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G1000 ® Integrated Flight Deck Pilot’s Guide ® G1000 Pilot’s Guide Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p:913.397.8200 f:913.397.8282 Garmin (Europe) Ltd. Liberty House, Bulls Copse Road Houndsdown Business Park Southampton, SO40 9RB, U.K. p:44/0870.8501241 f:44/0870.8501251 Garmin Corporation No. 68, Jangshu 2nd Road Shijr, Taipei County, Taiwan p:886/02.2642.9199 f:886/02.2642.9099 www.garmin.com Diamond DA42NG Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. p:503.391.3411 f:503.364.2138 190-00962-00 Revision B Diamond DA42NG System Software 0670.02 or later Untitled-1 1 11/13/2007 9:15:37 AM SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Copyright © 2009 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 0670.02 or later for the Diamond DA42NG. 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, Bulls Copse Road, Hounsdown Business Park, Southampton, SO40 9RB, U.K Tel: 44/0870.8501241 Fax: 44/0870.8501251 Garmin Corporation, No. 68, Jangshu 2nd Road, Shijr, Taipei County, Taiwan Tel: 886/02.2642.9199 Fax: 886/02.2642.9099 Website 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. Garmin® and G1000® are registered trademarks of Garmin Ltd. or its subsidiaries. FliteCharts®, and SafeTaxi® are trademarks of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin. Honeywell® is a registered trademark of Honeywell International, Inc. Stormscope® is a registered trademark of L-3 Communications. Avidyne® is a registered trademark of Avidyne Corporation. XM® is a registered trademark of XM Satellite Radio, Inc. Printed in the U.S.A April 2009 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG Limited Warranty LIMITED WARRANTY This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this period, Garmin will, at its sole option, repair or replace any components that fail in normal use. Such repairs or replacement will be made at no charge to the customer for parts and labor, provided that the customer shall be responsible for any transportation cost. This warranty does not cover failures due to abuse, misuse, accident, or unauthorized alterations or repairs. THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES EXPRESS OR IMPLIED OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO STATE. IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER RESULTING FROM THE USE, MISUSE, OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT. Some states do not allow the exclusion of incidental or consequential damages, so the above limitations may not apply to you. Garmin retains the exclusive right to repair or replace the unit or software, or to offer a full refund of the purchase price, at its sole discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY. To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in locating a Service Center near you, visit the Garmin Website at “http://www.garmin.com” or contact Garmin Customer Service at 800-800-1020. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG i 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 G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters, such as the Air Data Computer, or other altimeters in aircraft. GPS altitude should never be used for vertical navigation. Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft. WARNING: Do not use outdated database information. Databases used in the G1000 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 the G1000 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: Use of the Stormscope is not intended for hazardous weather penetration (thunderstorm penetration). Stormscope information, as displayed on the G1000, is to be used only for weather avoidance, not penetration. WARNING: XM Weather should not be used for hazardous weather penetration. Weather information provided by the GDL 69A is approved only for weather avoidance, not penetration. Warning: NEXRAD weather data is to be used for long-range planning purposes only. Due to inherent delays in data transmission and the relative age of the data, NEXRAD weather data should not be used for short-range weather avoidance. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG iii Warnings, Cautions, and Notes WARNING: The Garmin G1000, as installed in this 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 G1000. 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, G1000 operational procedures must be learned on the ground. 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 Garmin G1000 utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the G1000 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 G1000 Pilot’s Guide documentation and the Airplane Flight Manual. Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications from the G1000 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 G1000 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 anomalies in the earth’s magnetic field, operating the G1000 within the following areas could result in loss of reliable attitude and heading indications. North of 70° North latitude and south of 70° South latitude. An area north of 65° North latitude between longitude 75º West and 120º West. An area south of 55° South latitude between longitude 120º East and 165º East. 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. iv Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Warnings, Cautions, and Notes CAUTION: The Garmin G1000 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. NOTE: When using Stormscope, there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the strike display mode. However, clusters of two or more discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after the screen has been cleared. NOTE: All visual depictions contained within this document, including screen images of the G1000 panel and displays, are subject to change and may not reflect the most current G1000 system. 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: 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 feet 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: 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. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG v Revision Information Record of Revision Part Number 190-00962-00 190-00962-00 vi Revision A B Date 02/19/09 04/29/09 Page Range Description i - I-6 Initial release i - I-6 Added Synthetic Vision System Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Table of Contents 1.1 1.2 1.3 1.4 1.5 1.6 1.7 Section 1 System overview Line Replaceable Units............................................ 2 Secure Digital (SD) Cards........................................ 7 System Power-up...................................................... 8 System Operation..................................................... 9 Display Operation. ........................................................ 9 G1000 System Annunciations....................................... 10 System Status............................................................. 11 AHRS Operation.......................................................... 13 GPS Receiver Operation............................................... 14 G1000 Controls....................................................... 18 PFD/MFD Controls....................................................... 18 Softkey Function. ........................................................ 20 Accessing G1000 Functionality............................ 27 Menus. ...................................................................... 27 Data Entry.................................................................. 27 Page Groups............................................................... 29 System Settings. ......................................................... 33 Timers........................................................................ 38 Electronic Checklists.................................................... 41 Display Backlighting.............................................. 43 Section 2 Flight Instruments 2.1 Flight Instruments.................................................. 48 Airspeed Indicator....................................................... 48 Attitude Indicator........................................................ 50 Altimeter.................................................................... 51 Vertical Speed Indicator (VSI). ...................................... 53 Vertical Deviation........................................................ 54 Horizontal Situation Indicator (HSI)............................... 55 Course Deviation Indicator (CDI)................................... 60 2.2 Supplemental Flight Data..................................... 67 Outside Air Temperature. ............................................. 67 Wind Data.................................................................. 69 Vertical Navigation (VNV) Indications. .......................... 70 2.3 PFD Annunciations and Alerting Functions......... 71 System Alerting........................................................... 71 Marker Beacon Annunciations...................................... 72 Traffic Annunciation. ................................................... 72 Altitude Alerting. ........................................................ 73 Low Altitude Annunciation........................................... 73 Minimum Descent Altitude/Decision Height Alerting....... 74 190-00962-00 Rev. B 2.4 Abnormal Operations............................................ 75 Abnormal GPS Conditions............................................ 75 Unusual Attitudes. ...................................................... 76 Section 3 Engine Indication System (EIS) 3.1 Engine Display........................................................ 80 3.2 System Display....................................................... 82 3.3 Fuel Display............................................................. 84 4.1 4.2 4.3 4.4 4.5 Section 4 Audio Panel and CNS Overview................................................................. 87 MFD/PFD Controls and Frequency Display...................... 88 Audio Panel Controls................................................... 90 COM Operation....................................................... 92 COM Transceiver Selection and Activation. .................... 92 COM Transceiver Manual Tuning................................... 93 Quick-tuning and Activating 121.500 MHz. ................... 94 Auto-tuning the COM Frequency. ................................. 95 Frequency Spacing. ..................................................... 99 Automatic Squelch.................................................... 100 Volume. ................................................................... 100 NAV Operation...................................................... 101 NAV Radio Selection and Activation............................ 101 NAV Receiver Manual Tuning. .................................... 102 Auto-tuning a NAV Frequency from the MFD. .............. 104 Marker Beacon Receiver. ........................................... 109 ADF/DME Tuning....................................................... 110 GTX 33 Mode S Transponder............................... 114 Transponder Controls. ............................................... 114 Transponder Mode Selection. ..................................... 115 Entering a Transponder Code...................................... 118 IDENT Function......................................................... 119 Flight ID Reporting.................................................... 120 Additional Audio Panel Functions...................... 121 Power-up.................................................................. 121 Mono/Stereo Headsets. ............................................. 121 Speaker.................................................................... 121 Intercom. ................................................................. 122 Passenger Address (PA) System. ................................. 124 Clearance Recorder and Player................................... 124 Split COM................................................................. 125 Entertainment Inputs................................................. 125 Garmin G1000 Pilot’s Guide for the Diamond DA42NG vii Table of Contents 4.6 Audio Panel Preflight Procedure........................ 126 4.7 Abnormal Operation............................................ 127 Stuck Microphone..................................................... 127 COM Tuning Failure................................................... 127 Audio Panel Fail-safe Operation.................................. 127 Reversionary Mode. .................................................. 127 5.1 5.2 5.3 5.4 5.5 5.6 viii Section 5 Flight Management Introduction.......................................................... 129 Navigation Status Box............................................... 131 Using Map Displays.............................................. 132 Map Orientation. ...................................................... 132 Map Range............................................................... 134 Map Panning............................................................ 136 Measuring Bearing and Distance. ............................... 141 Topography. ............................................................. 142 Map Symbols............................................................ 145 Airways.................................................................... 151 Track Vector.............................................................. 153 Wind Vector.............................................................. 154 Nav Range Ring........................................................ 155 Fuel Range Ring........................................................ 156 Field of View (SVS). ................................................... 157 Waypoints.............................................................. 158 Airports.................................................................... 159 Intersections............................................................. 165 NDBs. ...................................................................... 167 VORs........................................................................ 169 User Waypoints......................................................... 171 Airspaces............................................................... 176 Direct-to-Navigation . ......................................... 180 Flight Planning...................................................... 185 Flight Plan Creation................................................... 186 Adding Waypoints to an Existing Flight Plan................ 189 Adding Airways to a Flight Plan.................................. 191 Adding Procedures to a Stored Flight Plan................... 194 Flight Plan Storage.................................................... 201 Flight Plan Editing..................................................... 203 Along Track Offsets. .................................................. 206 Parallel Track. ........................................................... 208 Activating a Flight Plan Leg........................................ 211 Inverting a Flight Plan. .............................................. 212 Flight Plan Views....................................................... 213 Closest Point of FPL................................................... 215 5.7 Vertical Navigation.............................................. 216 Altitude Constraints. ................................................. 218 5.8 Procedures............................................................ 222 Departures. .............................................................. 222 Arrivals . .................................................................. 225 Approaches . ............................................................ 227 5.9 Trip Planning......................................................... 233 Trip Planning. ........................................................... 233 5.10 RAIM Prediction................................................... 237 5.11 Navigating a Flight Plan...................................... 241 5.12 Abnormal Operation............................................ 269 6.1 6.2 6.3 6.4 6.5 6.6 Section 6 Hazard Avoidance XM Satellite Weather........................................... 271 Activating Services.................................................... 272 Using XM Satellite Weather Products.......................... 273 WX-500 Stormscope............................................ 296 Setting Up Stormscope on the Navigation Map............ 296 Selecting the Stormscope Page................................... 300 Terrain Proximity.................................................. 301 Displaying Terrain Proximity Data. .............................. 302 Terrain Proximity Page............................................... 304 TERRAIN-SVS......................................................... 306 TERRAIN-SVS Page.................................................... 310 TERRAIN-SVS Alerts................................................... 312 System Status........................................................... 315 Traffic Information Service (TIS)......................... 316 Displaying TRAFFIC Data............................................ 317 Traffic Map Page....................................................... 320 TIS Alerts.................................................................. 321 System Status........................................................... 322 AVIDYNE TAS600 (Optional)................................ 325 TAS Symbology......................................................... 325 Displaying Traffic Data............................................... 326 Altitude Display. ....................................................... 328 Traffic Map Page Display Range.................................. 328 TAS Alerts................................................................. 330 System Status........................................................... 331 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Table of Contents Section 7 Automatic Flight Control System 7.1 AFCS Controls....................................................... 334 7.2 Flight Director Operation.................................... 336 Activating the Flight Director...................................... 336 AFCS Status Box. ...................................................... 337 Command Bars......................................................... 338 Flight Director Modes................................................ 338 7.3 Vertical Modes...................................................... 339 Pitch Hold Mode (PIT)................................................ 340 Selected Altitude Capture Mode (ALTS). ...................... 341 Altitude Hold Mode (ALT)........................................... 342 Vertical Speed Mode (VS)........................................... 343 Flight Level Change Mode (FLC). ................................ 344 Vertical Navigation Modes (VPTH, ALTV). .................... 345 Glidepath Mode (GP) (WAAS only). ............................ 350 Glideslope Mode (GS)................................................ 352 Go Around Mode (GA)............................................... 353 7.4 Lateral Modes....................................................... 354 Roll Hold Mode (ROL)................................................ 355 Heading Select Mode (HDG)....................................... 356 Navigation Modes (GPS, VOR, LOC, BC)....................... 357 Approach Modes (GPS, VAPP, LOC).............................. 359 7.5 Autopilot and Yaw Damper Operation.............. 361 Flight Control. .......................................................... 361 Engaging the Autopilot and Yaw Damper. ................... 362 Control Wheel Steering.............................................. 362 Disengaging the Autopilot and Yaw Damper................ 363 7.6 Example Flight Plan............................................. 364 Departure................................................................. 364 Intercepting a VOR Radial.......................................... 366 Flying a Flight Plan/GPS Course.................................. 