WAAS) is currently available in the United States, including Alaska and Hawaii. The European Geostationary Navigation Overlay Service (EGNOS) offers coverage of Europe, parts of the middle east and northern Africa. The Multi-functional Satellite Augmentation System (MSAS) covers mainly Japan and parts of northern Australia. How does SBAS affect approach operations? Both LNAV/VNAV and LPV approaches use the accuracy of SBAS to include vertical (glide path) guidance capability. The additional accuracy and vertical guidance capability allows improved instrument approaches to an expanded number of airports throughout the U.S. The implementation of LPV approaches further improves precision approach capabilities. LPV approaches are designed to make full use of the improved GPS signal from the SBAS. This approach combines the LNAV/ VNAV vertical accuracy with lateral guidance similar to the typical Instrument Landing System (ILS). LPV approaches allow lower approach minimums. What is RAIM and how does it affect approach operations? RAIM is an acronym for Receiver Autonomous Integrity Monitoring. RAIM is a GPS receiver function that performs the following functions: • Monitors and verifies integrity and geometry of tracked GPS satellites • Notifies the pilot when satellite conditions do not provide the necessary coverage to support a certain phase of flight • Predicts satellite coverage of a destination area to determine whether the number of available satellites is sufficient to satisfy requirements NOTE: If RAIM is not predicted to be available for the final approach course, the approach does not become active, as indicated by the “RAIM not available from FAF to MAP” message and the LOI annunciation flagging on the HSI. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 707 APPENDIX D For RAIM to work correctly, the GPS receiver must track at least five satellites. A minimum of six satellites is required to allow RAIM to eliminate a single corrupt satellite from the navigation solution. RAIM ensures that satellite geometry allows for a navigation solution calculation within a specified protection limit (2.0 nm for oceanic and en route, 1.0 nm for terminal, and 0.3 nm for non-precision approaches). The system monitors RAIM and issues an alert message when RAIM is not available (see Appendix A). Without RAIM, GPS position accuracy cannot be monitored. If RAIM is not available when crossing the FAF, the pilot must fly the missed approach procedure. Why are there not any approaches available for a flight plan? Approaches are available for the final destination airport in a flight plan or as a direct-to (keep in mind that some VOR/VORTAC identifiers are similar to airport identifiers). If a destination airport does not have a published approach, the system indicates “NONE” for the available procedures. What happens when an approach is selected? Can a flight plan with an approach, a departure, or an arrival be stored? When an approach, departure, or arrival is loaded into the active flight plan, a set of approach, departure, or arrival waypoints is inserted into the flight plan, along with a header line showing the title of the selected instrument procedure. The original en route portion of the flight plan remains active, unless the instrument procedure is activated. This may be done either when the procedure is loaded or at a later time. Flight plans can also be stored with an approach, a departure, or an arrival. Note that the active flight plan is erased when the system is turned off. Also, the active flight plan is overwritten when another flight plan is activated. When storing flight plans with an approach, a departure, or an arrival, the system uses the waypoint information from the current database to define the waypoints. If the database is changed or updated, the system automatically updates the information, provided the procedure has not been modified. Should an approach, departure, or arrival procedure no longer be available, the flight plan becomes locked until the procedure is deleted from the flight plan. Can “slant Golf” (“/G”) be filed using the Prodigy® System? “/G” may be filed for a flight plan. The Prodigy® System meets the requirements of TSO-C145a Class 3 and ETSO C145 Class 3 installations. GPS approaches are not to be flown with an expired database. See the approved Pilot’s Operating Handbook (POH) as well as the Aeronautical Information Manual (AIM) for more information. What does the OBS Softkey do? The OBS Softkey is used to select manual sequencing of waypoints. Activating OBS mode sets the current active-to waypoint as the primary navigation reference and prevents the system from sequencing to the next waypoint in a flight plan. When OBS mode is cancelled, automatic waypoint sequencing is continued, and the system automatically activates the next waypoint in the flight plan once the aircraft has crossed the present active waypoint. 708 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX D Normal (OBS not activated) • Automatic sequencing of waypoints OBS • Manual sequencing - ‘holds’ on selected waypoint • Manual course change on HSI not possible • Manually select course to waypoint from HSI • Always navigates ‘TO’ the active waypoint • Indicates ‘TO’ or ‘FROM’ waypoint • Must be in this mode for final approach course • Cannot be set for final approach course or published holding patterns When OBS mode is active, the system allows the pilot to set a desired course to/from a waypoint using the CRS/BARO Knob and HSI (much like a VOR). The most common application for using the OBS Softkey is the missed approach. The system suspends automatic waypoint sequencing (indicated by a ‘SUSP’ annunciation placed on the HSI) when the missed approach point (MAP) is crossed. This prevents the system from automatically sequencing to the missed approach holding point (MAHP). During this time, the OBS Softkey designation changes to SUSP. Pressing the SUSP Softkey reactivates automatic waypoint sequencing. The OBS Softkey then resumes its normal functionality. Why does the system not automatically sequence to the next waypoint? The system only sequences flight plan waypoints when automatic sequencing is enabled (i.e., no “OBS” or ‘SUSP’ annunciation). For automatic sequencing to occur, the aircraft must also cross the “bisector” of the turn being navigated. The bisector is a line passing through the waypoint common to two flight plan legs at an equal angle from each leg. How can a waypoint be skipped in an approach, a departure, or an arrival? The system allows the pilot to manually select any approach, departure, or arrival leg as the active leg of the flight plan. This procedure is performed on the MFD from the Active Flight Plan Page by highlighting the desired waypoint and selecting the ACT LEG Softkey then the ENT Key to approve the selection. The GPS then provides navigation along the selected flight plan leg. When does turn anticipation begin? The system smooths adjacent leg transitions based on a normal 15° bank angle (with the ability to roll up to 30°) and provides three pilot cues for turn anticipation: • A waypoint alert (‘Next DTK ###° in # seconds’ or ‘Next HDG ###° in # seconds’) appears on the PFD 10 seconds before the turn point and flashes as it counts down to zero. • A flashing turn advisory (‘Turn [right/left] to ###° in # seconds’) appears on the PFD 10 seconds before the turn and flashes as it counts down to zero. ‘Turn [right/left] to ###° now’ or ‘Next [DTK/HDG] to ###° now’ is displayed when the pilot is to begin the turn and the HSI (GPS mode) automatically sequences to the next DTK or HDG value. • The To/From indicator on the HSI flips momentarily to indicate that the midpoint of the turn has been crossed. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 709 APPENDIX D When does the CDI scale change? Once a departure is activated, the Prodigy® Course Deviation Indicator (CDI) full scale deflection is set to 0.3 nm. The CDI scale changes to 1.0 nm (terminal mode) then ramps up to 2.0 nm (enroute mode) at 30 nm from the departure airport. When 31 nm from the destination, the CDI scale smoothly transition from 2.0 nm back to 1.0 nm (terminal mode). At 2.0 nm before the FAF during an active approach, the CDI scale transitions down further based on the type of approach activated (LNAV, LNAV/VNAV, LPV). When a missed approach is activated, the CDI is set to 0.3 nm. See the Flight Instruments Section for more details on CDI scaling. Why does the HSI not respond like a VOR when OBS mode is active? Unlike a VOR, the CDI scale used on GPS equipment is based on the crosstrack distance to the desired course, not on the angular relationship to the destination. Therefore, the CDI deflection on the GPS is constant regardless of the distance to the destination and does not become less sensitive when further away from the destination. What is the correct missed approach procedure? How is the missed approach holding point selected? To comply with TSO specifications, the system does not automatically sequence past the MAP. The first waypoint in the missed approach procedure becomes the active waypoint when the SUSP Softkey is selected after crossing the MAP, or the go-around button is pressed. All published missed approach procedures must be followed, as indicated on the approach plate. To execute the missed approach procedure prior to the MAP (not recommended), select the Active Flight Plan Page and use the ACT LEG Softkey to activate the missed approach portion of the procedure. After a missed approach, how can the same approach be re-selected? How can a new approach be activated? NOTE: Do not attempt to reactivate the current approach prior to crossing the missed approach point (MAP). If an attempt to do so is made, an alert message “Are you sure you want to discontinue the current approach?” appears. The system directs the pilot back to the transition waypoint and does not take into consideration any missed approach procedures, if the current approach is reactivated. After flying the missed approach procedure, the pilot may reactivate the same approach for another attempt by pressing the PROC Key. Once the clearance is given for another attempt, activate the approach by highlighting ‘ACTIVATE APPROACH’ using the large FMS Knob and pressing the ENT Key. The system provides navigation along the desired course to the waypoint and rejoins the approach in sequence from that point. To activate a new approach for the same airport, select the new procedure by pressing the PROC Key. Choose ‘SELECT APPROACH’, select the desired approach from the list shown, and press the ENT Key. Select the desired transition, then activate the approach using the ENT Key. To activate a new approach to a different airport, press the Direct-to Key and select the desired airport using the FMS Knobs. Press the ENT Key to accept the selected airport, then follow the steps in the preceding paragraph to select an approach for the new airport. 710 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX E GENERAL TIS INFORMATION INTRODUCTION NOTE: Aircraft without an operating transponder are invisible to TIS. The Traffic Information Service (TIS) provides traffic advisory information to non-TAS/TCAS-equipped aircraft. TIS is a ground-based service providing the relative locations of all ATCRBS Mode-A and Mode-C transponder equipped aircraft within a specified service volume. The TIS ground sensor uses real-time track reports to generate traffic notification. The system displays TIS traffic information on the Traffic Map Page of the MFD. TIS information may also be displayed for overlay on the MFD Navigation Map Page, as well as on the PFD Inset Map. Surveillance data includes all transponder-equipped aircraft within the coverage volume. The system displays up to eight traffic targets within a 7.5 nm radius, from 3,000 feet below, to 3,500 feet above the requesting aircraft. TIS VS. TAS/TCAS The Traffic Information System (TIS) is a ground-based service that requires contact with a ground station through a datalink radio in order to receive traffic information. Traffic Advisory (TAS) and Traffic Collision Avoidance Systems (TCAS) are self-contained. TAS/TCAS uses an airborne interrogator with a half-second update rate, while TIS utilizes the terminal Mode-S ground interrogator and accompanying data link to provide a five-second update rate. TIS and TAS/TCAS have similar ranges. TIS LIMITATIONS NOTE: TIS is not intended to be used as a collision avoidance system and does not relieve the pilot of the responsibility to “see and avoid” other aircraft. TIS shall not be used for avoidance maneuvers during instrument meterorlogical conditions (IMC) or when there is no visual contact with the intruder aircraft. NOTE: Refer to the TIS Limitations section of the Aeronautical Information Manual (AIM) for a more comprehensive explanation. TIS relies on surveillance of the Mode-S radar system, which is a “secondary surveillance” radar system similar to that used by ATCRBS. Many limitations are inherent in secondary radar surveillance. Information provided by TIS is neither better nor more accurate than the information used by ATC. TIS is intended only to assist in visual acquisition of other aircraft in visual meterological conditions (VMC). While TIS is a useful aid for visual traffic avoidance, system limitations must be considered to ensure proper use. No recommended avoidance maneuvers are given, nor authorized, as a direct result of a TIS intruder display or TIS advisory. • TIS operation may be intermittent during turns or other maneuvering. • TIS is dependent on two-way, line-of-sight communications between the aircraft and the Mode-S radar antenna. Whenever the structure of the aircraft comes between the transponder antenna and the groundbased radar antenna, the signal may be temporarily interrupted. • Other limitations and anomalies associated with TIS are described in the AIM. 