367 Descent.................................................................... 368 Approach. ................................................................ 371 Go Around/Missed Approach...................................... 374 7.7 AFCS Annunciations and Alerts.......................... 376 AFCS Status Alerts..................................................... 376 Overspeed Protection. ............................................... 378 Section 8 Additional Features 8.1 Synthetic Vision System (SVS) (Optional).......... 380 SVS Operation. ......................................................... 381 SVS Features............................................................. 383 190-00962-00 Rev. B Field of View............................................................. 391 8.2 SafeTaxi................................................................. 393 SafeTaxi Cycle Number and Revision........................... 396 8.3 ChartView.............................................................. 399 ChartView Softkeys. .................................................. 399 Terminal Procedures Charts........................................ 400 Chart Options........................................................... 408 Day/Night View......................................................... 414 ChartView Cycle Number and Expiration Date. ............ 416 8.4 FliteCharts............................................................. 420 FliteCharts Softkeys................................................... 420 Terminal Procedures Charts........................................ 421 Chart Options........................................................... 428 Day/Night View......................................................... 432 FliteCharts Cycle Number and Expiration Date............. 434 8.5 XM Radio Entertainment (Optional).................. 438 Activating XM Satellite Radio Services. ....................... 438 Using XM Radio........................................................ 440 8.6 Scheduler............................................................... 443 8.7 Electronic Checklists............................................ 445 8.8 Abnormal Operation............................................ 448 SVS Troubleshooting.................................................. 448 Reversionary Mode. .................................................. 448 Unusual Attitudes. .................................................... 449 GDL 69/69A Data Link Receiver Troubleshooting.......... 450 Appendices Annunciations and Alerts.............................................. 453 SVS Terrain Alerts...................................................... 470 SVS Terrain Status Annunciations................................ 470 SD Card Use and Databases.......................................... 471 Glossary........................................................................... 475 Frequently Asked Questions......................................... 481 General TIS Information................................................ 485 Introduction.............................................................. 485 TIS VS. TAS/TCAS....................................................... 485 TIS Limitations.......................................................... 485 Map Symbols.................................................................. 487 Index Index . ...............................................................................I-1 Garmin G1000 Pilot’s Guide for the Diamond DA42NG ix Table of Contents Blank Page x Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview SYSTEM OVERVIEW Section 1 System overview FLIGHT INSTRUMENTS NOTE: Refer to the Automatic Flight Control System (AFCS) Section for details on the GFC 700 AFCS. The G1000 Integrated Flight Deck System presents flight instrumentation, position, navigation, communication, and identification information using flat-panel color displays. The system is distributed across the following Line Replaceable Units (LRUs): • GDU 1040 Primary Flight Display (PFD) EIS • GDU 1045 Multi Function Display (MFD) • GRS 77 Attitude and Heading Reference System (AHRS) • GMU 44 Magnetometer • GDL 69/69A Data Link Receiver • GIA 63W Integrated Avionics Units (IAU) • GSA 80 AFCS Yaw Damper Servo • GDC 74A Air Data Computer (ADC) • GSA 81 AFCS Servos (3) • GEA 71 Engine/Airframe Unit • GSM 85 Servo Mounts (4) AUDIO PANEL & CNS • GMA 1347 Audio Panel with Integrated Marker Beacon Receiver FLIGHT MANAGEMENT • GTX 33 Mode S Transponder Figure 1-1 shows interactions between the LRUs. Additional/optional equipment are shown in Figure 1-2. The Diamond DA42NG may be optionally equipped with a GFC 700 Automated Flight Control System (AFCS), providing flight director (FD), autopilot (AP), and manual electric trim (MET) functions of the G1000 System. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 1 SYSTEM OVERVIEW System Overview 1.1 Line Replaceable Units FLIGHT INSTRUMENTS • GDU 1040/1045 (2) – A GDU 1040 is configured as the Primary Flight Display (PFD) and a GDU 1045 as the Multi Function Display (MFD). Both displays feature 10.4-inch LCD screens with 1024 x 768 resolution. The displays communicate with each other through a High-speed Data Bus (HSDB) Ethernet connection. Each display is also paired with an Ethernet connection to an IAU. GDU 1045 AUDIO PANEL & CNS EIS GDU 1040 HAZARD AVOIDANCE FLIGHT MANAGEMENT • GMA 1347 – The Audio Panel integrates navigation/communication radio (NAV/COM) digital audio, intercom, and marker beacon controls, and is installed between the displays. This unit also provides manual control of display Reversionary Mode (red DISPLAY BACKUP button; see Section 1.4, System Operation) and communicates with both IAUs using an RS-232 digital interface. ADDITIONAL FEATURES AFCS • GIA 63W (2) – The Integrated Avionics Units (IAU) function as the main communications hub, linking all LRUs with the PFD. Each GIA 63W contains a GPS WAAS receiver, VHF COM/NAV/GS receivers, a flight director (FD; if GFC 700 is installed), and system integration microprocessors. Each GIA 63W is paired with the on-side display via an HSDB connection. The IAUs are not paired together and do not communicate with each other directly. INDEX APPENDICES NOTE: Refer to the Aircraft Flight Manual (AFM) to determine whether WAAS functionality is approved. 2 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview SYSTEM OVERVIEW GDC 74A – The Air Data Computer (ADC) processes data from the pitot/static system and outside air temperature (OAT) sensor. The ADC provides pressure altitude, airspeed, vertical speed, and OAT information to the G1000 System, and it communicates with the primary IAU, displays, and AHRS using an ARINC 429 digital interface. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS • GEA 71 – The Engine Airframe Unit receives and processes signals from the engine and airframe sensors. This unit communicates with both IAUs using an RS-485 digital interface. FLIGHT MANAGEMENT HAZARD AVOIDANCE • GTX 33 – The solid-state Transponder provides Modes A, C, and S capability and communicates with both IAUs through an RS-232 digital interface. AFCS ADDITIONAL FEATURES • GRS 77 (2) – The Attitude and Heading Reference System (AHRS) provides aircraft attitude and heading information via ARINC 429 to both the PFD and the primary IAU. The AHRS contains advanced sensors (including accelerometers and rate sensors) and interfaces with the Magnetometer to obtain magnetic field information, with the ADC to obtain air data, and with both IAUs to obtain GPS information. AHRS operation is discussed in Section 1.4, System Operation. APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 3 SYSTEM OVERVIEW System Overview FLIGHT INSTRUMENTS • GMU 44 – The Magnetometer measures local magnetic field and sends data to the AHRS for processing to determine aircraft magnetic heading. This unit receives power directly from the AHRS and communicates with it via an RS-485 digital interface. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS • GDL 69/69A – The Data Link Satellite Radio Receiver provides real-time weather information to MFD maps and the PFD Inset Map. The GDL 69A model is also capable of providing digital audio entertainment. The Data Link Receiver communicates with the MFD via an HSDB connection. A subscription to XM Satellite Radio Service is required to enable Data Link Receiver capability. • GSA 80, GSA 81 and GSM 85 – The GSA servos are used for the automatic control of pitch, pitch trim, roll and yaw. These units interface with each IAU. INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE The GSM 85 servo mounts are responsible for transferring the output torque of the servo actuators to the mechanical flight-control surface linkages (not displayed in Figure 1-1). 4 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview GDU 1045 GMA 1347 Multi Function Display Audio Panel FLIGHT INSTRUMENTS Reversionary Control SYSTEM OVERVIEW GDU 1040 Primary Flight Display Reversionary Control EIS GDC 74A Air Data Computer Integrated Avionics Unit No. 2 GIA 63W Integrated Avionics Unit OAT Airspeed Altitude Vertical Speed System Integration Processors I/O Processors VHF COM VHF NAV/LOC GPS/WAAS Glideslope GRS 77 FLIGHT MANAGEMENT System Inegration Processors I/O Processors VHF COM VHF NAV/LOC GPS/WAAS Glideslope Flight Director (with AFCS option) AUDIO PANEL & CNS No. 1 GIA 63W AHRS GPS Output GPS Output Attitude Rate of Turn Slip/Skid GMU 44 HAZARD AVOIDANCE Magnetometer Heading GTX 33 Transponder AFCS GEA 71 Engine/Airframe Unit Autopilot Calculations (optional) GSA 81 Pitch Trim Servo Autopilot Calculations (optional) GSA 81 Roll Servo Autopilot Calculations (optional) ADDITIONAL FEATURES GSA 81 Pitch Servo GSA 80 Yaw Damper Servo Yaw Damper Calculations (optional) Figure 1-1 G1000 System Block Diagram APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 5 EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW System Overview No. 2 GIA 63W AUDIO PANEL & CNS Integrated Avionics Unit FLIGHT MANAGEMENT System Integration Processors I/O Processors VHF COM VHF NAV/LOC GPS/WAAS Glideslope Becker RA 3502-(1) HAZARD AVOIDANCE ADF Receiver (optional) Honeywell KN 63 DME (optional) L3 Stormscope Lightning Strike and Thunderstorm Detection (optional) GDL 69/69A Data Link Receiver Real-time Weather Digital Audio Entertainment (optional subscriptionbased service) Avidyne TAS600 Series Honeywell KAP 140 Traffic Advisory System (optional) Autopilot (optional) Figure 1-2 G1000 With Optional/Additional Interfaces AFCS NOTE: The GDU 1040 is available in systems using the Honeywell KAP 140 Autopilot. NOTE: For information on additional equipment shown in Figure 1-2, consult the applicable optional interface INDEX APPENDICES ADDITIONAL FEATURES user’s guide. This document assumes that the reader is already familiar with the operation of this additional equipment. 6 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview SYSTEM OVERVIEW 1.2 Secure Digital (SD) Cards FLIGHT INSTRUMENTS NOTE: Ensure the G1000 System is powered off before inserting an SD card. NOTE: Refer to the Appendix for instructions on updating databases. EIS The PFD and MFD data card slots use Secure Digital (SD) cards and are located on the upper right side of the display bezels. Each display bezel is equipped with two SD card slots. SD cards are used for aviation database and system software updates as well as terrain database storage. Installing an SD card: AUDIO PANEL & CNS 1) 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. 2) To eject the card, gently press on the SD card to release the spring latch. FLIGHT MANAGEMENT HAZARD AVOIDANCE SD Card Slots AFCS ADDITIONAL FEATURES Figure 1-3 Display Bezel SD Card Slots APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 7 SYSTEM OVERVIEW System Overview 1.3 System Power-up FLIGHT INSTRUMENTS NOTE: See the Aircraft Flight Manual (AFM) for specific procedures concerning avionics power application and emergency power supply operation. NOTE: Refer to the Appendix for system-specific annunciations and alerts. EIS The G1000 System is integrated with the aircraft electrical system and receives power directly from electrical busses. The PFD, 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. AUDIO PANEL & CNS During system initialization, test annunciations are displayed, as shown in Figure 1-4. All system annunciations should disappear typically within the first minute of power-up. Upon power-up, key annunciator lights also become momentarily illuminated on the Audio Panel and the display bezels. FLIGHT MANAGEMENT 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 the first minute of power-up. The AHRS can align itself both while taxiing and during level flight. HAZARD AVOIDANCE When the MFD powers up, the screen (Figure 1-5) displays the following information: • System version • Obstacle database name and version • Copyright • Terrain database name and version • Land database name and version • Aviation database name, version, and effective dates Current database information includes 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. INDEX APPENDICES ADDITIONAL FEATURES AFCS Pressing the ENT Key acknowledges this information, and displays the Navigation Map Page. When the system has acquired a sufficient number of satellites to determine a position, the aircraft’s current position is shown on the Navigation Map Page. Figure 1-4 PFD Initialization 8 Figure 1-5 Example MFD Power-up Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview SYSTEM OVERVIEW 1.4 System Operation FLIGHT INSTRUMENTS NOTE: Refer to the Appendix for detailed descriptions of all alerts and annunciations. Refer to the Aircraft Flight Manual (AFM) for additional information regarding pilot responses to these annunciations. The displays are connected together via a single Ethernet bus for high-speed communication. As shown in Figure 1-1, each IAU is connected to the on-side display. This allows the units to share information, enabling true system integration EIS Display Operation NOTE: In normal operating mode, backlighting can only be adjusted from the PFD. In Reversionary Mode, it AUDIO PANEL & CNS can be adjusted from the remaining display. FLIGHT MANAGEMENT In normal operating mode, the PFD presents graphical flight instrumentation (attitude, heading, airspeed, altitude, vertical speed), replacing the traditional flight instrument cluster (see the Flight Instruments Section for more information). The MFD normally displays a full-color moving map with navigation information (see the Flight Management Section), while the left portion of the MFD is dedicated to the Engine Indication System (EIS; see the EIS Section). Both displays offer control for COM and NAV frequency selection. HAZARD AVOIDANCE AFCS Figure 1-6 G1000 Normal Operation ADDITIONAL FEATURES APPENDICES In the event of a display failure, the G1000 System automatically switches to reversionary (backup) mode. In Reversionary Mode, all important flight information from the PFD is presented on the remaining display in the same format as in normal operating mode, with the addition of the EIS. EIS operation while in Reversionary Mode is discussed in the EIS Section. As when the PFD is operating normally, windows for flight planning, nearest airports, and procedures are available. The Inset Map is moved to the right side of the display. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX If a display fails, the appropriate IAU-display Ethernet interface is cut off. Thus, the IAU can no longer communicate with the remaining display (refer to Figure 1-1), and the NAV and COM functions provided to the failed display by the IAU are flagged as invalid on the remaining display. The system reverts to backup paths for the AHRS, ADC, Engine/Airframe Unit, and Transponder, as required. The change to backup paths is completely automated for all LRUs and no pilot action is required. 9 SYSTEM OVERVIEW System Overview If the system fails to detect a display problem, Reversionary Mode may be manually activated by pressing the Audio Panel’s red DISPLAY BACKUP Button. Pressing this button again deactivates Reversionary Mode. AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS NAV1 and COM1 (provided by the failed PFD) Flagged Invalid DISPLAY BACKUP Button Manually Activates/ Deactivates Reversionary Mode on Both Displays FLIGHT MANAGEMENT Figure 1-7 G1000 Reversionary Mode (Failed PFD) G1000 System Annunciations HAZARD AVOIDANCE When an LRU or an LRU function fails, a large red ‘X’ is typically displayed over the instrument experiencing failed data (Figure 1-8 displays all possible flags and responsible LRUs). The G1000 System alerts the pilot when backup paths are utilized by the LRUs. Upon G1000 power-up, certain instruments remain invalid as equipment begins to initialize. All instruments should be operational within one minute of power-up. If any instrument remains flagged, the G1000 should be serviced by a Garmin-authorized repair facility. GIA 63W AFCS GRS 77, GMU 44 or GIA 63W ADDITIONAL FEATURES GDC 74A Database Mismatch in PFD and MFD APPENDICES GEA 71, GIA 63W, or ECU GIA 63W or DME/ADF Source INDEX GIA 63W GDC 74A GIA 63W GTX 33 or GIA 63W Figure 1-8 G1000 System Failure Annunciations 10 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview SYSTEM OVERVIEW System Status FLIGHT INSTRUMENTS The System Status Page displays the statuses, serial numbers, and software version numbers for all detected system LRUs. Active LRUs are indicated by green check marks; failed, by red ‘X’s. Failed LRUs should be noted and a service center or Garmin-authorized dealer informed. Viewing LRU information: 1) Use the FMS Knob to select the AUX - System Status Page. 2) To place the cursor in the ‘LRU Info’ Box, EIS a) Press the LRU Softkey. Or: a) Press the MENU Key. AUDIO PANEL & CNS b) With ‘Select LRU Window’ highlighted, press the ENT Key. 3) Use the FMS Knob to scroll through the box to view LRU status information. FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 1-9 Example System Status Page INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 11 SYSTEM OVERVIEW System Overview Airframe information which includes system software, Cockpit Reference Guide (CRG) part number, system ID, and checklist are also displayed on this page. FLIGHT INSTRUMENTS Viewing airframe information: 1) Use the FMS Knob to select the AUX - System Status Page. 2) To place the cursor in the ‘Airframe’ Box, a) Press the ARFRM Softkey. Or: EIS a) Press the MENU Key. b) Highlight ‘Select Airframe Window’ and press the ENT Key. AUDIO PANEL & CNS 3) Use the FMS Knob to scroll through the box to view airframe information. Pertinent information on all system databases is also displayed on this page. Refer to the Appendices and Additional Features sections for more information about databases. Viewing database information: FLIGHT MANAGEMENT 1) Use the FMS Knob to select the AUX - System Status Page. 2) To place the cursor in the ‘Database’ Box, a) Press the DBASE Softkey. HAZARD AVOIDANCE Or: a) Press the MENU Key. b) Highlight ‘Select Dbase Window’ and press the ENT Key. 3) Use the FMS Knob to scroll through the box to view database status information. AFCS The G1000 uses aural tones to convey the priority of airframe-specific alerts. The alerting system’s annunciation tone may be tested from the System Status Page. Refer to the Appendices for airframe-specific alerts. Testing the system annunciation tone: ADDITIONAL FEATURES 1) Use the FMS Knob to select the AUX - System Status Page. 2) Press the ANN TEST Softkey. Or: a) Press the MENU Key. INDEX APPENDICES b) Highlight ‘Enable Annunciator Test Mode’ and press the ENT Key. 12 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview SYSTEM OVERVIEW AHRS Operation NOTE: Aggressive maneuvering while AHRS is not operating normally may degrade AHRS accuracy. FLIGHT INSTRUMENTS The Attitude and Heading Reference System (AHRS) performs attitude, heading, and vertical acceleration calculations for the G1000 System, utilizing GPS, magnetometer, and air data in addition to information from its internal sensors. Attitude and heading information are updated on the PFD while the AHRS receives appropriate combinations of information from the external sensor inputs. unavailable available available unavailable FLIGHT MANAGEMENT le ab AHRS no-GPS Mode ail av AHRS no- AHRS no-Mag/ Mag Mode no-Air Mode Heading Invalid Air Data un available unavailable available unavailable available Air Data AHRS Normal Operation Magnetometer Data AUDIO PANEL & CNS Magnetometer Data EIS GPS Data Attitude/Heading Invalid HAZARD AVOIDANCE AFCS Figure 1-10 AHRS Operation ADDITIONAL FEATURES Loss of GPS, magnetometer, or air data inputs is communicated to the pilot by message advisory alerts (refer to Appendix A for specific AHRS alert information). Any failure of the internal AHRS inertial sensors results in loss of attitude and heading information (indicated by red ‘X’ flags over the corresponding flight instruments). APPENDICES Two GPS inputs are provided to the AHRS. If GPS information from one of the inputs fails, the AHRS uses the remaining GPS input and an alert message is issued to inform the pilot. If both GPS inputs fail, the AHRS can continue to provide attitude and heading information to the PFD as long as magnetometer and airspeed data are available and valid. If the magnetometer input fails, the AHRS continues to output valid attitude information; however, the heading output on the PFD is flagged as invalid with a red ‘X’. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX Failure of the air data input has no effect on the AHRS output while AHRS is receiving valid GPS information. Invalid/unavailable airspeed data in addition to GPS failure results in loss of all attitude and heading information. 13 SYSTEM OVERVIEW System Overview GPS Receiver Operation FLIGHT INSTRUMENTS Each Integrated Avionics Unit (IAU) contains a GPS receiver. Internal system checking is performed to ensure both GPS receivers are providing accurate data to the PFD. When both GPS receivers are providing accurate data, the GPS receiver producing the better solution is used by the system. Information collected by the specified receiver (GPS1 for the #1 IAU or GPS2 for the #2 IAU) may be viewed on the AUX - GPS Status Page. Viewing GPS receiver status information: EIS 1) Use the large FMS Knob on the MFD to select the Auxiliary Page Group (see Section 1.6 for information on navigating MFD page groups). 2) Use the small FMS Knob to select GPS Status Page (third page in the AUX Page Group). AUDIO PANEL & CNS Press the desired GPS Softkey. FLIGHT MANAGEMENT 3) To change the selected GPS receiver: b) Use the FMS Knob to highlight the receiver which is not selected and press the ENT Key. Or: a) Press the MENU Key. Satellite Signal Information GPS Receiver Status AFCS HAZARD AVOIDANCE Satellite Constellation Diagram ADDITIONAL FEATURES RAIM Availability Prediction INDEX APPENDICES Satellite Signal Strength Bars Figure 1-11 GPS Status Page 14 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview SYSTEM OVERVIEW NOTE: Refer to the Aircraft Flight Manual (AFM) to determine whether WAAS functionality is approved. FLIGHT INSTRUMENTS For WAAS-enabled systems, 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 a WAAS signal. While the aircraft is on the ground, the WAAS 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 WAAS signal. If no failure message exists, check the GPS Status Page and compare the information for GPS1 and GPS2. Discrepancies may indicate a problem. EIS GPS receiver status AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 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. Satellite-Based Augmentation System (SBAS) status should be indicated as INACTIVE at this point. When acquisition is complete, the solution status changes to 3D DIFF NAV and SBAS becomes active. In certain situations, such as when the aircraft is outside or on the fringe of the WAAS or MSAS (used only in Japan) coverage area, it may be desirable to disable WAAS or MSAS (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 and MSAS enabling/disabling. HAZARD AVOIDANCE Disabling WAAS or MSAS 1) Select the GPS Status Page. AFCS 2) If necessary, press the SBAS Softkey. 3) Press the FMS Knob, and turn the large FMS Knob to hightlight ‘MSAS’ or ‘WAAS’. 4) Press the ENT Key to uncheck the box. ADDITIONAL FEATURES 5) Press the FMS Knob to remove the cursor. APPENDICES INDEX Figure 1-12 Enable/Disable WAAS 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 15 SYSTEM OVERVIEW System Overview RAIM Prediction FLIGHT INSTRUMENTS 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. EIS 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. In G1000 systems with WAAS enabled, performing RAIM prediction is not necessary in most cases. However, if the selected approach is outside the WAAS coverage area, it may be necessary to perform a RAIM prediction for the intended approach. AUDIO PANEL & CNS NOTE: Refer to the Aircraft Flight Manual (AFM) to determine whether WAAS functionality is approved. FLIGHT MANAGEMENT Because of the tighter protection limit on approaches, there may be times when RAIM is not available. The G1000 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 message “Approach is not active”. 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. HAZARD AVOIDANCE 2) Press the RAIM Softkey. 2) Press the FMS Knob. The ‘WAYPOINT’ field is highlighted. 3) Turn the small FMS Knob to display the Waypoint Information Window. 4) Enter the desired waypoint and press the ENT Key (refer to Section 1.6 for instructions on data entry). AFCS Or: a) To use the present position, press the MENU Key. b) With ‘Set WPT to Present Position’ highlighted, press the ENT Key. ADDITIONAL FEATURES c) Press the ENT Key to accept the waypoint entry. 5) Enter an arrival time and press the ENT Key. 6) Enter an arrival date and press the ENT Key. INDEX APPENDICES 7) With the cursor highlighting ‘COMPUTE RAIM?’, press the ENT Key. Once RAIM availability is computed, one of the following is displayed: 16 • ‘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 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview SYSTEM OVERVIEW Satellite Information FLIGHT INSTRUMENTS Satellites currently in view are shown at their respective positions on a satellite constellation diagram. This sky view is always oriented north-up, 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. EIS 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 indicated by signal bar appearance: • No signal strength bar—Receiver is looking for the indicated satellite. AUDIO PANEL & CNS • Hollow signal strength bar—Receiver has found the satellite and is collecting data. Each satellite has a 30second data transmission that must be collected (signal strength bar is hollow) before the satellite may be used for navigation (signal strength bar becomes solid). • Solid signal strength bar—Receiver has collected the necessary data and the satellite signal can be used. FLIGHT MANAGEMENT • Checkered signal strength bar—Receiver has excluded the satellite (Fault Detection and Exclusion; FDE). • “D” indication on signal strength bar—Satellite is being used for differential computations. • Green signal strength bar—Satellites that are actually being used in the position calculation. • Blue signal strength bar—Satellite is locked on but not yet being used in the position calculation. HAZARD AVOIDANCE Using the current satellite signal information, the system calculates the aircraft’s GPS position, time, altitude, ground speed, and track for the aircraft (displayed below the satellite signal accuracy measurements for reference). The following quantities denote the accuracy of the aircraft’s GPS fix: • Estimated Position Uncertainty (EPU)—A statistical error indication; the radius of a circle centered on an estimated horizontal position in which actual position has 95% probability of lying AFCS • Horizontal Dilution of Precision (HDOP)—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 ADDITIONAL FEATURES • Horizontal and Vertical Figures of Merit (HFOM and VFOM)—Measures of horizontal and vertical position uncertainty; the current 95% confidence horizontal and vertical accuracy values reported by the GPS receiver NOTE: Refer to the Aircraft Flight Manual (AFM) to determine whether WAAS functionality is approved. APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 17 SYSTEM OVERVIEW System Overview 1.5 G1000 Controls FLIGHT INSTRUMENTS The G1000 controls have been designed to simplify operation of the system and minimize workload and the time required to access sophisticated functionality. Controls are located on the PFD and MFD bezels and Audio Panel. PFD and MFD controls and softkeys are discussed in this section. See the Audio Panel and CNS Section for more information about Audio Panel and NAV/COM controls. AFCS controls (on the bezel of the MFD) are described in the AFCS section. EIS PFD/MFD Controls 2 3 4 5 6 7 8 9 HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS 1 10 13 11 14 12 15 AFCS 16 18 17 ADDITIONAL FEATURES Figure 1-13 PFD/MFD Controls The NAV, CRS/BARO, COM, FMS, and ALT knobs are concentric dual knobs, each having small (inner) and large (outer) control portion. When a portion of the knob is not specified in the text, either may be used. APPENDICES Large (Outer) Knob Small (Inner) Knob INDEX Figure 1-14 Dual Concentric Knob 18 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview NAV VOL/ID Knob Turn to control NAV audio volume (shown in the NAV Frequency Box as a percentage) NAV Frequency Transfer Key 3 NAV Knob Heading Knob Press to toggle light blue tuning box between NAV1 and NAV2 Turn to manually select a heading Joystick Press to display a digital heading momentarily to the left of the Horizontal Situation Indicator (HSI) and synchronize the Selected Heading to the and current heading Turn to change map range CRS/BARO Knob Press to activate Map Pointer and move in desired direction to pan map Turn large knob for altimeter barometric pressure setting AUDIO PANEL & CNS 6 Turn to tune NAV receiver standby frequencies (large knob for MHz; small for kHz) EIS 5 Press to toggle Morse code identifier audio on/off Transfers the standby and active NAV frequencies FLIGHT INSTRUMENTS 2 4 SYSTEM OVERVIEW 1 Turn small knob to adjust course (only when HSI is in VOR or OBS Mode) COM Knob FLIGHT MANAGEMENT 7 Press to re-center the CDI and return course pointer directly to bearing of active waypoint/station Turn to tune COM transceiver standby frequencies (large knob for MHz; small for kHz) Press to toggle light blue tuning box between COM1 and COM2 COM Frequency Transfer Key (EMERG) HAZARD AVOIDANCE 8 The selected COM (green) is controlled with the COM MIC Key (Audio Panel). Transfers the standby and active COM frequencies 11 FPL Key 12 CLR Key (DFLT MAP) MENU Key 14 PROC Key 15 ENT Key 190-00962-00 Rev. B Press and hold to display the MFD Navigation Map Page (MFD only). Displays a context-sensitive list of options for accessing additional features or making setting changes Gives access to IFR departure procedures (DPs), arrival procedures (STARs), and approach procedures (IAPs) for a flight plan or selected airport Validates/confirms selection or data entry Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX 13 Erases information, cancels entries, or removes menus APPENDICES Direct-to Key ( Press to turn the COM automatic squelch on/off ) Activates the direct-to function and allows the user to enter a destination waypoint and establish a direct course to the selected destination (specified by identifier, chosen from the active route) Displays flight plan information ADDITIONAL FEATURES 10 AFCS Press and hold two seconds to tune the emergency frequency (121.5 MHz) automatically into the active frequency field 9 COM VOL/SQ Knob Turn to control COM audio volume level (shown as a percentage in the COM Frequency Box) 19 SYSTEM OVERVIEW System Overview FLIGHT INSTRUMENTS 16 Press to turn the selection cursor on/off FMS Knob (Flight Management Data Entry: With cursor on, turn to enter data in the highlighted field (large System Knob) knob moves cursor location; small knob selects character for highlighted cursor location) EIS Scrolling: When a list of information is too long for the window/box, a scroll bar appears, indicating more items to view. With cursor on, turn large knob to scroll through the list. 17 AUDIO PANEL & CNS Softkey Selection Keys 18 ALT Knob Page Selection: Turn knob on MFD to select the page to view (large knob selects a page group; small knob selects a specific page from the group) Press to select softkey shown above the bezel key on the PFD/MFD display Sets the Selected Altitude, shown above the Altimeter (the large knob selects the thousands, the small knob selects the hundreds) Softkey Function FLIGHT MANAGEMENT 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. When a softkey function is disabled, the softkey label is subdued (dimmed). HAZARD AVOIDANCE Softkeys revert to the previous level after 45 seconds of inactivity. AFCS Bezel-Mounted Softkeys (Press) Softkey On Softkey Names (Displayed) Figure 1-15 Softkeys (Second-Level PFD Configuration) ADDITIONAL FEATURES In the following descriptions, top level softkeys are denoted with bullets. PFD Softkeys APPENDICES The CDI, IDENT, TMR/REF, NRST, and ALERTS softkeys undergo a momentary change to black text on gray background and automatically switch back to white text on black background when selected. INDEX 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 selected to return to the previous level. The ALERTS Softkey is visible at all softkey levels (label changes if messages are issued). 20 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview PFD OBS CDI (optional) ADF/DME XPDR IDENT TMR/REF NRST SYSTEM OVERVIEW INSET ALERTS FLIGHT INSTRUMENTS Press the CDI Softkey to cycle through navigation sources: - GPS - NAV1 (VOR/LOC) - NAV2 (VOR/LOC) Figure 1-16 Top Level PFD Softkeys EIS Displays Inset Map in PFD lower left corner Removes Inset Map Selects desired amount of map detail; cycles through declutter levels: DCLTR (No Declutter): All map features visible INSET DCLTR-1: Removes land data (optional) INSET PFD OBS ADF/DME DCLTR-2: Removes landCDI and SUA data XPDR IDENT TMR/REF NRST ALERTS DCLTR-3: Removes everything except active flight plan Inset (optional) Map TRAFFIC (2) Displays/removes traffic information on Press the CDI Softkey to cycle through (optional) (optional) navigation sources: TRFC-1: Displays Inset Map. STRMSCP NEXRAD XM LTNG TRAFFIC traffic ALERTS OFF DCLTR TOPOon TERRAIN BACK - GPS TRFC-2: Removes everything except traffic. Inset- Map HDG UP only. NAV1position (VOR/LOC) - NAV2 (VOR/LOC) Displays/removes topographical data (e.g., coastlines, terrain, on Softkey Inset Map TOPO Pressrivers, the OFFlakes) or BACK DCLTR-1 TRFC-1 to return to the top-level softkeys. Displays/removes terrain information on Inset Map TERRAIN DCLTR-2 TRFC-2 Displays/removes Stormscope weather information on Inset Map (optional) STRMSCP DCLTR-3 Displays/removes NEXRAD weather and coverage information on Inset Map (optional) NEXRAD Displays/removes XM lightning information on Inset Map (optional) XM LTNG • INSET OFF DCLTR (3) AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS INSET ADDITIONAL FEATURES (optional) (optional) (optional) OFF TRAFFIC DCLTR-1 TRFC-1 DCLTR-2 TRFC-2 TOPO TERRAIN STRMSCP NEXRAD XM LTNG BACK ALERTS Press the OFF or BACK Softkey to return to the top-level softkeys. APPENDICES DCLTR DCLTR-3 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX Figure 1-17 INSET Softkeys 21 SYSTEM OVERVIEW System Overview Displays second-level softkeys for additional PFD configuration Displays the softkeys for enabling or disabling Synthetic Vision features (optional) Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan SYN TERR Enables synthetic terrain depiction HRZN HDG Displays compass heading along the Zero-Pitch line APTSIGNS 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 DFLTS Displays softkeys to select and configure wind data WIND Displays wind data in longitudinal and lateral components OPTN1 Displays wind data total direction and speed OPTN2 Displays wind data total direction with head and cross-wind speed components OPTN3 Removes wind information from display OFF Displays/removes DME Information Window (optional) DME Cycles the Bearing 1 Information Window through: BRG1 NAV1: Waypoint frequency/identifier and DME information GPS: Waypoint identifier and GPS distance information ADF: Waypoint frequency Off: Removes window Displays softkeys to select the HSI format HSI FMT Displays HSI as a 360° compass rose 360 HSI Displays HSI as a 140° viewable arc (Bearing Information windows unavailable) ARC HSI Cycles the Bearing 2 Information Window through: BRG2 NAV2: Waypoint frequency/identifier and DME information GPS: Waypoint identifier and GPS distance information ADF: Waypoint frequency Off: Removes window Displays softkeys for changing the Altimeter barometric setting and altitude displays to ALT UNIT metric units Displays the current and Selected altitudes in meters in addition to feet, when selected METERS Displays the Altimeter barometric setting in inches of mercury (in Hg) IN Displays the Altimeter barometric setting in hectopascals (hPa) HPA Sets barometric pressure to 29.92 in Hg (1013 hPa if metric display is selected) STD BARO Selects OBS Mode on the CDI when navigating by GPS (only available with active leg) • OBS Cycles CDI through GPS, NAV1 (VOR/LOC), and NAV2 (VOR/LOC) navigation sources • CDI • ADF/DME Displays/removes ADF/DME Radio Tuning Window (optional; may appear as ADF, DME, or ADF/DME depending on installation) INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS • PFD SYN VIS PATHWAY 22 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview SYSTEM OVERVIEW PFD SYN VIS FLIGHT INSTRUMENTS (optional) (optional) DFLTS WIND DME BRG1 HSI FMT ALT UNIT STD BARO BRG2 BACK ALERTS OPTN2 OPTN3 OFF 360 HSI IN HPA PATHWAY SYN TERR HRZN HDG APTSIGNS ALERTS BACK ALERTS BACK ALERTS BACK ALERTS FLIGHT MANAGEMENT METERS ARC HSI BACK AUDIO PANEL & CNS OPTN1 EIS Press the BRG1/BRG2 Press the STD BARO or BACK softkeys to display/remove Softkey to return to the top-level the Bearing Information softkeys. windows and cycle through bearing sources: - NAV1/NAV2 - GPS - ADF HAZARD AVOIDANCE Figure 1-18 PFD Configuration Softkeys AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 23 System Overview (optional) WIND SYSTEM OVERVIEW DFLTS FLIGHT INSTRUMENTS • XPDR STBY ON ALT GND AUDIO PANEL & CNS EIS VFR CODE 0—7 BKSP • IDENT FLIGHT MANAGEMENT • TMR/REF • NRST • ALERTS BRG1 DME ALT UNIT STD BARO BRG2 HSI FMT BACK ALERTS Displays transponder mode selection softkeys: Pressdoes the BRG1/BRG2 Press the STD BARO or BACK Selects standby mode (Transponder not reply to any interrogations) softkeys to display/remove Softkey to return to the top-level Selects Mode A (Transponder replies to interrogations) the Bearing Information softkeys. windows and cycle through Selects Mode C – altitude reporting mode (Transponder replies to identification and altitude bearing sources: interrogations) - NAV1/NAV2 - GPS Manually selects Ground Mode (Transponder does not allow Mode A and Mode C - ADF replies, but does permit acquisition squitter and replies to discretely addressed Mode S interrogations) BACK ALERTS OFF OPTN1 OPTN2 OPTN3 Automatically enters the VFR code (1200 in U.S.A. only) Displays transponder code selection softkeys 0-7 360 HSI ARC HSI BACK ALERTS Use numbers to enter code Removes numbers entered, one at a time METERS HPA BACK ALERTS Activates the Special Position Identification IN (SPI) pulse for 18 seconds, identifying the transponder return on the ATC screen Displays/removes Timer/References Window Displays/removes Nearest Airports Window Displays/removes Alerts Window HAZARD AVOIDANCE XPDR ON ALT GND VFR CODE AFCS STBY IDENT BACK ALERTS ADDITIONAL FEATURES Press the BACK Softkey to return to the top-level softkeys. 