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 711 APPENDIX E WARNING: Garmin is not responsible for Mode S geographical coverage. Operation of the ground stations is the responsibility of the FAA. Refer to the AIM for a Terminal Mode S radar site map. NOTE: TIS is unavailable at low altitudes in many areas of the United States. This is often the case in mountainous regions. TIS information is collected during a single radar sweep. Collected information is then sent through the Mode S uplink on the next radar sweep. Because of this, the surveillance information is approximately five seconds old. TIS ground station tracking software uses prediction algorithms to compensate for this delay. These algorithms use track history data to calculate expected intruder positions consistent with the time of display. Occasionally, aircraft maneuvering may cause variations in this calculation and create slight errors on the Traffic Map Page. Errors affect relative bearing information and target track vector. This can cause a delay in the displayed intruder information. However, intruder distance and altitude typically remain relatively accurate and may be used to assist in spotting traffic. The following errors are common examples: • When the client or intruder aircraft maneuvers excessively or abruptly, the tracking algorithm may report incorrect horizontal position until the maneuvering aircraft stabilizes. • When a rapidly closing intruder is on a course that intercepts the client aircraft course at a shallow angle (either overtaking or head-on) and either aircraft abruptly changes course within 0.25 nm, TIS may display the intruder aircraft on the incorrect side of the client aircraft. These are rare occurrences and are typically resolved within a few radar sweeps once the client/intruder aircraft course stabilizes. Pilots using TIS can provide valuable assistance in the correction of malfunctions by reporting observations of undesirable performance. Reports should identify the time of observation, location, type and identity of the aircraft, and describe the condition observed. Reports should also include the type of transponder and transponder software version. Since TIS performance is monitored by maintenance personnel, not ATC, malfunctions should be reported in the following ways: • By telephone to the nearest Flight Service Station (FSS) facility • By FAA Form 8000-7, Safety Improvement Report (postage-paid card can be obtained at FAA FSSs, General Aviation District Offices, Flight Standards District Offices, and General Aviation Fixed Base Operators) 712 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX F DISPLAY SYMBOLS NOTE: Refer to the GPS Navigation Section for the topography legend and the Hazard Avoidance Section for SiriusXM Weather Product legends. AIRPORT LINE SYMBOLS Item Symbol Unknown Airport Item ICAO Control Area Class B Airspace Symbol Mode C Tower Area Non-towered, Non-serviced Airport Warning Area Prohibited Area Alert Area Restricted Area Caution Area Training Area Danger Area Unknown Area Class C Terminal Radar Service Area Mode C Area Towered, Non-serviced Airport Non-towered, Serviced Airport Towered, Serviced Airport Military Operations Area (MOA) Restricted (Private) Airport State or Province Border Heliport International Border NAVAIDS Road Item Symbol Intersection LOM (compass locator at outer marker) Railroad Latitude/Longitude NDB (non-directional radio beacon) VOR VOR/DME VOR/ILS VORTAC TACAN 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 713 APPENDIX F MISCELLANEOUS TRAFFIC Item Symbol ARTCC Frequency or FSS Frequency Traffic Symbol Description Non-Threat Traffic Default Map Pointer Proximity Advisory (PA) (Not avialable with TIS Elevation Pointer Traffic Advisory (TA) Wind Vector Traffic Advisory Off Scale Measuring Pointer Resolution Advisory (RA) (TCAS II only) Resolution Advisory Off Scale (TCAS II only) Overzoom Indicator Terrain Proximity or TAWS Enabled Traffic Enabled User Waypoint Vertical Navigation Along Track Waypoint Parallel Track Waypoint Unanchored Flight Path Waypoint Top of Descent (TOD) Bottom of Descent (BOD) Navigating using Dead Reckoning 714 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A APPENDIX F TERRAIN AVOIDANCE COLORS AND SYMBOLS Potential Impact Point Terrain Above Aircraft Altitude Projected Flight Path 100 ft Threshold 1000 ft Unlighted Obstacle Terrain Color Terrain Location Red (WARNING) Terrain above, or within 100 ft below the aircraft altitude Yellow (CAUTION) Terrain between 100 ft and 1000 ft below the aircraft altitude Black Terrain more than 1000 ft below the aircraft altitude TAWS Color Chart Figure E-3 TAWS Potential Impact Points Obstacle Symbol Unlighted Obstacle Lighted Obstacle Height < 1000 ft AGL > 1000 ft AGL < 1000 ft AGL > 1000 ft AGL Obstacle Color Obstacle Location Red (WARNING) Obstacle within 100 ft of or above aircraft altitude Yellow (CAUTION) Obstacle within 1000 ft of aircraft altitude Gray Obstacle more than 1000 ft below aircraft altitude Obstacle Symbols and Colors 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide 715 APPENDIX F HAZARD AVOIDANCE FEATURES Feature Symbol Terrain Proximity/TAWS display enabled Traffic display enabled NEXRAD display enabled Cloud Top display enabled Echo Top display enabled XM Lightning display enabled Cell Movement display enabled SIGMETs/AIRMETs display enabled METARs display enabled City Forecast display enabled Surface Analysis display enabled Freezing Levels display enabled Winds Aloft display enabled County Warnings display enabled Cyclone Warnings display enabled Icing Potential (CIP and SLD) (ICNG) Pilot Weather Report (PIREPs) Air Report (AIREPs) Turbulence (TURB) Loss of hazard avoidance feature (due to loss of GPS position) 716 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A INDEX A Airport Directory------------------------------------- 693, 694 Abnormal engine operations------------------------------119 Access Code-------------------------------------------------374 Activate a Flight Plan---------------------------------------257 Active database---------------------------------------------691 Active frequency------------------------------------- 126, 145 ADF---------------------------------------------------------153 AC-U-KWIK-------------------------------547, 694, 695, 607 ADF ADF mode------------------------------------ 136, 153, 155 ANT mode------------------------------------------ 136, 155 ADF/BFO---------------------------------------------- 136, 155 ADF/DME tuning--------------------------------------------156 AFCS status box---------------------------------------------- 62 AHRS----------------------------- 30, 32, 667, 676, 677, 678 Airborne Color Weather Radar----------------------------399 Aircraft symbol----------------------------------------------- 68 Air Data Computer---------------------------1, 32, 665, 667 AIREP---------------------------------------------------------369 Airport Information-----------------------------------------------215 Nearest----------------------------------------------------- 52 Airport Directory------------------ 547, 607, 608, 609, 608 Airspace alerts-----------------------------------------------230 Airspace Alerts----------------------------------------------231 Airspeed bug----------------------------------------- 507, 515 Airspeed Indicator---------------------------------------62, 64 Airspeed Reference----------------------------- 62, 509–510 Airways-------------------------------------------------------- 23 Collapsed--------------------------------------------------270 Expanded--------------------------------------------------270 Alert messages----------------------------------------------677 Alerts Airspace---------------------------------------------------- 49 Alerts, Aircraft-----------------------------------------------659 Along Track Offset------------------------------------------262 ALT------------------------------------------------------------331 Altimeter--------------------------------------------------62, 69 Altitude alerting---------------------------------------------- 92 Altitude buffer------------------------------------------------ 49 Altitude constraints---------------------------------- 277, 318 Altitude Hold Mode----------------------------------------506 Altitude trend vector---------------------------------------- 69 Annunciations Test tone---------------------------------------------------- 54 Annunciations, Prodigy System---------------------------- 31 Annunciator lights------------------------------------------167 ANT/BFO-----------------------------------------------------155 Antenna Stabilization--------------------------------------416 Antenna Tilt--------------------------------------------------413 AOPA------------------------------- 547, 694, 695, 701, 607 AOPA Airport Directory-------------------------------------610 190-00728-06 Rev. A Approach-----------------------------------------------------708 Activating-------------------------------------------------292 ILS----------------------------------------------------------539 Loading--------------------------------------- 254, 289, 291 Missed-----------------------------------------------------542 Removing--------------------------------------------------292 WAAS------------------------------------------------------541 Approach channel----------------------------------- 254, 289 Approach Mode-------------------------------------- 525, 539 Approach Mode, AFCS-------------------------------------541 APR softkey------------------------------------------- 291, 299 Arrival procedure------238, 252, 285, 287, 316, 318, 327 Attitude---------------------------------------------------------- 1 Attitude & Heading Reference System-------------------665 Attitude indicator------------------------------ 62, 67, 67–68 Attitude Indicator-------------------------------------------485 Audio Panel Fail-Safe Operation--------------------------175 Aural alerts--------------------------------------------------687 Automatic Flight Control System (AFCS)--------- 497–546 Alerts and annunciations------------------------ 544–545 Controls-------------------------------------------- 498–499 Status Box-------------------------------------------------501 Automatic squelch------------------------------------------134 Automatic Thrust Reserve (ATR)------------------- 105–106 Automatic Thrust Reserve Status-------------------------106 Autopilot----------------------------------------497, 527–529 Autopilot Disconnect-------------------------------- 499, 519 Auto-tuning--------------------------------------------------151 Auto-tuning, COM------------------------------------------129 Auto-tuning, NAV-------------------------------------------148 Auto Zoom---------------------------------------------------183 Auxiliary Pages (AUX)--------------------------------------- 40 AUX - system status page-565, 567, 587, 588, 604, 605, 606, 609 Aviation Symbols------------------------------------- 195, 238 B Backlighting----------------------------------------------59, 60 Barometric setting----------------------------------62, 70–71 Baro Transition Alert----------------------------------------- 72 Basic Empty Weight----------------------------------------300 Basic Operating Weight------------------------------------300 Battery indications----------------------------------- 104, 108 Bearing/distance, measuring------------------------------190 Bearing information----------------------------------------- 63 Bearing line------------------------------------------- 411, 415 Bearing pointer----------------------------------------------- 78 Bearing source----------------------------------------------- 78 C Cabin speaker-----------------------------------------------167 Calibrated Airspeed-----------------------------------------296 Cargo---------------------------------------------------------301 Embraer Prodigy® Flight Deck 100 Pilot’s Guide I-1 INDEX CDI---------------------------- 288, 307, 318, 326, 333, 680 CELL MOV Softkey------------------------------------------355 Chart Not Available---------------------------------- 570, 591 Chart options----------------------------------------- 578, 598 CHART SETUP box----------------------------------- 584, 602 ChartView---------------------------------547, 568, 569, 587 Checklists--------------------------------------------- 652–653 Checklist softkeys-------------------------------------------652 City Forecast-------------------------------------------------360 CLD TOP Softkey------------------------------------- 353, 387 Clearance Recorder and Player---------------------------170 Closest Point-------------------------------------------------270 CLR Key-------------------------------------------------------166 Code selection softkeys------------------------------------164 COM channel spacing--------------------------------------133 COM frequency box----------------------------------------- 62 COM Frequency Box----------------------------------------126 Command Bars----------------------------------------------503 Commanded N1 Rating------------------------------------106 Comparator window---------------------------------------- 90 COM radio Channel spacing------------------------------------------ 52 COM Tuning Failure-----------------------------------------174 Connext Data Request-------------------------------------381 Controls Softkeys------------------------------------------------ 15–18 Control Wheel Steering (CWS)--------------------- 499, 528 Copy a Flight Plan------------------------------------------257 County Warnings--------------------------------------------365 Course deviation indicator (CDI)-----------------62, 79–80 Course Deviation Indicator (CDI)-------------------------- 52 Cruise Speed Control (CSC)-------------------------------108 Current Speed Control Arc--------------------------------106 Cyclone-------------------------------------------------------366 D Data Bar fields, MFD---------------------------------------- 51 Database------------------------------------------------------ 27 Databases----------------------------------------------------689 Database synchronization---------------------------------- 54 Database Synchronization-------------------- 690, 695, 696 Data link-------------------------------------------------------- 1 Data Link Receiver------------------------------------------658 Data Link Receiver troubleshooting----------------------657 Date and time------------------------------------------------ 48 Day/Night Views------------------------------------- 584, 602 Day View---------------------------------------------- 585, 603 DB Mismatch------------------------------------------------689 Dead reckoning---------------------------------------------- 97 Declutter------------------------------------------------------ 24 I-2 Declutter, display--------------------------------------------- 99 Delete Flight Plans------------------------------------------257 Deleting an entire airway--------------------------- 259, 260 Deleting an entire procedure----------------------- 259, 260 Deleting an individual waypoint------------------- 258, 259 Deleting Flight Plan Items---------------------------------258 Density Altitude---------------------------------------------298 Departure Select------------------------------------282, 285, 289, 292 Timer-------------------------------------------------------- 56 Departure procedure--------------------250, 264, 282, 284 Departure Time----------------------------------------------296 Digital audio entertainment---------------------------------- 4 Dilution of Precision (DOP)--------------------------------- 34 Direct-to-208, 232, 233, 234, 