0 1 2 3 4 5 6 7 IDENT BKSP BACK ALERTS APPENDICES Press the IDENT or BACK Softkey to return to the toplevel softkeys. INDEX Figure 1-19 XPDR Softkeys 24 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview SYSTEM OVERVIEW MFD Softkeys MFD softkeys vary depending on the page selected. EIS and Navigation Map Page (default MFD page) softkeys are described here. DCLTR FLIGHT INSTRUMENTS MAP ENGINE SHW CHRT CHKLIST DCLTR-1 DCLTR-2 EIS DCLTR-3 SYSTEM FUEL ENGINE SYSTEM FUEL BACK DEC FUEL INC FUEL RST FUEL AUDIO PANEL & CNS ENGINE BACK FLIGHT MANAGEMENT Press the BACK Softkey to return to the top-level softkeys. TRAFFIC TOPO (optional) (optional) (optional) TERRAIN AIRWAYS STRMSCP NEXRAD XM LTNG BACK HAZARD AVOIDANCE Press the BACK softkey to return to the top-level softkeys. AIRWY ON AIRWY LO AIRWY HI DONE EXIT EMERGCY AFCS ENGINE The DONE Softkey label changes to UNDO when the checklist item is already checked. ADDITIONAL FEATURES Figure 1-20 EIS and MFD Softkeys • ENGINE Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX 190-00962-00 Rev. B APPENDICES SYSTEM FUEL DEC FUEL INC FUEL RST FUEL Displays the Engine Page and top-level engine softkeys (see the EIS Section for more information) Displays the System Page Displays the Fuel Page Decreases displayed fuel remaining in 1-gal increments Increases displayed fuel remaining in 1-gal increments Resets displayed fuel remaining to maximum fuel capacity for aircraft and fuel used to zero 25 SYSTEM OVERVIEW System Overview Enables second-level Navigation Map Page softkeys Displays/removes traffic information on Navigation Map Page Displays/removes topographical data (e.g., coastlines, terrain, rivers, lakes) on Navigation Map Page Displays/removes terrain information on Navigation Map Page TERRAIN Selects the desired display of Airways; cycles through: AIRWAYS AIRWY ON: All Airways displayed AIRWY LO: Low Altitude (Victor) Airways displayed AIRWY HI: High Altitude Airways (Jet Routes) displayed AIRWAYS: Airways are not displayed STRMSCP Displays/removes Stormscope weather information on Inset Map (optional) Displays/removes NEXRAD weather/coverage on Navigation Map Page (optional) NEXRAD XM LTNG Displays/removes XM lightning information on Navigation Map Page (optional) Returns to top-level softkeys BACK • DCLTR (3) Selects desired amount of map detail; cycles through declutter levels: DCLTR (No Declutter): All map features visible DCLTR-1: Removes land data DCLTR-2: Removes land and SUA data DCLTR-3: Removes everything except the active flight plan • SHW CHRT Displays optional Flite Charts or Chart View charts (optional) Displays the Checklist Page • CHKLIST Selects the highlighted checklist item DONE Returns to the top-level softkeys EXIT EMERGCY Immediately accesses the emergency procedures INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS • MAP TRAFFIC TOPO 26 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview SYSTEM OVERVIEW 1.6 Accessing G1000 Functionality Menus FLIGHT INSTRUMENTS The G1000 has a dedicated MENU Key that when pressed displays a context-sensitive list of options. This options list allows the user to access additional features or make setting 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 additional features or settings for the window/page selected. EIS Navigating a menu: 1) Press the MENU Key to display the menu. AUDIO PANEL & CNS 2) Turn the FMS Knob to scroll through a list of available options (a scroll bar always appears to the right of the window/box when the option list is longer than the window/box). 3) Press the ENT Key to select the desired option. 4) Press the CLR Key or FMS Knob to remove the menu and cancel the operation. Options for FPL Window FLIGHT MANAGEMENT No Options for NRST Window HAZARD AVOIDANCE Figure 1-21 Page Menu Examples AFCS Data Entry ADDITIONAL FEATURES The FMS Knob can be used for directly entering alphanumeric data (e.g., Flight ID, waypoint identifiers, barometric minimum descent altitude) into the G1000 In some instances, such as when entering an identifier, the G1000 tries to predict the desired identifier based on the characters being entered. In this case, if the desired identifier appears, use the ENT Key to confirm the entry without entering the rest of the identifier manually. This can save the pilot from having to enter all the characters of the identifier. APPENDICES Besides character-by-character data entry, the system also provides a shortcut for entering waypoint identifiers. When the cursor is on a field awaiting entry of a waypoint identifier, turning the small FMS Knob counterclockwise accesses three different lists of waypoint identifiers for quick selection: flight plan (FPL), nearest (NRST), and recently-entered (RECENT). The G1000 automatically fills in the identifier, facility, and city fields with the information for the selected waypoint. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 27 SYSTEM OVERVIEW System Overview Using the FMS Knob to enter data: 1) If needed, press the FMS Knob to activate the cursor. FLIGHT INSTRUMENTS 2) Use the large FMS Knob to highlight the desired field. 3) Begin entering data. a) To quickly enter a waypoint identifier, turn the small FMS Knob counter-clockwise to display a list of waypoints in the active flight plan (list is titled FPL). If desired, turn the small FMS Knob clockwise to scroll through lists of nearest waypoints (NRST) and recently-entered waypoints (RECENT). EIS b) Turn the large FMS Knob to highlight the desired waypoint from the list and press the ENT Key. Or: a) Turn the small FMS Knob to select a character for the first placeholder. AUDIO PANEL & CNS Turning the knob clockwise scrolls through the alphabet (where appropriate) toward the letter Z, starting at K, and the digits zero through nine. Afterwards, turning the knob counter-clockwise scrolls in the opposite direction. b) Use the large FMS Knob to move the cursor to the next placeholder in the field. FLIGHT MANAGEMENT c) Repeat, using the small FMS Knob to select a character and the large FMS Knob to move the cursor, until the field is complete. d) Press the ENT Key to confirm entry. INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE 7) Press the FMS Knob or CLR Key to cancel data entry (the field reverts back to its previous information). 28 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview SYSTEM OVERVIEW Page Groups Note: Refer to other supporting sections in this Pilot’s Guide for details on specific pages. Active Page Title EIS Page Group MFD FLIGHT INSTRUMENTS 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, the current page group, number of pages available in the group, and placement of the current page within the group are indicated by icons. For some of these pages (Airport/Procedures/Weather Information, XM, Procedure Loading), the title of the page changes while the page icon remains the same. AUDIO PANEL & CNS FLIGHT MANAGEMENT Page Groups Pages in Current Group HAZARD AVOIDANCE Selected Page Figure 1-22 Page Title and Page Group Icons There are four main page groups, navigated using the FMS Knob; specific pages within each group can vary depending on the configuration of optional equipment. AFCS Selecting a page using the FMS Knob: 1) Turn the large FMS Knob until the desired page group is selected. ADDITIONAL FEATURES 2) Turn the small FMS Knob until the desired page is selected. APPENDICES 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. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 29 SYSTEM OVERVIEW System Overview • Map Page Group (MAP) Navigation Map FLIGHT INSTRUMENTS Traffic Map Stormscope (optional) Weather Data Link (optional) AUDIO PANEL & CNS EIS Terrain Proximity FLIGHT MANAGEMENT Figure 1-23 Map Pages • Waypoint Page Group (WPT) HAZARD AVOIDANCE - Airport Information (INFO Softkey) AFCS Airport/Procedures/Weather Information Pages: - Arrival Information (STAR Softkey) - Departure Information (DP Softkey) ADDITIONAL FEATURES - Approach Information (APR Softkey) - Weather Information (optional) (WX Softkey) Intersection Information Airport, Procedures and Weather Information Pages APPENDICES NDB Information VOR Information Figure 1-24 Waypoint Pages INDEX User Waypoint Information 30 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview SYSTEM OVERVIEW • Auxiliary Page Group (AUX) Trip Planning Utility FLIGHT INSTRUMENTS GPS Status System Setup XM Satellite Pages (optional): - XM Radio (RADIO Softkey) EIS - XM Information (INFO Softkey) XM Pages AUDIO PANEL & CNS System Status FLIGHT MANAGEMENT Figure 1-25 Auxiliary Pages • Nearest Page Group (NRST) HAZARD AVOIDANCE Nearest Airports Nearest Intersections Nearest NDB Nearest VOR AFCS Nearest User Waypoints Nearest Frequencies ADDITIONAL FEATURES Nearest Airspaces APPENDICES Figure 1-26 Nearest Pages INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 31 SYSTEM OVERVIEW System Overview In addition to the main page groups accessed exclusively using the FMS Knob, there are pages for flight planning (FPL) and loading procedures (PROC) which are accessed by key. In some instances, softkeys may be used to access the Procedure Loading pages. FLIGHT INSTRUMENTS The Flight Plan pages are accessed using the FPL Key on the MFD. Main pages within this group are selected by turning the small FMS Knob. • Flight Plan Page Group (FPL) Active Flight Plan Flight Plan Catalog FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS - Stored Flight Plan (NEW Softkey) Figure 1-27 Flight Plan Pages HAZARD AVOIDANCE The Procedure Loading pages may be accessed at any time on the MFD by pressing the PROC Key. A menu is initialized, and when a departure, approach, or arrival is selected, the appropriate Procedure Loading page is opened. These pages can also be accessed from the Active and Stored Flight Plan pages using the LD softkeys. Turning the FMS Knob does not scroll through the Procedure Loading pages (note the single page icon in the lower right corner). • Procedure Loading Page Group (PROC) AFCS Departure Loading Arrival Loading APPENDICES ADDITIONAL FEATURES Approach Loading Figure 1-28 Procedure Loading Pages INDEX Information on optional electronic checklist pages is offered later in this section. Checklist pages may be accessed from any page on the MFD using the CHKLIST Softkey. 32 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview SYSTEM OVERVIEW System Settings G1000 system settings are managed from the System Setup Page. The following settings can be changed: • Date/time • Display Units (see Flight Instruments Section) • Baro Transition Alert (see Flight Instruments Section) • Airspace alerts (see Flight Management Section) • Audio Alerts • CDI scaling for GPS navigation source (see Flight Instruments Section) • COM channel spacing (see Audio Panel and CNS Section) • Criteria for displaying nearest airports (see Flight Management Section) EIS • Arrival alerts (see Flight Management Section) FLIGHT INSTRUMENTS • MFD Data Bar Fields (see Flight Management Section) AUDIO PANEL & CNS Restoring system setup defaults: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the DFLTS Softkey. FLIGHT MANAGEMENT Or: a) Press the MENU Key. b) Highlight ‘Restore Defaults’ and press the ENT Key. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 1-29 AUX - System Setup Page INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 33 SYSTEM OVERVIEW System Overview Date/Time FLIGHT INSTRUMENTS The G1000 obtains the current Universal Coordinated Time (UTC) date and time directly from the GPS satellite signals (shown on the AUX - GPS Status Page, Figure 1-11). System time (displayed in the lower right corner of the PFD) can be displayed in three formats: local 12-hr, local 24-hr, or UTC. Local time is set by adding/subtracting an offset (hours:minutes) to/from UTC. AUDIO PANEL & CNS EIS PFD FLIGHT MANAGEMENT Figure 1-30 System Time (Local 24-hr Format) Configuring the system time: HAZARD AVOIDANCE 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 the ‘Time Format’ field. 4) Turn the small FMS Knob to select the desired format and press the ENT Key to confirm selection. The ‘Time Offset’ field is highlighted. APPENDICES ADDITIONAL FEATURES AFCS 5) Use the FMS Knob to enter the desired time offset (±HH:MM) and press the ENT Key to confirm selection. INDEX Figure 1-31 Date/Time Settings (AUX - System Setup Page) 34 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview SYSTEM OVERVIEW Display Units Units in which various quantities are displayed on the G1000 screens are listed on the System Setup Page. The Navigation Angle reference can be set from here (refer to the Flight Instruments Section). FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS Figure 1-32 Display Unit Settings (AUX - System Setup Page) Altimeter Vertical Speed Indicator VNV altitudes (Active Flight Plan) Engine Indication System (EIS) APPENDICES Engine Indication System (EIS) N/A N/A INDEX Pounds N/A Kilograms HDDD°MM.MM’ All positions HDDD°MM’SS.S” ADDITIONAL FEATURES Position All temperatures on PFD Total Air Temperature (Trip Planning Page) Fuel parameters (Trip Planning Page) Airspeed Indicator True Airspeed (PFD) Wind speed vector Map range (Traffic Page, Terrain Proximity/TAWS Page) CDI scaling (System Setup) Fuel range calculation (EIS) AFCS Fuel and Fuel Flow Weight Celsius Fahrenheit Gallons HAZARD AVOIDANCE Temperature Exceptions FLIGHT MANAGEMENT Category Settings Affected Quantities Navigation Angle Magnetic (North) Heading True (North) Course Bearing Track Desired Track Wind direction (Trip Planning Page) Distance and Metric Crosstrack error (HSI) Speed Nautical Bearing distances (information windows) DME distance (information window) Flight plan distances Map ranges DIS, GS, TAS, XTK fields (Navigation Status Box) All distances on MFD Altitude buffer distance (System Setup) Arrival Alert trigger distance (System Setup) All speeds on MFD Altitude and Feet All altitudes on MFD Vertical Speed Meters All elevations on MFD Table 1-1 Display Units Settings (AUX - System Setup Page) 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 35 SYSTEM OVERVIEW System Overview Pilot Profiles HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 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 1-5). The G1000 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. Figure 1-33 Pilot Profile Settings (AUX - System Setup Page) Creating a profile: AFCS 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. ADDITIONAL FEATURES 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. APPENDICES 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. INDEX 7) Press the ENT Key. 36 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 9) To cancel the process, select ‘CANCEL’ with the large FMS Knob and press the ENT Key. 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. EIS 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 G1000 loads and displays the system settings for the selected profile. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 3) Turn the large FMS Knob to highlight ‘RENAME’ in the Pilot Profile Box. 4) Press the ENT Key. 5) In the ‘Rename Profile’ window, turn the FMS Knob to select the profile to rename. HAZARD AVOIDANCE 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. AFCS Deleting 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. ADDITIONAL FEATURES 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. APPENDICES 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. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 37 SYSTEM OVERVIEW System Overview Timers The G1000 timers available include: FLIGHT INSTRUMENTS • Stopwatch-like generic timers (available from the PFD Timer/References Window and on the MFD AUX Utility Page) • Total-time-in-flight timer (MFD AUX - Utility Page) • Time since departure (MFD AUX - Utility Page) EIS 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. AUDIO PANEL & CNS Setting the generic timer (PFD): 1) Press the TMR/REF Softkey. 2) Turn the large FMS Knob to select the timer field (hh/mm/ss). FLIGHT MANAGEMENT 3) Use the FMS Knob to enter the desired time and press the ENT Key. 4) With the UP/DN field highlighted, turn the small FMS Knob to select the timer counting direction. 5) Press the ENT Key. 6) With ‘START?’ highlighted, press the ENT Key to start the timer. The field changes to ‘STOP?’. HAZARD AVOIDANCE 7) To stop the timer, press the ENT Key with ‘STOP?’ highlighted. The field changes to ‘RESET?’. 8) To reset the timer, press the ENT Key with ‘RESET?’ highlighted. The field changes back to ‘START?’ and the digits are reset. 9) To remove the window, press the CLR Key or the TMR/REF Softkey. APPENDICES ADDITIONAL FEATURES AFCS PFD INDEX Figure 1-34 Generic Timer (Timer/References Window) 38 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview SYSTEM OVERVIEW 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 generic timer (MFD AUX - Utility Page): FLIGHT INSTRUMENTS 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 specific starting time is desired: EIS 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. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS Figure 1-35 Timers (AUX - Utility Page) ADDITIONAL FEATURES 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. APPENDICES 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. Resetting the flight timer: 1) Use the FMS Knob to select the AUX - Utility Page. INDEX 2) Press the MENU Key. 3) With ‘Reset Flight Timer’ highlighted, press the ENT Key. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 39 SYSTEM OVERVIEW System Overview FLIGHT INSTRUMENTS The G1000 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. 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. EIS 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: AUDIO PANEL & CNS 1) Use the FMS Knob to select the AUX - Utility Page. 2) Press the MENU Key. INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT 3) Use the FMS Knob to highlight ‘Reset Departure Time’ and press the ENT Key. 40 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview SYSTEM OVERVIEW Electronic Checklists NOTE: The checklists presented in this section are for example only and may not reflect checklists actually FLIGHT INSTRUMENTS available for the Diamond DA42NG. The information described in this section is not intended to replace the checklist information described in the AFM or the Pilot Safety and Warning Supplements document. 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. EIS NOTE: Checklists cannot be edited from within the system. Refer to the Garmin Aviation Checklist Editor (ACE) User’s Guide for information on creating and editing checklists. AUDIO PANEL & CNS FLIGHT MANAGEMENT The MFD is able to display optional electronic checklists which allow a pilot to quickly find the proper procedure on the ground and during each phase of flight. The G1000 accesses the checklists from an SD card inserted into the bezel slot (see Figure 1-3). If the SD card contains an invalid checklist file or no checklist, the Power-up Screen displays ‘Invalid Checklist File’ or ‘Checklist File Not Present’ and the CHKLIST Softkey is not available. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX Figure 1-36 Checklist Page Example 41 SYSTEM OVERVIEW System Overview Accessing and navigating checklists: 1) From any page, press the CHKLIST Softkey. FLIGHT INSTRUMENTS 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 FMS Knob to select the desired checklist and press the ENT Key. EIS 6) Turn the FMS Knob to scroll through the checklist and highlight the desired checklist item (has a hollow white box for checkmark). AUDIO PANEL & CNS The following colors are used for checklist items: • Blue - Items has not been highlighted • Green - Item has been selected • White - Item is highlighted for selection • Yellow - Warning notes 7) Press the ENT Key or DONE Softkey to select the highlighted checklist item (item turns green and a checkmark is placed in the box next to the item). The next item is automatically highlighted for selection. FLIGHT MANAGEMENT Press the CLR Key to remove a check mark from an item. 8) Once the last item in a checklist is selected, ‘Go to the next checklist?’ is highlighted. Press the ENT Key to advance to the next checklist displayed. HAZARD AVOIDANCE Immediately accessing emergency procedures: 9) Press the EXIT Softkey or hold down the CLR Key momentarily to exit the Checklist Page and return to the page last viewed. 1) From any page, press the CHKLIST Softkey. INDEX APPENDICES ADDITIONAL FEATURES AFCS 2) Press the EMERGCY Softkey. Figure 1-37 Sample Checklist 42 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B System Overview SYSTEM OVERVIEW 1.7 Display Backlighting FLIGHT INSTRUMENTS The backlighting of the PFD and MFD displays and bezel and Audio Panel keys can be adjusted automatically or manually. The default setting (automatic backlighting adjustment) uses photocell technology to automatically adjust for ambient lighting conditions. Photocell calibration curves are pre-configured to optimize display appearance through a broad range of cockpit lighting conditions. Manual backlighting adjustment can be accomplished using the existing instrument panel dimmer bus or the following procedures. In normal operating mode, backlighting can only be adjusted from the PFD. In Reversionary Mode, it can be adjusted from the remaining display. Adjusting display backlighting: EIS 1) Press the PFD MENU Key to display the PFD Setup Menu. ‘AUTO’ is now highlighted next to ‘PFD DSPL’. 2) Turn the small FMS Knob to select ‘MANUAL’. AUDIO PANEL & CNS 3) Press the ENT Key. The intensity value is now highlighted. 4) Use the FMS Knob to enter the desired backlighting then press the ENT Key. 5) Turn the large FMS Knob to highlight ‘AUTO’ next to ‘MFD DSPL’ and repeat steps 2-4. FLIGHT MANAGEMENT 6) To remove the menu, press the CLR or MENU Key. Adjusting key backlighting: 1) Press the PFD MENU Key to display the PFD Setup Menu. ‘AUTO’ is now highlighted next to ‘PFD DSPL’. 2) Turn the large FMS Knob to highlight ‘PFD DSPL’. HAZARD AVOIDANCE 3) Turn the small FMS Knob in the direction of the green arrowhead to display ‘PFD KEY’. 4) Turn the large FMS Knob to highlight ‘AUTO’. 5) Turn the small FMS Knob to select ‘MANUAL’. 6) Press the ENT Key. The intensity value is now highlighted. AFCS 7) Use the FMS Knob to enter the desired backlighting and press the ENT Key. 8) Turn the large FMS Knob to highlight ‘MFD DSPL’. 9) Turn the small FMS Knob in the direction of the green arrowhead to display ‘MFD KEY’ and repeat steps 4-7. ADDITIONAL FEATURES 10) To remove the menu, press the CLR or MENU Key. PFD APPENDICES INDEX Figure 1-38 PFD Setup Menu 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 43 INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW System Overview Blank Page 44 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Instruments SYSTEM OVERVIEW Section 2 Flight Instruments FLIGHT INSTRUMENTS WARNING: If the airspeed, attitude, altitude, or heading indications become unusable, refer to the backup instruments. Increased situational awareness is provided by replacing the traditional instruments on the panel with an easyto-scan Primary Flight Display (PFD) that features a large horizon, 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 PFD and explained in other sections of this Pilot’s Guide. EIS The following flight instruments and supplemental flight data are displayed on the PFD: • Airspeed Indicator, showing • Horizontal Situation Indicator, showing – True airspeed – Bearing pointers and information windows – Airspeed awareness ranges – Navigation source – Vspeed reference flags – Course Deviation Indicator (CDI) • Attitude Indicator with slip/skid indication – Bearing pointers and information windows • Altimeter, showing – DME Information Window • Transponder Mode, Code, and Ident/Reply – Barometric setting • Course Deviation Indicator (CDI) – Selected altitude • Timer/References Window, showing • Vertical Deviation, Glideslope, and Glidepath Indicators – Generic timer • Vertical Speed Indicator (VSI) – Barometric minimum descent altitude (MDA) – Vspeed values AFCS • Vertical Navigation (VNV) indications HAZARD AVOIDANCE – Trend vector FLIGHT MANAGEMENT – Turn Rate Indicator AUDIO PANEL & CNS – Indicated airspeed • Wind data • Outside air temperature (OAT) ADDITIONAL FEATURES The PFD also displays various alerts and annunciations. APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 45 SYSTEM OVERVIEW Flight Instruments FLIGHT INSTRUMENTS 21 20 19 1 18 17 16 2 EIS 15 FLIGHT MANAGEMENT AUDIO PANEL & CNS 14 3 13 4 12 5 11 6 10 7 9 APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE 8 1 NAV Frequency Box 12 Current Track Indicator 2 Airspeed Indicator 13 Barometric Altimeter Setting 3 True Airspeed 14 Vertical Speed Indicator (VSI) 4 Current Heading 15 Reference Altitude Bug 5 Turn Rate Indicator 16 Altimeter 6 Horizontal Situation Indicator ( HSI) 17 Selected Altitude 7 Outside Air Temperature (OAT) 18 COM Frequency Box 8 Softkeys 19 Navigation Status Box 9 System Time 20 Slip/Skid Indicator 10 Transponder Data Box 21 Attitude Indicator 11 Heading Bug INDEX Figure 2-1 Primary Flight Display (Default) 46 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Instruments SYSTEM OVERVIEW 14 FLIGHT INSTRUMENTS 13 1 12 2 EIS 11 10 AUDIO PANEL & CNS 9 3 4 8 6 FLIGHT MANAGEMENT 5 7 Flight Plan Window 2 Selected Heading 9 Annunciation Window 3 Wind Data 10 Selected Course 4 Inset Map 11 Required Vertical Speed Indicator 5 DME Information Window 12 Vertical Deviation Indicator 6 Bearing Information Windows 13 VNV Target Altitude 7 Barometric Minimum Descent Altitude / Decision Height 14 AFCS Status Annunciation ADDITIONAL FEATURES 8 AFCS Traffic Annunciation HAZARD AVOIDANCE 1 Figure 2-2 Additional PFD Information APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 47 SYSTEM OVERVIEW Flight Instruments 2.1 Flight Instruments FLIGHT INSTRUMENTS Airspeed Indicator Note: Refer to the Aircraft Flight Manual (AFM) for airspeed criteria and Vspeed values. AUDIO PANEL & CNS EIS The Airspeed Indicator displays airspeed on a moving tape rolling number gauge. The true airspeed is displayed in knots below the Airspeed Indicator. The numeric labels and major tick marks on the moving tape are marked at intervals of 10 knots. The minor tick marks on the moving tape are marked at intervals of five knots. Speed indication starts at 20 knots, with 50 knots of airspeed viewable at any time. The indicated airspeed is displayed inside the black pointer. The pointer remains black until reaching never-exceed speed (VNE), at which point it turns red. FLIGHT MANAGEMENT VYSE Vspeed References Indicated Airspeed VMCA Airspeed Trend Vector HAZARD AVOIDANCE Speed Ranges True Airspeed AFCS Airspeed Indicator Operating Ranges Low Speed Range Red and White Barber Pole at VNE Figure 2-3 Airspeed Indicator Ranges ADDITIONAL FEATURES Color coded stripes appear on the Airspeed Indicator to show the operating ranges. The low speed range stripe is red. Normal operating range is green, caution range is yellow, and the never exceed speed (VNE) begins with a red and white barber pole. The flap operating range is indicated by a white stripe. INDEX APPENDICES 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 shows approximately what the indicated airspeed value will be in six seconds. 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. 48 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Instruments SYSTEM OVERVIEW NOTE: Refer to the Aircraft Flight Manual Supplement (AFMS) for Vspeed values. FLIGHT INSTRUMENTS Vspeeds (Glide, VR, VX, VY,, VLE, and VLO) can be changed and their flags turned on/off from the Timer/ References Window. When active (on), the Vspeeds are displayed to the right of the airspeed scale. All Vspeed values are reset and all flags turned off during power up. Changing Vspeeds and turning Vspeed flags on/off: 1) Press the TMR/REF Softkey. 2) Turn the large FMS Knob to highlight the field of the desired Vspeed to be changed. EIS 3) Use the FMS Knob to enter the desired value. When a speed has been changed from a default value, an asterisk appears next to the speed. AUDIO PANEL & CNS 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 the TMR/REF Softkey. FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 2-4 Timer/References Window and Menu Turning all Vspeed flags on/off: AFCS 1) Press the TMR/REF Softkey. 2) Press the MENU Key. 3) To activate all Vspeed flags, press the ENT Key with All References On highlighted. ADDITIONAL FEATURES 4) To remove all Vspeed flags, turn the FMS Knob to highlight All References Off and press the ENT Key. Restoring all Vspeed defaults: 1) Press the TMR/REF Softkey. APPENDICES 2) Press the MENU Key. 3) Turn the FMS Knob to highlight Restore Defaults and press the ENT Key. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 49 SYSTEM OVERVIEW Flight Instruments Attitude Indicator FLIGHT INSTRUMENTS 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 EIS 2 6 AUDIO PANEL & CNS 3 4 FLIGHT MANAGEMENT 5 1 Roll Pointer 2 Roll Scale 3 Horizon Line 4 Aircraft Symbol 5 Land Representation 6 Pitch Scale 7 Slip/Skid Indicator 8 Sky Representation 9 Roll Scale Zero Figure 2-5 Attitude Indicator HAZARD AVOIDANCE 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˚. 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. APPENDICES ADDITIONAL FEATURES AFCS 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. INDEX Figure 2-6 Slip/Skid Indication 50 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Instruments SYSTEM OVERVIEW Altimeter FLIGHT INSTRUMENTS 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. EIS A magenta Altitude Trend Vector extends up or down the left of the altitude tape, the end resting at 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. T urn the ALT Knob to set the Selected Altitude (large knob for 1000-ft increments, small knob for 100-ft increments (increments reduce to 10 feet for approach). If set, the Minimum Descent Altitude/Decision Height (MDA/DH) value is also available for the Selected Altitude. Selected Altitude Bug Barometric Minimums Bug Indicated Altitude (Meters) Barometric Setting Box (Hectopascals) ADDITIONAL FEATURES Barometric Setting Selected Altitude Bug AFCS Indicated Altitude Selected Altitude (Meters) HAZARD AVOIDANCE Altitude Trend Vector FLIGHT MANAGEMENT Selected Altitude AUDIO PANEL & CNS Setting the Selected Altitude: Figure 2-7 Altimeter Settings, In Hg and Metric APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 51 SYSTEM OVERVIEW Flight Instruments Altitudes can also be displayed in meters (Figure 2-7). Note that the altitude tape does not change scale. Displaying altitude in meters: FLIGHT INSTRUMENTS 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 to return to the top-level softkeys. AUDIO PANEL & CNS EIS The barometric pressure setting is displayed below the Altimeter in inches of mercury (in Hg) or hectopascals (hPa) when metric units are selected. Adjusting the altimeter barometric pressure setting creates discontinuities in VNV vertical navigation, moving the descent path. For large adjustments, it may take several minutes for the aircraft to re-establish on the descent patch. 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. Selecting the altimeter barometric pressure setting: Turn the BARO Knob to select the desired setting. FLIGHT MANAGEMENT Selecting standard barometric pressure (29.92 in Hg): 1) Press the PFD Softkey to display the second-level softkeys.. HAZARD AVOIDANCE 2) Press the STD BARO Softkey; STD BARO is displayed in barometric setting box. Figure 2-8 Standard Barometric Altimeter Setting AFCS Changing altimeter barometric pressure setting units: 1) Press the PFD Softkey to display the second-level softkeys. ADDITIONAL FEATURES 2) Press the ALT UNIT Softkey. 3) Press the IN Softkey to display the barometric pressure setting in inches of mercury (in Hg). Or, press the HPA Softkey to display the barometric pressure setting in hectopascals (hPa). INDEX APPENDICES 4) Press the BACK Softkey to return to the top-level softkeys. 52 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Instruments SYSTEM OVERVIEW A Baro Transition Alert is provided to alert the pilot to change the barometric pressure setting when crossing the transition altitude in either direction. This is displayed by the flashing light blue barometric pressure setting when crossing the transition altitude. The flashing stops when the barometric pressure setting is changed. FLIGHT INSTRUMENTS 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. EIS 5) Turn the small FMS Knob to change the altitude and press the ENT Key. 6) To cancel the selection, press the FMS Knob. AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Figure 2-9 Aux System Setup Page, Baro Transition Alert Vertical Speed Indicator (VSI) APPENDICES The Vertical Speed Indicator (VSI) displays the aircraft vertical speed on a fixed scale with labels at 1000 and 2000 fpm and minor tick marks every 500 fpm. Digits appear in the pointer when the climb or descent rate is greater than 100 fpm. If the rate of ascent/descent exceeds 2000 fpm, the pointer appears at the edge of the tape and the rate appears inside the pointer. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 53 SYSTEM OVERVIEW Flight Instruments Vertical Deviation Note: The Glidepath Indicator is only shown for aircraft with GIA 63W Integrated Avionics Units when FLIGHT INSTRUMENTS WAAS is available. EIS The Vertical Deviation Indicator (VDI) 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. AUDIO PANEL & CNS The Glideslope Indicator 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. FLIGHT MANAGEMENT The glidepath is analogous to the glideslope for GPS approaches supporting WAAS vertical guidance (LNAV+V, L/VNAV, LPV). When an approach of this type is loaded into the flight plan and GPS is the selected navigation source, the Glidepath Indicator appears as a magenta diamond. If the approach type downgrades past the final approach fix (FAF), “NO GP” is displayed in place of the diamond. Full-scale deflection of two dots is 1000 feet. HAZARD AVOIDANCE VNV Target Altitude Marker Beacon Annunciation Vertical Speed Indicator Vertical Speed Pointer AFCS Vertical Deviation Indicator Glipepath Indicator Glideslope Indicator ADDITIONAL FEATURES Required Vertical Speed Indicator APPENDICES Vertical Speed and Deviation Indicator (VSI and VDI) Glideslope Indicator Glidepath Indicator INDEX Figure 2-10 Vertical Speed and Vertical Deviation Indications 54 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Instruments SYSTEM OVERVIEW Horizontal Situation Indicator (HSI) FLIGHT INSTRUMENTS 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: EIS 1) Press the PFD Softkey 2) Press the HSI FRMT Softkey. 3) Press the 360 HSI or ARC HSI Softkey. AUDIO PANEL & CNS 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. 14 FLIGHT MANAGEMENT 15 13 1 12 HAZARD AVOIDANCE 2 11 3 10 4 5 9 6 AFCS 8 7 9 Lateral Deviation Scale 2 Current Track Indicator 10 Flight Phase 3 To/From Indicator 11 Course Pointer 4 Navigation Source 12 Heading Bug 5 Aircraft Symbol 13 6 7 Course Deviation Indicator (CDI) Rotating Compass Card 15 8 OBS Mode Active APPENDICES Turn Rate Indicator ADDITIONAL FEATURES 1 Turn Rate and Heading Trend Vector 14 Current Heading Lubber Line INDEX Figure 2-11 Horizontal Situation Indicator (360˚ HSI) 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 55 SYSTEM OVERVIEW Flight Instruments FLIGHT INSTRUMENTS 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 Current Track Indicator Flight Phase Annunciation EIS Navigation Source Course Deviation and To/From Indicator AUDIO PANEL & CNS Lateral Deviation Scale Figure 2-12 Arc HSI FLIGHT MANAGEMENT The selected heading is shown to the upper left of the HSI for 3 seconds after being adjusted. The light blue heading bug on the compass rose corresponds to the selected heading. While the HSI is displayed as an arc, if the heading bug is adjusted off the shown portion of the compass rose, the digital reading is displayed. HAZARD AVOIDANCE Adjusting the selected heading: Turn the HDG Knob to set the selected heading. Press the HDG Knob to synchronize the bug to the current heading. The Selected Course is shown to the upper right of the HSI for 3 seconds after being adjusted. While the HSI is displayed as an arc, the Selected Course is displayed whenever the Course Pointer is not within the 140˚ currently shown. ADDITIONAL FEATURES AFCS Adjusting the Selected Course: Turn the CRS Knob to set the Selected Course. 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 Heading Heading Bug APPENDICES Selected Heading Selected Course INDEX Figure 2-13 Heading and Course Indications (Magnetic) 56 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Instruments SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS EIS Figure 2-14 Heading and Course Indications (True) AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 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) HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 2-15 Navigation Angle Settings (AUX - System Setup Page) INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 57 SYSTEM OVERVIEW Flight Instruments Turn Rate Indicator FLIGHT INSTRUMENTS The Turn Rate Indicator is located directly above the rotating compass card. 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 6 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. EIS Half-standard Turn Rate Arrow Shown for Turn Rate > 4 deg/sec AUDIO PANEL & CNS Standard Turn Rate Figure 2-16 Turn Rate Indicator and Trend Vector Bearing Pointers and Information Windows HAZARD AVOIDANCE FLIGHT MANAGEMENT Two bearing pointers and associated information can be displayed on the HSI for NAV, GPS, and ADF sources by pressing the PFD Softkey then a BRG or DME Softkey. The bearing pointers are light blue and are single-line (BRG1) or double-line (BRG2). A pointer symbol is shown in the information windows 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 Bearing 2 Pointer AFCS Distance ADDITIONAL FEATURES Distance to Bearing Source Station Identifier ADF Frequency Bearing Source Pointer 1 Pointer 2 Bearing Source APPENDICES Bearing 1 Information Window Bearing 2 Information Window INDEX Figure 2-17 HSI with Bearing and Distance Information 58 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Instruments SYSTEM OVERVIEW 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: • Station/waypoint identifier (NAV, GPS) • Pointer icon (BRG1 = single line, BRG2 = double line) • GPS-derived great circle distance to bearing source FLIGHT INSTRUMENTS • Bearing source (NAV, GPS, ADF) EIS • Frequency (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. AUDIO PANEL & CNS 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. Selecting bearing display and changing sources: 1) Press the PFD Softkey. FLIGHT MANAGEMENT 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) To remove the bearing pointer and information window, press the BRG Softkey again. HAZARD AVOIDANCE DME Information Window The DME Information Window is displayed above the BRG1 Information Window on the 360˚ HSI and in a box above and along side 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 tuning the DMEs. AFCS Displaying the DME Information Window: 1) Press the PFD Softkey. ADDITIONAL FEATURES 2) Press the DME Softkey to display the DME Information Window. 3) To remove the DME Information Window, press the DME Softkey again. APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 59 SYSTEM OVERVIEW Flight Instruments Course Deviation Indicator (CDI) NOTE: During a heading change of greater than 105˚ with respect to the course, the CDI on the Arc HSI FLIGHT INSTRUMENTS 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. EIS 360º HSI Arc HSI AUDIO PANEL & CNS Navigation Source Flight Phase Scale FLIGHT MANAGEMENT Crosstrack Error Navigation Source Flight Phase CDI CDI Scale CDI HAZARD AVOIDANCE Figure 2-18 Course Deviation Indicator APPENDICES ADDITIONAL FEATURES AFCS The CDI can display two sources of navigation, GPS or VOR/LOC. The color indicates the current navigation source, magenta for GPS and green for VOR and LOC. The full scale limits for the CDI are defined by a GPSderived distance when navigating GPS. When navigating using a VOR or localizer (LOC), the CDI uses the same angular deviation 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. INDEX Figure 2-19 Navigation Sources 60 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Instruments SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 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. NAV1 Selected for Tuning NAV2 Selected for Tuning EIS LOC1 Selected VOR2 Selected AUDIO PANEL & CNS GPS Selected FLIGHT MANAGEMENT Selecting the CDI Softkey Cycles through Navigation Sources Figure 2-20 Selecting a Navigation Source HAZARD AVOIDANCE 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. AFCS • 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. ADDITIONAL FEATURES 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. APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 61 SYSTEM OVERVIEW Flight Instruments GPS CDI Scaling FLIGHT INSTRUMENTS 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. EIS 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. AUDIO PANEL & CNS 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. ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT 5) To cancel the selection, press the FMS Knob or the CLR Key. Figure 2-21 GPS CDI Settings (AUX-System Setup Page) INDEX APPENDICES When set to Auto (default), the GPS CDI scale automatically adjusts to the desired limits based upon the current phase of flight (Figure 2-22, Table 2-1). 62 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Enroute (Oceanic if >200 nm from nearest airport) Terminal Approach 0.3 nm 1.0 nm 1.0 nm 2.0 nm 0.3 nm 1.0 nm Terminal Refer to accompanying approach CDI scaling figures FLIGHT INSTRUMENTS Departure SYSTEM OVERVIEW CDI Full-scale Deflection Flight Instruments Missed Approach EIS AUDIO PANEL & CNS Figure 2-22 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: FLIGHT MANAGEMENT - 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 (see Glossary for leg type definitions) - After any leg in the departure procedure that is not a CA or FA HAZARD AVOIDANCE • 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. AFCS • 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 (2.0 nm). ADDITIONAL FEATURES • 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: - When navigating with an active arrival route, the flight phase and CDI scale does not change until the aircraft arrives at the first waypoint in the arrival route (if within 31 nm from the destination airport). APPENDICES • During approach, the CDI scale ramps down even further (Figures 2-23 and 2-24). 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 activated 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. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX - 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. 63 2 nm FAF CDI scale varies if VTF is activated 0.3 nm 1.0 nm 2 nm FAF EIS angle based on database information course width angle set by system CDI Full-scale Deflection 0.3 nm 1.0 nm CDI scale is set to the smaller of 0.3 nm or an angle set by the system 350 ft FLIGHT INSTRUMENTS CDI Full-scale Deflection SYSTEM OVERVIEW Flight Instruments Landing Threshold CDI scale varies if VTF is activated Figure 2-23 Typical LNAV and LNAV+V Approach CDI Scaling Figure 2-24 Typical LNAV/VNAV and LPV Approach CDI Scaling AUDIO PANEL & CNS • 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 FLIGHT MANAGEMENT - The next leg in the missed approach procedure is not a CA, CD, CF, CI, CR, DF, FA, FC, FD, FM, IF, or TF AFCS HAZARD AVOIDANCE - After any leg in the missed approach procedure that is not a CA or FA Flight Phase Departure Terminal Enroute Oceanic Annunciation* DPRT TERM ENR OCN Approach (Non-precision) LNAV APPENDICES ADDITIONAL FEATURES Approach (Non-precision with Vertical Guidance) Approach (LNAV/VNAV) Approach (LPV) Missed Approach Automatic CDI Full-scale Deflection 0.3 nm 1.0 nm 2.0 nm 2.0 nm 1.0 nm decreasing to 350 feet depending on variables (Figure 2-23) LNAV + V L/VNAV LPV MAPR 1.0 nm decreasing to a specified course width, then 0.3 nm, depending on variables (Figure 2-24) 0.3 nm * Flight phase annunciations are normally shown in magenta, but when cautionary conditions exist the color changes to yellow. INDEX Table 2-1 Automatic GPS CDI Scaling 64 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Instruments SYSTEM OVERVIEW OBS Mode NOTE: VNV is inhibited while automatic waypoint sequencing has been suspended. FLIGHT INSTRUMENTS 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. EIS While OBS 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 plan on the moving map retains the modified course line. AUDIO PANEL & CNS GPS Selected FLIGHT MANAGEMENT Extended Course Line OBS Mode Enabled Pressing the OBS Softkey Again Disables OBS Mode HAZARD AVOIDANCE Pressing the OBS Softkey Enables OBS Mode Figure 2-25 Omni-bearing Selector (OBS) Mode AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 65 SYSTEM OVERVIEW Flight Instruments Enabling/disabling OBS Mode while navigating a GPS flight plan: 1) Press the OBS Softkey to select OBS Mode. FLIGHT INSTRUMENTS 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. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 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 2-26. Pressing the SUSP Softkey deactivates the suspension and resumes automatic sequencing of approach waypoints. HAZARD AVOIDANCE Pressing the SUSP Softkey Suspends Waypoint Sequencing SUSP Annunciation INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 2-26 Suspending Automatic Waypoint Sequencing 66 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Instruments SYSTEM OVERVIEW 2.2 Supplemental Flight Data FLIGHT INSTRUMENTS Note: Pressing the DFLTS Softkey turns off metric Altimeter display, the Inset Map and wind data display. In addition to the flight instruments, the PFD also displays various supplemental information, including temperatures, wind data, and Vertical Navigation (VNV) indications. Outside Air Temperature EIS The Outside Air Temperature (OAT) is displayed in degrees Celsius (°C) or Fahrenheit (°F) as selected by the pilot, in the lower left of the PFD under normal display conditions. Temperature is displayed below the true airspeed in reversionary mode. AUDIO PANEL & CNS Normal Display FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS Reversionary Mode ADDITIONAL FEATURES APPENDICES INDEX Figure 2-27 Outside Air Temperature 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 67 SYSTEM OVERVIEW Flight Instruments Changing temperature display units: 1) Select the AUX - System Setup Page on the MFD using the FMS Knob. FLIGHT INSTRUMENTS 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight the TEMP field in the Display Units box. 4) Turn the small FMS Knob to highlight either CELSIUS or FAHRENHEIT and press the ENT Key to confirm the selection. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 5) To cancel the selection, press the FMS Knob or the CLR Key. INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 2-28 Temperature Selection (AUX-System Setup Page) 68 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Instruments SYSTEM OVERVIEW Wind Data Option 2 Option 3 No Data EIS Option 1 FLIGHT INSTRUMENTS 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. Wind data can be displayed in three different ways. AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 2-29 Wind Data HAZARD AVOIDANCE 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 or tailwind and crosswind components • OPTN 2: Wind direction arrow and numeric speed • OPTN 3: Total wind direction arrow with numeric headwind or tailwind and crosswind speed components AFCS ADDITIONAL FEATURES 4) To remove the window, press the OFF Softkey. APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 69 SYSTEM OVERVIEW Flight Instruments Vertical Navigation (VNV) Indications FLIGHT INSTRUMENTS 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” message 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 the table. Top of Descent Message EIS VNV Target Altitude AUDIO PANEL & CNS Vertical Deviation Indicator FLIGHT MANAGEMENT Required Vertical Speed Indicator HAZARD AVOIDANCE GPS is the Selected Navigation Source Phase of Flight Figure 2-30 Vertical Navigation Indications (PFD) APPENDICES ADDITIONAL FEATURES AFCS VNV Indication Removed Criteria 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 pressed 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 INDEX Table 2-2 VNV Indication Removal Criteria 70 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Instruments SYSTEM OVERVIEW 2.3 PFD Annunciations and Alerting Functions FLIGHT INSTRUMENTS The following annunciations and alerting functions are displayed on the PFD. Refer to Appendix A for more information on alerts and annunciations. System Alerting EIS Messages appear in the Alerts Window in the lower right corner of the PFD when a warning, caution, advisory alert, or G1000 message advisory occurs. System alert messages are provided for awareness of G1000 system problems or status and may or may not require pilot action. The Alerts Window allows system alerts to be displayed simultaneously. The FMS Knob is used to scroll through the alert messages. The Alerts Window is enabled/disabled by pressing the ALERTS Softkey. If the window is already open when a new message is generated, pressing the ALERTS Softkey to acknowledge the message turns the softkey gray. AUDIO PANEL & CNS The ALERTS Softkey label changes to display the appropriate annunciation when an alert is issued. The annunciation flashes and the appropriate aural alert sounds until acknowledged by pressing the softkey. The softkey then reverts to the ALERTS label, and when pressed again opens the Alerts Window to display a descriptive message of the alert. FLIGHT MANAGEMENT The Annunciation Window appears to the right of the Vertical Speed Indicator and displays abbreviated annunciation text for aircraft alerts. Warnings appear in red, cautions in yellow, advisory alerts in white, and safe operating annunciations in green. New alerts are displayed at the top of the Annunciation Window, regardless of priority. Once acknowledged, they are sequenced based on priority. HAZARD AVOIDANCE Annunciation Window Alerts Window AFCS ADDITIONAL FEATURES Softkey Annunciations Figure 2-31 G1000 Alerting System APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 71 SYSTEM OVERVIEW Flight Instruments Marker Beacon Annunciations FLIGHT INSTRUMENTS 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. Middle Marker Inner Marker EIS Outer Marker AUDIO PANEL & CNS Altimeter Figure 2-32 Marker Beacon Annunciations FLIGHT MANAGEMENT Traffic Annunciation Traffic is displayed symbolically on the PFD Inset Map, the MFD Navigation Map Page, and various other MFD page maps. Refer to the Hazard Avoidance Section and Appendix for more details about the Traffic Information Service (TIS) and optional Traffic Advisory Systems (TAS). When a traffic advisory (TA) is detected, the following automatically occur: HAZARD AVOIDANCE • The PFD Inset Map is enabled and displays traffic. • A flashing black-on-yellow TRAFFIC annunciation appears to the top left of the Attitude Indicator for five seconds and remains displayed until no TAs are detected in the area. • A single “TRAFFIC” aural alert is heard, unless an optional Traffic Advisory System (TAS) is installed. Refer to the applicable TAS documentation for alerts generated by TAS equipment. ADDITIONAL FEATURES AFCS If additional TAs appear, new aural and visual alerts are generated. APPENDICES Traffic Symbols INDEX Figure 2-33 Traffic Annunciation and Inset Map with TAS Traffic Displayed 72 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Instruments SYSTEM OVERVIEW Altitude Alerting FLIGHT INSTRUMENTS Altitude Alerting provides the pilot with a visual alert when approaching the Selected Altitude. Whenever the Selected Altitude is changed, the Altitude Alerter is reset. The Altitude Alerter is independent of the GFC 700 AFCS, but alerting tones are heard only when the GFC 700 is installed. The following occur when approaching the Selected Altitude: • Upon passing through 1000 feet of the Selected Altitude an aural tone is heard. The Selected Altitude changes to black text on a light blue background and flashes for 5 seconds. EIS • 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 5 seconds. Within 1000 ft Within 200 ft AUDIO PANEL & CNS • After reaching the Selected Altitude, if the pilot flies outside the deviation band (±200 feet of the Selected Altitude) an aural tone is heard. The Selected Altitude changes to yellow text on a black background and flashes for 5 seconds. Deviation of ±200 ft FLIGHT MANAGEMENT Figure 2-34 Altitude Alerting Visual Annunciations Low Altitude Annunciation HAZARD AVOIDANCE NOTE: A Low Altitude Annunciation is available only when WAAS is available. AFCS When the Final Approach Fix (FAF) is the active waypoint in a GPS WAAS 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 right of the Altimeter, flashing for several seconds, then remaining displayed until the condition is resolved. ADDITIONAL FEATURES Figure 2-35 Low Altitude on GPS WAAS Approach APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 73 SYSTEM OVERVIEW Flight Instruments Minimum Descent Altitude/Decision Height Alerting FLIGHT INSTRUMENTS For altitude awareness, a barometric Minimum Descent Altitude (MDA) or Decision Height (DH) can be set in the Timer/References Window and is reset when the power is cycled. When active, the altitude setting is displayed to the bottom left of the Altimeter. Once the altitude is within the range of the tape, a bug appears at the reference altitude on the Altimeter. The following visual annunciations occur when approaching the MDA/DH: • When the aircraft altitude descends to within 2500 feet of the MDA/DH setting, the BARO MIN box appears with the altitude in light blue text. The bug appears on the altitude tape in light blue once in range. EIS • When the aircraft passes through 100 feet of the MDA/DH, the bug and text turn white. • Once the aircraft reaches MDA/DH, the bug and text turn yellow and the aural alert, “Minimums. Minimums”, is heard. FLIGHT MANAGEMENT AUDIO PANEL & CNS Light Blue Within 2500 ft White Within 100 ft Yellow When Altitude Reached Barometric Minimum Bug HAZARD AVOIDANCE Barometric Minimum Box Figure 2-36 Barometric MDA/DH Alerting Visual Annunciations Setting the barometric Minimum Descent Altitude/Decision Height and bug: AFCS 1) Press the TMR/REF Softkey. 2) Turn the large FMS Knob to highlight the Minimums field. ADDITIONAL FEATURES 3) Turn the small FMS Knob to select BARO. 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 from zero to 16,000 feet. APPENDICES 5) To remove the window, press the CLR Key or the TMR/REF Softkey. Figure 2-37 Barometric MDA/DH INDEX Alerting is inhibited while the aircraft is on the ground and until the aircraft reaches 150 feet above the MDA. If the aircraft proceeds to climb after having reached the MDA, once it reaches 50 feet above the MDA, alerting is disabled. 74 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Instruments SYSTEM OVERVIEW 2.4 Abnormal Operations Abnormal GPS Conditions FLIGHT INSTRUMENTS The annunciations listed in the table can appear on the HSI when abnormal GPS conditions occur. Annunciation LOI DR 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 5 seconds) Dead Reckoning–System is using projected position rather than GPS position to compute navigation data and sequence active flight plan waypoints EIS INTEG OK Location Lower left of aircraft symbol Lower left of aircraft symbol Upper right of aircraft symbol AUDIO PANEL & CNS Table 2-3 Abnormal GPS Conditions Annunciated on HSI FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 2-38 Example HSI Annunciations In Dead Reckoning (DR) Mode the CDI is removed from the display when GPS is the selected navigation source. The following items on the PFD are then shown in yellow: AFCS • Current Track Bug • Wind Data (calculated based on GPS information) • Distances in the Bearing Information Windows ADDITIONAL FEATURES • GPS bearing pointers 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. Refer to the Flight Management Section for more information on DR Mode APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 75 SYSTEM OVERVIEW Flight Instruments Unusual Attitudes FLIGHT INSTRUMENTS When the aircraft enters an unusual pitch attitude, red chevrons pointing toward the horizon warn of extreme pitch. The chevrons are displayed on the Attitude Indicator, starting at 50˚ above and 30˚ below the horizon line. Nose Low AUDIO PANEL & CNS EIS Nose High FLIGHT MANAGEMENT Figure 2-39 Pitch Attitude Warnings HAZARD AVOIDANCE 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 their softkeys are disabled when the aircraft experiences unusual attitudes: • Traffic Annunciations • System Time • Minimum Descent Altitude/ Decision Height Readout • AFCS Annunciations • PFD Setup Menu • Inset Map • Windows displayed in the lower right corner of the PFD: • Vertical Deviation, Glideslope, and Glidepath Indicators • Outside Air Temperature (OAT) – Timer/References • Altimeter Barometric Setting • Wind Data – Nearest Airports • Selected Altitude • Selected Heading Readout – Flight Plan • VNV Target Altitude • Selected Course Readout – Messages • Transponder Status Box – Procedures INDEX APPENDICES ADDITIONAL FEATURES AFCS • Flight Director Command Bars 76 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Engine Indication System SYSTEM OVERVIEW Section 3 Engine Indication System (EIS) NOTE: Refer to the Aircraft Flight Manual (AFM) for limitations. FLIGHT INSTRUMENTS The G1000 Engine Indication System (EIS) for the Diamond DA42NG displays critical engine, electrical, fuel, and other system parameters on the left side of the Multi Function Display (MFD) during normal operations (Figure 3-1). EIS EIS Display AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 3-1 Multi Function Display (Normal) EIS information is presented in three displays, accessed using the ENGINE Softkey on the MFD: AFCS • Engine Display – Default display, shows all critical engine and fuel indicators • System Display – Shows graphic and numeric readouts of critical engine and electrical indicators • Fuel Display – Shows numeric readouts of fuel indicators and calculations ADDITIONAL FEATURES The engine load indicator and tachometer are present on all three displays. APPENDICES The EIS instrument types include vertical slider gauges, horizontal slide bar indicators, and digital readouts. Green bands indicate normal ranges of operation; yellow and red bands indicate caution and warning, respectively. When unsafe operating conditions occur, readouts and labels may change color corresponding to the level of the condition. The pointers (labeled left, L, and right, R) on the horizontal bar indicators appear in white to indicate normal operation and change to yellow or red to indicate caution or warning conditions. If sensory data to an instrument becomes invalid or unavailable, a red “X” is shown across the instrument. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 77 SYSTEM OVERVIEW Engine Indication System FLIGHT INSTRUMENTS In reversionary display mode, the remaining display is re-configured to present PFD symbology together with the EIS Display (Figure 3-2). When the G1000 displays enter reversionary mode, each EIS Display (Engine, System, Fuel) and the softkey functionality remains the same (refer to the System Overview for information about display Reversionary Mode). FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS EIS Display INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Figure 3-2 Primary Flight Display (Reversionary Mode) 78 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Engine Indication System SYSTEM OVERVIEW The Engine softkeys provide access to the three EIS Displays (Engine, System, Fuel). To return to the Engine Display from the System or Fuel Display, press the ENGINE or BACK Softkey. ENGINE SYSTEM FLIGHT INSTRUMENTS ENGINE BACK FUEL Press the BACK Softkey to return to the top-level softkeys. ENGINE SYSTEM FUEL DEC FUEL INC FUEL RST FUEL BACK EIS Figure 3-3 EIS Softkeys AUDIO PANEL & CNS Displays second-level engine softkeys Displays the EIS System Display Displays the EIS Fuel Display Decreases displayed fuel remaining in 1-gal increments Increases displayed fuel remaining in 1-gal increments Resets displayed fuel remaining to maximum fuel capacity for aircraft and fuel used to zero FLIGHT MANAGEMENT • ENGINE • SYSTEM • FUEL DEC FUEL INC FUEL RST FUEL HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 79 SYSTEM OVERVIEW Engine Indication System 3.1 Engine Display FLIGHT INSTRUMENTS Note: The Fuel Quantity Indicator shows 25 gallons per side when full. The Engine Display is the default EIS display and can be selected by pressing the ENGINE or BACK Softkey when another EIS display is currently shown. Beneath the vertical slider gauges are readouts for fuel flow and horizontal bar indicators for oil temperature and pressure, coolant temperature, and fuel temperature and quantity. 