235, 236, 275, 276, 316, 318, 333 Display backup----------------------------------------- 29, 125 Diversity transponder---------------------------------------157 DME HOLD mode-----------------------------------------------156 NAV1 mode-----------------------------------------------156 NAV2 mode-----------------------------------------------156 Tuning mode--------------------------------------- 153, 156 DME audio---------------------------------------------------146 DME information-----------------------------------------63, 79 Door status--------------------------------------------------111 Dual navigation database---------------------------------691 E ECHO TOP Softkey------------------------------------------352 Electrical indications--------------------------------- 108, 114 Electronic checklists--------------------------- 652, 653, 654 Emergency checklist----------------------------------------653 Emergency frequency---------------------------------------174 Engine failure------------------------------------------------119 Engine Fan Speed---------------------------------------------------------106 Engine fire---------------------------------------------------119 Engine High Pressure Compressor Speed---------------106 Engine Indication System (EIS)--------------------- 104–111 Engine maintenance----------------------------------------118 Engine rotation speeds----------------------------- 104, 106 Entering Flight ID-------------------------------------------157 Entertainment inputs---------------------------------------171 Environmental Control System (ECS)------------- 112–113 Estimated Landing Fuel------------------------------------302 Estimated Position Error (EPE)----------------------------- 34 Ethernet------------------------------------------------------- 28 Excess Fuel Weight-----------------------------------------302 Export Flight Plan-------------------------------------------688 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A INDEX F Failure Input-------------------------------------------------------- 31 Field of View (SVS)------------------------------------------206 Flap indicator-----------------------------------------110, 120, Flight director-----------------------------------497, 500–501 Modes, lateral------------------------------------- 520–546 Modes, vertical------------------------------------ 504–518 Switching--------------------------------------------------502 Flight ID------------------------------------------------------166 Flight instruments--------------------------------------- 61–76 Flight Level Change Mode-------------------------- 509, 535 Flight plan Closest point to reference------------------------------270 Storing-----------------------------------------------------708 Flight timer---------------------------------------------------- 55 FliteCharts-------------------------------------- 547, 589, 590 FliteCharts cycle---------------------------------------------605 FliteCharts expiration--------------------------------------605 FliteCharts functions---------------------------------------590 FPA----------------------------------------------------- 277, 323 Freezing Levels----------------------------------------------361 Frequency Nearest----------------------------------------------------228 Frequency spacing------------------------------------------133 Frequency transfer arrow----------------------------------127 Frequently asked questions--------------------------------707 Fuel Efficiency--------------------------------------------------298 Endurance-------------------------------------------------298 Remaining-------------------------------------------------298 Required---------------------------------------------------298 Fuel indications-------------------------------- 104, 108, 115 Fuel on Board---------------------------------- 298, 301, 302 Fuel Statistics------------------------------------------------298 G Gain-----------------------------------------------------------414 Garmin AFCS------------------------------------------------497 Garmin Connext--------------------------------------------547 GDC 74A-------------------------------------------------------- 1 GDL 69/69A---------------------------------------------------- 1 GDU 1040------------------------------------------------------ 1 GEA 71---------------------------------------------------------- 1 Geodetic Sea Level (GSL)--------------------------- 422, 436 GIA 63----------------------------------------------------------- 1 Glidepath-----------------------------------------------------331 Glidepath Indicator------------------------------------------ 73 Glidepath Mode-------------------------------------- 516, 525 Glidepath Mode (GP)---------------------------------------541 Glideslope----------------------------------------------------331 190-00728-06 Rev. A Glideslope indicator----------------------------------------- 73 Glideslope Mode------------------------------------- 518, 539 Global Positioning System (GPS) Navigation----------------------------------------- 232–336 Receiver information--------------------------------- 33–35 GMA 1347---------------------------------------------1, 27, 59 GMU 44--------------------------------------------------------- 1 Go Around Mode------------------------------519, 542–543 GPS Window-------------------------------------------------696 Ground Mapping--------------------------------------------418 Groundspeed------------------------------------------------- 56 GRS 77---------------------------------------------------------- 1 GSL----------------------------------------------------- 422, 436 GTS 850------------------------------------------------------469 GTX 33---------------------------------------------------------- 1 H Heading bug----------------------------------------------62, 75 Heading Bug-------------------------------------------------- 62 Heading indicator-------------------------------------------- 62 Heading Select Mode--------------------------------------522 HI SENS-------------------------------------------------------152 Horizontal Scan-------409, 410, 411, 412, 413, 417, 418 Horizontal Situation Indicator (HSI)--------------62, 74–76 HSI double green arrow------------------------------------145 HSI magenta arrow-----------------------------------------145 HSI single green arrow-------------------------------------145 Hurricane-----------------------------------------------------366 I Icing-----------------------------------------------------------367 IDENT function----------------------------------------------166 ID indicator--------------------------------------------------147 ILS approach-------------------------------------------------539 Import Flight Plan-------------------------------------------688 Indicated airspeed------------------------------------------- 64 Indicated Altitude-------------------------------------------296 Initialization (system)---------------------------------------- 27 Intercom------------------------------------------------------168 Intersection Information---------------------------------------- 216–217 Interstage Turbine Temperature---------------------------106 Interstage Turbine Temperature (ITT)-------------------- 119, Inverting a flight plan--------------------------------------257 IOI------------------------------------------429, 443, 682, 684 Iridium------------------------------------------------- 610, 618 Iridium satellite network--- 610, 611, 617, 622, 624, 626 ITT Steady State Limit--------------------------------------106 J Jeppesen aviation database-------------------------------690 Embraer Prodigy® Flight Deck 100 Pilot’s Guide I-3 INDEX K Key(s)------------------------------------------------------- 9, 11 L Landing Field Elevation (LFE)-----------------------------109 Landing gear status--------------------------------- 104, 110 Land Symbols------------------------------------------------194 Lateral modes, flight director----------------------- 520–546 LNAV----------------------------------------------------------307 LO SENS------------------------------------------------------152 Low Altitude Annunciation--------------------------------- 93 LPV----------------------------------------------- 307, 333, 530 M Mach number------------------------------------------------ 64 Mach number indicator------------------------------------- 62 Magnetometer-------------------------------------------- 1, 31 Map pages---------------------------------------------------- 39 Map Panning------------------------------------------------185 Marker beacon----------------------------------------- 91, 152 MASQ processing-------------------------------------------121 Measurement units, changing displayed----------------- 48 Menus--------------------------------------------------------- 37 Message advisories---669, 670, 672, 676, 678, 679, 680 Messages Reminder--------------------------------------------------- 56 Messages window------------------------------------------651 MFD Data Bar fields----------------------------------------- 51 Minimum descent altitude------------------------------63, 93 MISCOMP----------------------------------------------------664 Missed approach--------------------------------------------542 Missed Approach----------------- 238, 293, 303, 307, 333 MKR/MUTE--------------------------------------------------152 Mode S--------------------------------------------18, 157, 163 Mode selection softkeys--------- 158, 159, 160, 161, 162 Mode S Transponder----------------------------------------157 GTX 33/33D Controls-----------------------------------158 GTX 33/33D Mode Selection---------------------------159 TCAS II Transponder Controls--------------------------161 TCAS II Transponder Mode Selection------------------162 Morse code identifier---------------------------------------147 Multi Function Display (MFD) Softkeys----------------------------------------------------- 22 Music 1-------------------------------------------------------171 Music 2-------------------------------------------------------171 N N1 for Thrust Rating Max Speed-------------------------106 N1 gauge--------------------------------------------------- 119, N1 Transient Limit-------------------------------------------106 N2 indications-----------------------------------------------106 I-4 National Weather Service----------------------------------365 NAV1 audio--------------------------------------------------146 NAV2 audio--------------------------------------------------146 Navigation database--------------------277, 278, 277, 278 Navigation Map---------------------------------------------235 Navigation Mode----------------------- 523–524, 533–534 Navigation mode selection--------------------------------145 Navigation (NAV) frequency box-------------------------- 62 Navigation source-------------------------------------- 80–82 Navigation status box--------------------------------------- 62 Nav radio selection-----------------------------------------145 Nearest Airports---------------------------------------- 52, 228–231 VOR------------------------------------------------- 228–229 nearest airport---------------------------------- 212, 213, 214 Nearest Airport-------------------- 212, 213, 214, 215, 291 Minimum Runway Length------------------------------215 Surface Matching----------------------------------------215 Nearest airports, frequency tuning-----------------------129 Nearest Airports Page------------------------- 213, 214, 215 Nearest Pages (NRST)--------------------------------------- 42 NEXRAD------------------------------------------------------- 24 NEXRAD Softkey------------------------------------- 347, 385 Night view-------------------------------------------- 585, 603 NO COMP----------------------------------------------------664 Non-path descent------------------------------514, 537–538 Normal operating mode------------------------------------ 28 O Obstacles---------------------------------------------- 672, 673 Odometer----------------------------------------------------- 56 Oil, engine-------------------------------------------- 104, 106 Omni-bearing selector (OBS)------------------------------- 85 Omni Bearing Selector (OBS)----------------------- 708–709 Other Statistics--------------------------------------- 296, 298 Outside Air Temperature (OAT)---------------------------105 Overspeed protection, autopilot--------------------------504 Overview-------------------------------------------------------- 1 P Page groups--------------------------------------------- 38–41 Parallel Track------------------------------------------ 263, 264 Passenger----------------------------------------------------301 Passenger Address (PA) System---------------------------169 Passengers-------------------------------------------- 300, 301 PFD failure---------------------------------------------------174 Pilot and Stores Weight------------------------------------300 Pilot profiles--------------------------------------------- 44–45 PIREP-------------------------------------------------- 369, 395 Pitch Hold Mode--------------------------------------------505 Pitch indication----------------------------------------------- 67 Power ON settings------------------------------------------167 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A INDEX Power-up page----------------------------------------------652 Predefined message--------------------------- 631, 632, 633 Pressure, oil------------------------------------------- 104, 106 Pressurization-----------------------------------------------109 Primary Flight Display (PFD) Softkeys------------------------------------------------ 15–17 Procedures GFC 700-------------------------------------------- 530–543 Q Quick tuning 121.500 MHz-------------------------------128 R RA-------------------------------------------------------------484 Radar Altimeter------------------------------------------63, 95 RAIM-------------------------------- 288, 303, 304, 305, 306 Range---------------------------------------------------------204 Receiver Autonomous Integrity Monitoring (RAIM)-3 4 – 3 5 , 303, 707 Register-------------------------------------------------------374 Reminder messages----------------------------------------- 56 Required Vertical Speed------------------------------------324 Required Vertical Speed Indicator------------------------324 Resolution Advisory (RA)----------------------------------485 Reversionary mode-----------------------------------------176 Reversionary Mode-----------------------------------------176 Reversionary sensor----------------------------------------664 Reversionary sensor window------------------------------- 90 ROC----------------------------------------429, 443, 682, 684 Roll Hold Mode---------------------------------------------521 RS-232-------------------------------------------------------- 