1 AUDIO PANEL & CNS EIS Engine Load Indicator (LOAD %) 2 Tachometer (RPM) FLIGHT MANAGEMENT 3 4 5 HAZARD AVOIDANCE 6 7 Displays engine oil pressure ranges Displays coolant temperature ranges Displays fuel temperature ranges Displays the quantity of fuel in the tanks, in gallons (gal); up to 25 gal per side can be indicated INDEX APPENDICES ADDITIONAL FEATURES AFCS 8 Fuel Flow Indicator (FUEL FLOW GPH) Oil Temperature Indicator (OIL TEMP) Oil Pressure Indicator (OIL PRES) Coolant Temperature Indicator (COOLANT TEMP) Fuel Temperature Indicator (FUEL TEMP) Fuel Quantity Indicator (FUEL QTY GAL) Displays current engine loads as percentages on a vertical slider gauge with digital readouts below the gauge Displays propeller speeds in revolutions per minute (rpm) on a vertical slider gauge with digital readouts below the gauge Gauge indicators display propeller speed information provided by the FADEC. Digital readouts flash red to indicate an overspeed warning. Displays digital readouts of current fuel flow for each engine in gallons per hour (gph) Displays engine oil temperature ranges 80 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Engine Indication System SYSTEM OVERVIEW FLIGHT INSTRUMENTS 1 EIS AUDIO PANEL & CNS 2 FLIGHT MANAGEMENT 3 4 HAZARD AVOIDANCE 5 6 AFCS 7 ADDITIONAL FEATURES 8 APPENDICES Figure 3-4 Engine Display INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 81 SYSTEM OVERVIEW Engine Indication System 3.2 System Display FLIGHT INSTRUMENTS The System Display is accessed by pressing the SYSTEM Softkey. The instruments presented here, in addition to the engine load indicator and tachometer, are separated into three categories: Electrical (voltmeter and ammeter), Engine (gearbox and coolant temperature), and Oil (temperature and pressure). A horizontal bar indicator for deice fluid is located at the bottom of the display as an option. Accessing the EIS System Display: 1) Press the ENGINE Softkey. EIS 2) Press the SYSTEM Softkey. 3) To return to the default Engine Display, press the ENGINE or BACK Softkey. 1 Displays current engine loads as percentages on a vertical bar gauge with digital readouts below the gauge Displays propeller speeds in revolutions per minute (rpm) on a vertical slider gauge with digital readouts below the gauge Gauge indicators display propeller speed information provided by the FADEC. Digital readouts flash red to indicate an overspeed warning. Displays the primary bus voltage for each side with accompanying Voltmeter digital readouts (VOLTS) Displays each alternator load in amperes (amps) with accompanying Ammeter digital readouts (AMPS) Gearbox Temperature Indicator Displays the temperature of each gearbox in degrees Celsius (°C) (GEARBOX °C) Coolant Temperature Indicator Displays the coolant temperature of each side in °C (COOLANT °C) Displays oil temperature in °C Oil Temperature Indicator (OIL °C) Displays oil pressure in bars Oil Pressure Indicator (OIL BAR) Displays the quantity of deice fluid; tick marks are located at quarter Deice Fluid Indicator intervals (DEICE FLUID) (Optional) FLIGHT MANAGEMENT AUDIO PANEL & CNS Engine Load Indicator (LOAD %) 2 Tachometer (RPM) 3 HAZARD AVOIDANCE 4 5 AFCS 6 7 ADDITIONAL FEATURES 8 INDEX APPENDICES 9 82 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Engine Indication System SYSTEM OVERVIEW FLIGHT INSTRUMENTS 1 EIS AUDIO PANEL & CNS 2 FLIGHT MANAGEMENT 3 4 HAZARD AVOIDANCE 5 AFCS 6 ADDITIONAL FEATURES 7 8 9 APPENDICES Figure 3-5 System Display INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 83 SYSTEM OVERVIEW Engine Indication System 3.3 Fuel Display NOTE: Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time FLIGHT INSTRUMENTS the fuel was reset. Note: If optional auxiliary fuel tanks are installed, the fuel remaining can be adjusted up to a maximum of 76.4 gal; the Fuel Quantity Indicator does not account for fuel in the auxiliary tanks. EIS The Fuel Display is accessed by pressing the FUEL Softkey. Besides the engine load indicator and tachometer, all indications on this display are digital readouts, separated into two categories: Fuel and Fuel Calculations. Total aircraft time in service is at the bottom of the display. AUDIO PANEL & CNS Accessing the EIS Fuel Display: 1) Press the ENGINE Softkey. 2) Press the FUEL Softkey. FLIGHT MANAGEMENT 3) To return to the default Engine Display, press the ENGINE or BACK Softkey. 1 HAZARD AVOIDANCE Engine Load Indicator (LOAD %) 2 Tachometer (RPM) 3 AFCS 4 5 ADDITIONAL FEATURES 6 7 APPENDICES 8 9 Displays a digital readout of current fuel flow for each engine in gallons per hour (gph) Displays a digital readout of fuel temperature for each tank in degrees Celsius (°C) Displays current fuel remaining (gal) as set by the pilot and adjusted for fuel burn since last set Displays quantity of fuel used (gal) based on fuel flow since last reset Displays flight time remaining (HH:MM) based on the calculated fuel remaining Displays aircraft range in nautical miles (nm) based on the calculated fuel remaining Displays the aircraft’s total flight hours (hrs); activated when the aircraft becomes airborne INDEX 10 Fuel Quantity Indicator (FUEL GAL) Fuel Flow Indicator (FUEL GPH) Fuel Temperature Indicator (FUEL °C) Set Fuel Remaining (GAL REM) Calculated Fuel Used (GAL USED) Calculated Endurance (ENDUR) Calculated Range (RANGE NM) Total Time in Service (TTL TIME IN SVC) Displays current engine loads as percentages on a vertical bar gauge with digital readouts below the gauge Displays propeller speeds in revolutions per minute (rpm) on a vertical slider gauge with digital readouts below the gauge Gauge indicators display propeller speed information provided by the FADEC. Digital readouts flash red to indicate an overspeed warning. Displays a digital readout of fuel in the tanks, in gallons (gal) 84 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Engine Indication System SYSTEM OVERVIEW Fuel calculations are based on the fuel flow totalizer and the displayed fuel remaining (GAL REM), adjusted by the pilot using the following softkeys: • DEC FUEL – Decreases totalizer-based fuel remaining in one-gallon increments FLIGHT INSTRUMENTS • INC FUEL – Increases totalizer-based fuel remaining in one-gallon increments • RST FUEL – Resets totalizer-based fuel remaining (GAL REM) relative to the aircraft’s fuel capacity and sets the displayed fuel used (GAL USED) to zero Adjusting the fuel totalizer quantity: EIS From the Fuel Display, press the DEC FUEL or INC FUEL Softkey to obtain the desired number of gallons remaining (GAL REM). Resetting the fuel totalizer: From the Fuel Display, press the RST FUEL Softkey. This resets the displayed fuel remaining (GAL REM) to 50 gallons (or 76.4 gallons if optional aux fuel tanks are installed). The fuel used (GAL USED) is reset to zero. AUDIO PANEL & CNS FLIGHT MANAGEMENT 1 HAZARD AVOIDANCE 2 3 AFCS 4 5 6 ADDITIONAL FEATURES 7 8 9 APPENDICES 10 INDEX Figure 3-6 Fuel Display 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 85 INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Engine Indication System Blank Page 86 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS SYSTEM OVERVIEW Section 4 Audio Panel and CNS FLIGHT INSTRUMENTS 4.1 Overview The Communication/Navigation/Surveillance (CNS) system includes the Audio Panel, communication radios, navigation radios, and Mode S transponder. The System Overview Section provides a block diagram description of the Audio Panel and CNS system interconnection. CNS operation in Diamond DA42NG aircraft is performed by the following Line Replaceable Units (LRUs): • Audio Panel • Multifunction Display (MFD) • Mode S Transponder EIS • Primary Flight Display (PFD) AUDIO PANEL & CNS • Integrated Avionics Unit (2) The MFD/PFD controls are used to tune the communication transceivers and navigation radios. FLIGHT MANAGEMENT The Audio Panel provides the traditional audio selector functions of microphone and receiver audio selection. The 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. HAZARD AVOIDANCE The Mode S transponder is controlled with softkeys and the FMS Knob located on the Primary Flight Display (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 reply status (Figure 4-1). AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 87 Audio Panel and CNS SYSTEM OVERVIEW MFD/PFD Controls and Frequency Display 2 3 4 6 5 7 8 FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 1 9 10 HAZARD AVOIDANCE 11 12 INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 4-1 MFD/PFD Controls, NAV/COM Frequency Tuning Boxes, and ADF/DME Tuning Window (PFD Shown) 88 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS 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, volume setting, and modes, and DME tuning selection. Display by pressing 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 transponder codes, enter ADF frequencies, select ADF/DME modes, 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 transponder. ADDITIONAL FEATURES 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. AFCS 4 HAZARD AVOIDANCE 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. FLIGHT MANAGEMENT 3 AUDIO PANEL & CNS NAV Frequency Transfer Key – Transfers the standby and active NAV frequencies. EIS 2 FLIGHT INSTRUMENTS 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. SYSTEM OVERVIEW 1 APPENDICES INDEX 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 89 SYSTEM OVERVIEW Audio Panel and CNS 3 4 5 6 7 8 9 10 11 12 14 15 16 AUDIO PANEL & CNS 2 13 FLIGHT MANAGEMENT 1 18 19 20 21 HAZARD AVOIDANCE EIS FLIGHT INSTRUMENTS Audio Panel Controls 22 23 17 24 AFCS Figure 4-2 Audio Panel Controls INDEX APPENDICES ADDITIONAL FEATURES NOTE: When a key is selected, a triangular annunciator above the key is illuminated. 90 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. 5 COM3 MIC – Not used in DA42NG aircraft. Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS SPKR – Selects and deselects the cabin 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. Also, stops play of recorded COM audio. 12 HI SENS – Press to increase marker beacon receiver sensitivity. Press again to return to low sensitivity. 13 DME – Turns optional DME audio on or off. 14 NAV1 – When selected, audio from the #1 NAV receiver can be heard. 15 ADF – Turns optional ADF receiver audio on or off. 16 NAV2 – When selected, audio from the #2 NAV receiver can be heard. 17 AUX – Not used in DA42NG aircraft. 18 MAN SQ – Enables manual squelch for the intercom. When the intercom is active, press the PILOT Knob to illuminate SQ. Turn the PILOT/PASS Knobs to adjust squelch. 19 PLAY – Press once to play the last recorded COM audio. Press again while audio is playing and the previous block of recorded audio is played. Each subsequent press plays each previously recorded block. Pressing the MKR/MUTE Key during play of a memory block stops play. 20 PILOT – Selects and deselects the pilot intercom isolation. 21 COPLT – Selects and deselects the copilot intercom isolation. 22 PILOT Knob – Press to switch between volume and squelch control as indicated by illumination of VOL or SQ. Turn to adjust intercom volume or squelch. The MAN SQ Key must be selected to allow squelch adjustment. 23 PASS Knob – Turn to adjust Copilot/Passenger intercom volume or squelch. The MAN SQ Key must be selected to allow squelch adjustment. 24 DISPLAY BACKUP Button – Manually selects Reversionary Mode. APPENDICES 10 ADDITIONAL FEATURES PA – Selects the passenger address system. The selected COM transmitter is deselected when the PA Key is pressed. AFCS 9 HAZARD AVOIDANCE TEL – Not used in DA42NG aircraft. FLIGHT MANAGEMENT 8 AUDIO PANEL & CNS COM 1/2 – Split COM Key. Allows simultaneous transmission on COM1 and COM2 by the pilot and copilot. EIS 7 FLIGHT INSTRUMENTS COM3 – Not used in DA42NG aircraft. SYSTEM OVERVIEW 6 INDEX 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 91 SYSTEM OVERVIEW Audio Panel and CNS 4.2 COM Operation FLIGHT INSTRUMENTS 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 G1000 for use, the system remembers the last frequencies used and the active EIS COM transceiver state prior to shutdown. AUDIO PANEL & CNS 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. During reception of audio from the COM radio selected for transmission, audio from the other COM radio is muted. FLIGHT MANAGEMENT An active COM frequency displayed in green indicates that the COM transceiver is selected on the Audio Panel (COM1 MIC or COM2 MIC Key). Both active COM frequencies appearing in white indicate that no COM radio is selected for transmitting (PA Key is selected on the Audio Panel). Frequencies in the standby field are displayed in either white or gray. The standby frequency in the tuning box is white. The other standby frequency is gray. HAZARD AVOIDANCE Active Fields Standby Fields Top Section of the Audio Panel AFCS Tuning Box ADDITIONAL FEATURES COM2 Radio is Selected on the Audio Panel INDEX APPENDICES Figure 4-3 Selecting a COM Radio for Transmit 92 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS SYSTEM OVERVIEW Transmit/Receive Indications FLIGHT INSTRUMENTS 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. Entertainment audio, if selected, is muted during active COM radio reception. Refer to Additional Audio Panel Functions later in this section, and details on the Data Link Receiver in the Additional Features Section. EIS AUDIO PANEL & CNS Transmit and Receive Indicators Annunciator Flashes During Transmission Figure 4-4 COM Radio Transmit and Receive Indications FLIGHT MANAGEMENT COM Transceiver Manual Tuning The COM frequency controls and frequency boxes are on the right side of the MFD and PFD. Manually tuning a COM frequency: HAZARD AVOIDANCE 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. AFCS Turn the VOL/SQ Knob to adjust volume. Press the Knob to Turn Automatic Squelch On or Off ADDITIONAL FEATURES 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 APPENDICES Figure 4-5 COM Frequency Tuning INDEX 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 93 SYSTEM OVERVIEW Audio Panel and CNS Selecting the Radio to be Tuned FLIGHT INSTRUMENTS Press the small COM Knob to transfer the frequency tuning box and Frequency Transfer Arrow between the upper and lower radio frequency fields. EIS Press the COM Knob to Switch the Tuning Box From One COM Radio to the Other AUDIO PANEL & CNS Figure 4-6 Switching COM Tuning Boxes Quick-tuning and Activating 121.500 MHz FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE Press for Two Seconds to Load 121.500 MHz INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 4-7 Quickly Tuning 121.500 MHz 94 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS SYSTEM OVERVIEW 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) FLIGHT INSTRUMENTS • WPT – Airport Information Page • NRST – Nearest Airspaces Page • NRST – Nearest Airports Page Auto-tuning from the PFD EIS 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. AUDIO PANEL & CNS Auto-tuning a COM frequency for a nearby airport from the PFD: 1) Press 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. FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Press the NRST Softkey to Open the Nearest Airports Window Figure 4-8 Nearest Airports Window (PFD) INDEX 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 95 SYSTEM OVERVIEW Audio Panel and CNS Auto-tuning from the MFD FLIGHT INSTRUMENTS 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 the appropriate softkey. 2) Turn the FMS Knob to place the cursor on the desired COM frequency (Figure 4-11). EIS 3) Press the ENT Key to load the COM frequency into the standby field of the selected COM radio. AUDIO PANEL & CNS 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 FLIGHT MANAGEMENT Turn the FMS Knob to Scroll Through a List of Frequencies Figure 4-9 Frequency Auto-Tuning from the MFD HAZARD AVOIDANCE Or: 1) 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 on the desired selection. AFCS 4) Scroll through the frequency selections with the FMS Knob or the ENT Key. 5) Press the ENT Key to load the COM frequency into the standby field of the selected COM radio. INDEX APPENDICES ADDITIONAL FEATURES 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 96 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS Press Frequency Transfer Key to Load Frequency into COM Active Frequency Field Selected Airport Identifier and Information EIS AUDIO PANEL & CNS Runway Information Press INFO Softkey for AIRPORT, RUNWAYS, and FREQUENCIES Windows HAZARD AVOIDANCE Figure 4-11 WPT – Airport Information Page FLIGHT MANAGEMENT Press ENT Key to Load Frequency into COM Standby Field. Cursor then Advances to Next Frequency. AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 97 SYSTEM OVERVIEW Audio Panel and CNS AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 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. INDEX APPENDICES ADDITIONAL FEATURES Figure 4-12 NRST – Nearest Airspaces, NRST – Nearest Airports, and NRST – Nearest Frequencies Pages 98 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS SYSTEM OVERVIEW Frequency Spacing FLIGHT INSTRUMENTS The G1000 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. COM channel spacing is set on the System Setup Page of the AUX Page Group. 25-kHz Channel Spacing EIS 8.33-kHz Channel Spacing Figure 4-13 COM Channel Spacing AUDIO PANEL & CNS Changing COM frequency channel spacing: 1) Select the AUX – System Setup Page. 2) Press the FMS Knob to activate the flashing cursor. FLIGHT MANAGEMENT 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 Window is selected, the G1000 softkeys are blank. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Select 8.33-kHz or 25.0-kHz COM Frequency Channel Spacing AUX - SYSTEM SETUP PAGE INDEX Figure 4-14 AUX – System Setup Page 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 99 SYSTEM OVERVIEW Audio Panel and CNS Automatic Squelch FLIGHT INSTRUMENTS 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. EIS Press the COM VOL/ SQ Knob to turn off Automatic Squelch. Press again to restore Automatic Squelch. Figure 4-15 Overriding Automatic Squelch AUDIO PANEL & CNS Volume FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE COM Volume Level Remains for Two Seconds INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 4-16 COM Volume Level 100 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS SYSTEM OVERVIEW 4.3 NAV Operation NAV Radio Selection and Activation FLIGHT INSTRUMENTS 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. EIS A NAV radio is selected for navigation by pressing the CDI Softkey located on the PFD. The active NAV frequency selected for navigation is displayed in green. Pressing the CDI Softkey once selects NAV1 as the navigation radio. Pressing the CDI Softkey a second time selects NAV2 as the navigation radio. Pressing the CDI Softkey a third time activates GPS mode. Pressing 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. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT • 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. Active Fields HAZARD AVOIDANCE Standby Fields Tuning Box AFCS The NAV Radio is Selected by Pressing the CDI Softkey ADDITIONAL FEATURES Figure 4-17 Selecting a NAV Radio for Navigation APPENDICES See the Flight Instruments Section for selecting the DME and Bearing Information windows and using VOR or ADF as the source for the bearing pointer. INDEX 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 101 SYSTEM OVERVIEW Audio Panel and CNS EIS FLIGHT INSTRUMENTS NAV radios are selected for listening by pressing the corresponding keys on the Audio Panel. Pressing the NAV1, NAV2, ADF, or DME Key selects and deselects the navigation radio source. Selected audio can be heard over the headset and the speaker (if selected). All radios can be selected individually or simultaneously. AUDIO PANEL & CNS Figure 4-18 Selecting a NAV Radio Receiver NAV Receiver Manual Tuning The NAV frequency controls and frequency boxes are on the left side of the MFD and PFD. FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 4) Press the NAV VOL/ID Knob to turn the Morse code identifier audio on and off. AFCS 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 ADDITIONAL FEATURES Turn the NAV Knob to Tune the Frequency in the Tuning Box INDEX APPENDICES Figure 4-19 NAV Frequency Tuning 102 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS Press the NAV Knob to Switch the Tuning Box From One NAV Radio to the Other EIS Figure 4-20 Switching NAV Tuning Boxes AUDIO PANEL & CNS 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. HAZARD AVOIDANCE The Morse Code Identifier for the GHM VOR is On FLIGHT MANAGEMENT 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 with the small NAV Knob and press the VOL/ID Knob again to turn the Morse code off in the other radio. Station Identifier Figure 4-21 NAV Radio ID Indication AFCS Volume ADDITIONAL FEATURES 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. APPENDICES NAV Volume Level Remains for Two Seconds Figure 4-22 NAV Volume Levels INDEX 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 103 SYSTEM OVERVIEW Auto-tuning a NAV Frequency from the MFD FLIGHT INSTRUMENTS Audio Panel and CNS • WPT – VOR Information • NRST – Nearest Frequencies (FSS, WX) • NRST – Nearest Airports • NRST – Nearest Airspaces NAV frequencies can be selected and loaded from the following MFD pages: • WPT – Airport Information • NRST – Nearest VOR EIS 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 (Figures 4-23, 4-24, and 4-25). AUDIO PANEL & CNS 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 the appropriate softkey. FLIGHT MANAGEMENT 2) Turn the FMS Knob to place the cursor on the desired NAV identifier or NAV frequency. 