2, 4 RS-485-------------------------------------------------------- 3, 4 Runway Minimum length------------------------------------------- 53 Surface------------------------------------------------------ 53 RVSI---------------------------------------------------- 324, 325 RX indicator--------------------------------------------------127 S SafeTaxi------------------------------------------ 561, 562, 565 SafeTaxi®----------------------------------------------------547 SafeTaxi database-------------------------------------------566 SBAS-------------------------------, 705, 707, 303, 305, 306 Scheduler-------------------------------------56–57, 650, 652 SD card-------------------------------------------------------- 26 Sector scan---------------------------------------------------415 Secure Digital (SD) card----------------------------- 652, 689 Selected altitude-----------------------------------------62, 69 bug---------------------------------------------------------- 62 Selected Altitude------------ 505, 506, 508, 509, 511, 515 Selected Altitude Capture Mode-505, 506, 507, 508, 511 Selected Altitude Intercept Arc----------------------------207 190-00728-06 Rev. A Selected Course-------------------------------------- 523, 526 Selected heading-----------------------------------------63, 76 Selected Heading--------------------------------12, 498, 522 Selecting a COM radio-------------------------------------126 Sensor------------------------------------------------- 664, 665 Sequencing, automatic-------------------------------------709 Service Class-------------------------------------------------646 Servos, AFCS-------------------------------------------------497 SIGMET------------------------------------------------ 356, 389 Simultaneous COM Operation----------------------------169 SiriusXM radio------------------------------------------------- 338, 645 Receiver troubleshooting-------------------------------657 XM Satellite Weather------------------------------------338 SiriusXM active channel-----------------------------------647 SiriusXM channel list---------------------------------------647 SiriusXM lightning------------------------------------------- 24 SiriusXM presets--------------------------------------------648 SiriusXM radio volume-------------------------------------649 SiriusXM Satellite Radio-----------------------------------645 SiriusXM Satellite Weather AIRMETs---------------------------------------------------356 SiriusXM Weather AIRMETs---------------------------------------------------389 SIGMETs---------------------------------------------------389 SiriusXM weather/radio--------------------------------------- 4 Slip/Skid indicator----------------------------------------62, 67 SMS-----------------------------------------------------------547 Softkeys----------------------------------------------15–18, 62 LTNG-------------------------------------------------------354 Speaker-------------------------------------------------------167 STAB----------------------------------------------------------416 Standby frequency----------------------------- 126, 129, 145 ADF---------------------------------------------------------153 Standby frequency field------------------------------------126 Standby Navigation Database--------------- 691, 692, 693 Static air temperature (SAT)----------------------------62, 87 Stuck microphone-------------------------------------------174 Stuck Microphone------------------------------------------174 Sunrise--------------------------------------------------------297 Sunset--------------------------------------------------------297 Surface Analysis---------------------------------------------360 SVS------------------------------------------------------------681 SVT troubleshooting----------------------------------------655 Symbols, map------------------------------------------------713 Synoptics---------------------------------------------- 111–118 Synthetic vision (SVS)------------------------------- 547, 548 System alerting----------------------------------------------- 90 System annunciations--------------------------------- 31, 666 System message advisories--------------------------------669 System Setup Page------------------------------------------ 43 System Status Page------------------------------------------ 53 System time-----------------------------------------------48, 62 Embraer Prodigy® Flight Deck 100 Pilot’s Guide I-5 INDEX T TA-------------------------------------------------------------484 TAF----------------------------------------------------- 357, 390 Takeoff Mode------------------------------------------------519 TAS------------------------------------------------------------676 TAS Traffic Non-Threat Traffic--------------------------- 461, 470, 483 PA--------------------------------------------------- 470, 483 Proximity Advisory-------------------------------- 470, 483 TAWS------- 92, 422, 429, 443, 454, 682, 684, 435, 456 TAWS-A------------------------------------ 436, 400, 683, 92 TAWS-A Alerts Excessive below Glideslope/Glidepath----------------452 Excessive Closure Rate Alert----------------------------446 Excessive Descent Rate Alert---------------------------446 Flap Override Annunciation-----------------------------448 Flight Into Terrain Alert----------------------------------447 Inhibiting FLTA and PDA Alerts-------------------------445 Inhibiting GPWS Alerts----------------------------------451 Negative Climb Rate After Takeoff Alert--------------449 orward Looking Terrain Avoidance--------------------444 Premature Descent Alerting----------------------------445 TAWS-A Page------------------------------------------------440 TAWS-B-------------------------------------------------------422 System Status---------------------------------------------434 TAWS-B Alerts-----------------------------------------------428 Excessive Descent Rate Alert---------------------------430 Five-Hundred Aural Alert--------------------------------432 Forward Looking Terrain Avoidance (FLTA)-----------430 Negative Climb Rate After Takeoff Alert--------------432 Premature Descent Alerting----------------------------431 TAWS-B Page------------------------------------------------426 TCAS II Traffic------------------------------------------------483 Operation--------------------------------------------------488 Resolution advisories------------------------------------485 Symbology-------------------------------------------------483 System Status---------------------------------------------494 System Test------------------------------------------------487 TCAS II Alerts---------------------------------------------484 TCAS I Traffic------------------------------------------------469 Alerts-------------------------------------------------------472 Altitude Display------------------------------------------476 Operation--------------------------------------------------474 sensitivity level-------------------------------------------471 System Status---------------------------------------------481 system test------------------------------------------------473 TA Alerting Conditions----------------------------------471 Theory of operation--------------------------------------469 Surveillance Volume-------------------------------------469 Traffic Map Page-----------------------------------------474 Telephone-------------------------5, 40, 547, 610, 611, 612 I-6 TEMP COMP minimums---------------------------- 289, 291 Temperature, cabin and cockpit--------------------------112 Temperature compensated altitude--------------- 294, 295 Temperature, oil-------------------------------------- 104, 106 Temperature, Outside Air (OAT)---------------------------105 Terminal procedures charts------------------------- 570, 591 Terrain-------------------------------- 23, 429, 443, 672, 682 Color indications-----------------------------------------715 Terrain Awareness and Warning System------------------ 92 Terrain Awareness and Warning System (TAWS)-422, 436 Text message-----------------------------626, 628, 631, 634 Text messaging----------------------------------------------626 Thrust rating-------------------------------------------------107 Thrust Rating------------------------------------------------106 Thrust Rating Max Speed----------------------------------106 Tilt------------------------------------------------------ 412, 413 Tilt Line-------------------------------------------------------413 Timer----------------------------------------------------------680 Departure--------------------------------------------------- 56 Flight-------------------------------------------------------- 55 Timer, PFD generic------------------------------------------- 55 Time, system-------------------------------------------------- 48 TOD---------------------------------------------- 323, 324, 330 Toggling ADF frequencies---------------------------------154 TOPO DATA------------------------------------- 191, 192, 201 Top of Descent--------------------------------------- 323, 324 Topographical data------------------------------------------ 23 TOPO SCALE-------------------------------------------------193 Total air temperature (TAT)-----------------------------62, 87 Track indicator------------------------------------------------ 62 Traffic---------------------------------------------------------- 23 Traffic Advisory (TA)----------------------------------------409 Traffic Alert and Collision Avoidance System-----------469 Traffic annunciation----------------------------------------- 91 Traffic Information Service (TIS)--------------461, 711–712 Transponder-----------------------------------------------18, 19 Transponder code entry------------------------------------164 Transponder data box--------------------------------------121 Transponder ground mode--------------------------------160 Transponder mode field-----------------121, 160, 162, 163 Transponder standby mode------------------------ 159, 162 Transponder status box------------------------------------- 62 Trend vector, airspeed--------------------------------------- 64 Trend vector, altitude---------------------------------------- 69 Trend vector, turn rate--------------------------------------- 77 Trim Indicator-----------------------------------------110, 120, Trip Planning------------------------------------ 296, 297, 298 Trip statistics-------------------------------------------------- 56 Trip Statistics------------------------------------------ 297, 298 True Airspeed------------------------------------------------298 True airspeed (TAS)------------------------------------------ 62 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A INDEX Tuning ADF frequencies------------------------------------154 Turbulence---------------------------------------------------368 Turn anticipation--------------------------------------------709 Turn rate indicator---------------------------------------62, 77 TX indicator--------------------------------------------------127 U Unable to display chart----------------------------- 570, 591 Updating Garmin databases------------------------------566 User-defined hold------------------------------------ 270, 272 Using XM Radio---------------------------------------------647 V VDI----------------------------------------------------- 324, 325 Vertical deviation-------------------------------------- 70, 513 Vertical deviation guidance-------------------------------278 Vertical Deviation Indicator-------------------------------324 Vertical navigation------------------------------------------277 Direct-to---------------------------------------------------276 Vertical Navigation flight control------------------ 511–515 Vertical Path Tracking Mode------------------511–512, 536 Vertical scan------------------------------------------ 412, 413 Vertical speed guidance-----------------------------------278 Vertical Speed Indicator------------------------------------485 Vertical speed indicator (VSI)------------------------------ 72 Vertical Speed Mode---------------------------------------508 VFR code-----------------------------------------------------165 VNAV---------------------------------------------------------237 VNAV Target Altitude-------------------------------- 511–514 VNAV Target Altitude Capture Mode--------------------515 VNV---------------------------------------------- 323, 681, 706 VNV guidance Disabling--------------------------------------------------275 Enabling---------------------------------------------------275 VNV indications, PFD---------------------------------------- 89 Voice alerts, TIS Traffic--------------------------------------465 Voltmeter, battery------------------------------------ 104, 108 Volume-------------------------------------------------------649 VOR Nearest--------------------------------------------- 228–229 VOR selection------------------------------------------------145 VSI-------------------------------------------------------------325 Vspeeds-------------------------------------------------- 65–66 VS TGT------------------------------------------------- 277, 323 Waypoint Selection Submenu----------233, 241, 245, 303 Weather Attenuated Color Highlight--------------------416 Weather Radar Weather Alert --------------------------------------------------------------417 Wi-Fi------------------------------------------------ 4, 638, 642 Wind----------------------------------------------------------203 Wind data----------------------------------------------------- 88 Winds Aloft------------------------------------------- 362, 392 WIND Softkey----------------------------------------- 362, 392 X XM Radio Entertainment----------------------------------171 XPDR softkey-----------------------------159, 162, 164, 165 Z Zoom Auto--------------------------------------------------------183 W WAAS--------------------------------------307, 530, 706, 707 WAAS precision approach---------------------------------541 WATCH------------------------------------------------ 416, 417 Waypoint Automatic sequencing----------------------------------709 Skipping---------------------------------------------------709 Waypoint Pages (WPT)-------------------------------------- 39 190-00728-06 Rev. A Embraer Prodigy® Flight Deck 100 Pilot’s Guide I-7 INDEX Blank Page I-8 Embraer Prodigy® Flight Deck 100 Pilot’s Guide 190-00728-06 Rev. A Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p:913.397.8200 f:913.397.8282 www.garmin.com Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. p:503.391.3411 f:503.364.2138 Garmin (Europe) Ltd. Liberty House, Houndsdown Business Park Southampton, Hampshire SO40 9LR, U.K. p:44 (0) 23 8052 4000 f:44 (0) 23 8052 4004 Garmin Corporation No. 68, Jangshu 2nd Road Shijr, Taipei County, Taiwan p:886/02.2642.9199 f:886/02.2642.9099
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