3) On the Nearest VOR and Nearest Airports pages, press the FREQ Softkey to place the cursor on the NAV frequency (Figure 4-25). 4) Press the ENT Key to load the NAV frequency into the standby field of the selected NAV radio. HAZARD AVOIDANCE 5) Press the Frequency Transfer Key to transfer the frequency to the NAV Active Frequency Field. AFCS 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 INDEX APPENDICES ADDITIONAL FEATURES Figure 4-23 NAV Frequency Auto-Tuning from the MFD 104 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 3) Press the ENT Key to place the cursor in the desired window. 4) Scroll through the frequency selections with the FMS Knob or the ENT Key. 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. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Nearest Airports Menu Nearest VOR Menu Figure 4-24 Nearest Pages Menus HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 105 SYSTEM OVERVIEW Audio Panel and CNS AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 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. FLIGHT MANAGEMENT Press the ENT Key to Load the Frequency into the NAV Standby Field. HAZARD AVOIDANCE Press the VOR Softkey to Place the Cursor on the VOR Identifier Press the FREQ Softkey to Place the Cursor on the VOR Frequency INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 4-25 Loading the NAV Frequency from the NRST – Nearest VOR Page 106 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 4-26 NRST – Nearest Frequencies, WPT – VOR Information, WPT – Airport Information, and NRST – Nearest Airports Pages INDEX 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 107 SYSTEM OVERVIEW Audio Panel and CNS Auto-tuning NAV Frequencies on Approach Activation FLIGHT INSTRUMENTS 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 while navigating by GPS, the system automatically switches to LOC 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. EIS When loading or activating a VOR or ILS/LOC approach, the approach frequency is automatically transferred to a NAV frequency field as follows: AUDIO PANEL & CNS • If the current CDI navigation source is GPS, the approach frequency is transferred to the NAV1 active frequency field. The frequency that was previously in the NAV1 active frequency field is transferred to standby. FLIGHT MANAGEMENT • If the current CDI navigation source is GPS, and if the approach frequency is already loaded into the NAV1 standby frequency field, the standby frequency is transferred to active. INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE • 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. 108 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS SYSTEM OVERVIEW Marker Beacon Receiver NOTE: The marker beacon indicators operate independently of marker beacon audio and cannot be turned FLIGHT INSTRUMENTS 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. Middle Marker Indication Inner Marker Indication EIS Outer Marker Indication AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 4-27 Marker Beacon Annunciations on the PFD HAZARD AVOIDANCE Figure 4-28 Marker Beacon Keys AFCS The Audio Panel provides 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. ADDITIONAL FEATURES During marker beacon audio reception, pressing the MKR/MUTE Key mutes the audio but does not affect the marker annunciations (Figure 4-27). 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. APPENDICES 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. INDEX 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 109 SYSTEM OVERVIEW ADF/DME Tuning FLIGHT INSTRUMENTS 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. EIS Audio Panel and CNS 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. NOTE: When another auxiliary window is turned on, the ADF/DME Tuning Window is replaced on the PFD. The G1000 system tunes the ADF receiver (optional) and DME transceiver (optional). 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, ADF, or DME, depending on installed equipment.) AUDIO PANEL & CNS The following ADF/DME information is displayed in the ADF/DME Tuning Window: • Active and standby ADF frequencies • ADF receiver mode • ADF receiver volume FLIGHT MANAGEMENT • 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. HAZARD AVOIDANCE Turning the large FMS Knob moves the selection cursor through the various fields (standby ADF frequency, ADF receiver mode, ADF radio volume, 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. AFCS Active ADF Frequency Standby ADF Frequency ADF Mode ADF Volume ADDITIONAL FEATURES DME Tuning Mode INDEX APPENDICES Figure 4-29 ADF/DME Tuning Window 110 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS SYSTEM OVERVIEW 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 G1000 System does not tune the ADF emergency frequency, 2182.0‑kHz. FLIGHT INSTRUMENTS Tuning an ADF frequency: 1) Press 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. EIS 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. Turn the Small FMS Knob to Enter Data in the Standby ADF Frequency Field AUDIO PANEL & CNS Press the ENT Key to Complete ADF Frequency Entry FLIGHT MANAGEMENT Turn the Large FMS Knob to Move the Cursor to the Next Character Figure 4-30 Entering ADF Standby Frequencies HAZARD AVOIDANCE 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. AFCS 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. ADDITIONAL FEATURES Press the ENT Key to Transfer the ADF Frequencies APPENDICES Figure 4-31 Transferring ADF Frequencies INDEX 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 111 SYSTEM OVERVIEW Selecting ADF Receiver Mode FLIGHT INSTRUMENTS Audio Panel and CNS • ANT (Antenna) – The ADF bearing pointer parks on the HSI at 90 degrees. Best mode for listening to NDB audio. The following modes can be selected: (In all modes NDB audio can be heard by selecting the ADF Key on the Audio Panel.) • ADF (Automatic Direction Finder) – The ADF pointer points to the relative bearing of the NDB station. EIS • 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. AUDIO PANEL & CNS • 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. FLIGHT MANAGEMENT 2) Turn the small FMS Knob to select the desired ADF receiver mode. HAZARD AVOIDANCE Turn the Small FMS Knob to Select the Mode Figure 4-32 Selecting ADF Receiver Mode AFCS ADF receiver volume level can be adjusted in the tuning window from 0 to 100%. The default volume level is set to 50%. The ADF volume level is the same for both Audio Panels. ADDITIONAL FEATURES Adjusting ADF receiver volume: 1) Turn the large FMS Knob to place the selection cursor over the ADF volume field. 2) Turn the small FMS Knob to adjust volume as desired. INDEX APPENDICES Turn the Small FMS Knob to Select the Volume Figure 4-33 Adjusting ADF Receiver Volume 112 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS SYSTEM OVERVIEW DME Tuning NOTE: When turning on the G1000 for use, the system remembers the last frequency used for DME tuning FLIGHT INSTRUMENTS 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. EIS DME Modes AUDIO PANEL & CNS Figure 4-34 ADF/DME Tuning Window, DME Modes The following DME transceiver pairing can be selected: FLIGHT MANAGEMENT • 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. HAZARD AVOIDANCE Selecting DME transceiver pairing: 1) Press 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. AFCS 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. ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 113 SYSTEM OVERVIEW Audio Panel and CNS 4.4 GTX 33 Mode S Transponder FLIGHT INSTRUMENTS The GTX 33 Mode S Transponder provides Mode A, Mode C, and Mode S interrogation and reply capabilities. 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. EIS • Altitude reporting • Airborne status determination AUDIO PANEL & CNS • Transponder capability reporting • Mode S Enhanced Surveillance (EHS) requirements FLIGHT MANAGEMENT • 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 (TAS) to recognize the presence of Mode S-equipped aircraft for selective interrogation. The Hazard Avoidance Section provides more details on traffic avoidance systems. Transponder Controls HAZARD AVOIDANCE 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 pressed, the Mode Selection softkeys appear: STBY, ON, ALT, VFR, CODE, IDENT, BACK. AFCS When the CODE Softkey is pressed, 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. Pressing the numbered softkeys in sequence enters the transponder code. If an error is made, the code selection cursor can be moved back to the left one digit with each press of the BKSP Softkey. ADDITIONAL FEATURES Pressing the BACK Softkey during code selection reverts to the Mode Selection Softkeys. Pressing the BACK Softkey during mode selection reverts to the top-level softkeys. The code can also be entered with the FMS Knob on the PFD. Code entry must be completed with either the softkeys or the FMS Knob, but not a combination of both. APPENDICES Pressing the IDENT Softkey while in Mode or Code Selection initiates the ident function and reverts to the top-level softkeys. INDEX After 45 seconds of transponder softkey inactivity, the system reverts back to the top-level softkeys. 114 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS ALT GND VFR CODE IDENT BACK FLIGHT INSTRUMENTS ON IDENT SYSTEM OVERVIEW STBY XPDR ALERTS Pressing the BACK Softkey returns to the top-level softkeys. 0 1 2 3 4 5 6 7 BKSP IDENT BACK ALERTS EIS Pressing the BACK Softkey returns to the mode selection softkeys. AUDIO PANEL & CNS Figure 4-35 Transponder Softkeys (PFD) Transponder Mode Selection FLIGHT MANAGEMENT Mode selection can be automatic (Ground and Altitude Modes) or manual (Standby, ON, and Altitude Modes). The STBY, ON, and ALT Softkeys can be accessed by pressing the XPDR Softkey. Selecting a transponder mode: HAZARD AVOIDANCE 1) Press the XPDR Softkey to display the Transponder Mode Selection Softkeys. 2) Press the desired softkey to activate the transponder mode. Ground Mode AFCS 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 pressing any one of the Mode Selection Softkeys. A green GND indication and transponder code appear in the mode field of the Transponder Data Box. In 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. ADDITIONAL FEATURES When Standby Mode has been selected on the ground, the transponder can be returned to Ground Mode by pressing the GND Softkey. GND Mode APPENDICES Figure 4-36 Ground Mode INDEX 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 115 SYSTEM OVERVIEW Standby Mode (Manual) FLIGHT INSTRUMENTS Audio Panel and CNS Standby Mode can be selected at any time by pressing 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. NOTE: In Standby Mode, the IDENT function is inoperative. EIS STBY Mode (White Code Number and Mode) AUDIO PANEL & CNS Figure 4-37 Standby Mode Manual ON Mode FLIGHT MANAGEMENT ON Mode can be selected at any time by pressing the ON Softkey. ON Mode generates Mode A and Mode S replies, but 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. HAZARD AVOIDANCE ON Mode (No Altitude Reporting) INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 4-38 ON Mode 116 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 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) EIS Figure 4-39 Altitude Mode AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT Reply to Interrogation HAZARD AVOIDANCE Figure 4-40 Reply Indication AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 117 SYSTEM OVERVIEW Audio Panel and CNS Entering a Transponder Code Entering a transponder code with softkeys: FLIGHT INSTRUMENTS 1) Press the XPDR Softkey to display the Transponder Mode Selection Softkeys. 2) Press the CODE Softkey to display the Transponder Code Selection Softkeys, for digit entry. EIS 3) Press the digit softkeys to enter the code in the code field. When entering the code, the next softkey in sequence must be pressed within 10 seconds, or the entry is cancelled and restored to the previous code. Pressing 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. AUDIO PANEL & CNS Entering a Code Figure 4-41 Entering a Code FLIGHT MANAGEMENT Entering a transponder code with the PFD FMS Knob: 1) Press the XPDR and the CODE Softkeys as in the previous procedure to enable code entry. 2) Turn the small FMS Knob on the PFD to enter the first two code digits. 3) Turn the large FMS Knob to move the cursor to the next code field. HAZARD AVOIDANCE 4) Enter the last two code digits with the small FMS Knob. 5) Press the ENT Key to complete code digit entry. AFCS 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. ADDITIONAL FEATURES 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 INDEX APPENDICES Figure 4-42 Entering a Code with the FMS Knob 118 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS SYSTEM OVERVIEW VFR Code FLIGHT INSTRUMENTS The VFR code can be entered either manually or by pressing the XPDR Softkey, then the VFR Softkey. When the VFR Softkey is pressed, the pre-programmed VFR code is automatically displayed in the code field of the Transponder Data Box. Pressing 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 EIS Figure 4-43 VFR Code AUDIO PANEL & CNS IDENT Function NOTE: In Standby Mode, the IDENT Softkey is inoperative. FLIGHT MANAGEMENT Pressing 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 pressed, a green IDNT indication is displayed in the mode field of the Transponder Data Box for a duration of 18 seconds. HAZARD AVOIDANCE After the IDENT Softkey is pressed while in Mode or Code Selection, the system reverts to the top-level softkeys. IDNT Indication AFCS Press the IDENT Softkey to Initiate the ID Function Figure 4-44 IDENT Softkey and Indication ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 119 SYSTEM OVERVIEW 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 FLIGHT INSTRUMENTS 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 is not to exceed seven 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. EIS Entering a Flight ID: 1) Press the TMR/REF Softkey to display the Timer/References Window. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 5) Press the ENT Key to complete Flight ID entry. AFCS HAZARD AVOIDANCE 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 INDEX APPENDICES ADDITIONAL FEATURES Figure 4-45 Timer/References Window, Entering Flight ID 120 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS SYSTEM OVERVIEW 4.5 Additional Audio Panel Functions Power-up FLIGHT INSTRUMENTS The Audio Panel performs 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. Mono/Stereo Headsets EIS Stereo headsets are recommended for use in this aircraft. AUDIO PANEL & CNS Using a monaural headset in a stereo jack shorts the right headset channel output to ground. While this does not damage the Audio Panel, a person listening on a monaural headset hears only the left channel in both ears. If a monaural headset is used at one of the passenger positions, any other passenger using a stereo headset hears audio in the left ear only. Speaker FLIGHT MANAGEMENT All of the radios can be heard over the cabin speaker. Pressing the SPKR Key selects and deselects the cabin speaker. Speaker audio is muted when the PTT is pressed. Certain aural alerts and warnings (autopilot, traffic, altitude) are always heard on the speaker, even when the speaker is not selected. The speaker volume is adjustable within a nominal range. Contact a Garmin-authorized service center for volume adjustment. HAZARD AVOIDANCE Figure 4-46 Passenger Address and Speaker Keys AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 121 SYSTEM OVERVIEW Audio Panel and CNS Intercom FLIGHT INSTRUMENTS The Audio Panel includes a four-position intercom system (ICS) for the pilot, copilot and up to two passengers. The intercom provides Pilot and Copilot isolation from the passengers and aircraft radios. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS Figure 4-47 Intercom Controls PILOT KEY Annunciator COPLT KEY Annunciator Pilot Hears Copilot Hears Passenger Hears OFF OFF Selected radios, aural alerts, pilot, copilot, passengers Selected radios, aural alerts, pilot, copilot, passengers Selected radios, aural alerts, pilot, copilot, passengers ON OFF Selected radios, aural alerts, pilot Copilot, passengers Copilot, passengers OFF ON Selected radios, aural alerts, pilot; passengers Copilot Selected radios, aural alerts, pilot, passengers ON ON Selected radios, aural alerts, pilot, copilot Selected radios, aural alerts, pilot, copilot Passengers AFCS Table 4-1 ICS Isolation Modes ADDITIONAL FEATURES Pilot isolation is selected when the PILOT Annunciator is illuminated. During Pilot isolation, the pilot can hear the selected radios and aural alerts and warnings. The copilot and passengers can communicate with each other. The copilot is isolated from aural alerts and warnings. Copilot isolation is selected when the COPLT Annunciator is illuminated. The copilot is isolated from the selected radios, aural alerts, and warnings, and everyone else. The pilot and passengers can hear the selected radios, aural alerts, and communicate with each other. APPENDICES When both the PILOT and COPLT Annunciators are illuminated, the pilot and copilot can hear the selected radios, aural alerts, and communicate with each other. The passengers are isolated from the pilot and copilot but can communicate with each other. INDEX When both the PILOT and COPLT Annunciators are extinguished, everyone hears the selected radios, aural alerts, and is able to communicate with everyone else. 122 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS SYSTEM OVERVIEW Intercom Volume and Squelch FLIGHT INSTRUMENTS The PILOT/PASS Knob controls volume or manual squelch adjustment for the pilot and copilot/passenger. The small knob controls the pilot volume and squelch. The large knob controls the copilot/passenger volume and squelch. The VOL and SQ annunciations at the bottom of the unit indicate which function the knob is controlling. Pressing the PILOT/PASS Knob switches between volume and squelch control as indicated by the VOL or SQ annunciation being illuminated. The MAN SQ Key allows either automatic or manual control of the squelch setting. When the MAN SQ Annunciator is extinguished (Automatic Squelch is on), the PILOT/PASS Knob controls only the volume (pressing the PILOT/PASS Knob has no effect on the VOL/SQ selection). EIS When the MAN SQ Annunciator is illuminated (Manual Squelch), the PILOT/PASS Knob controls both volume and squelch. AUDIO PANEL & CNS Manual Squelch Annunciator; Off for Automatic Squelch, On for Manual Squelch Automatic/Manual Squelch FLIGHT MANAGEMENT HAZARD AVOIDANCE Pilot Volume or Manual Squelch. Press to switch between VOL and SQ. Turn to adjust Squelch when SQ Annunciation is lit, Volume when VOL Annunciation is lit. Copilot/Passenger Volume or Manual Squelch Volume Annunciation Squelch Annunciation AFCS Figure 4-48 Volume/Squelch Control ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 123 SYSTEM OVERVIEW Audio Panel and CNS Passenger Address (PA) System FLIGHT INSTRUMENTS A passenger address system is available for delivering voice messages over the cabin speaker. When the PA Key is selected on the Audio Panel, the COM MIC Annunciator is extinguished, and the active COM frequency changes to white, indicating that there is no COM selected. A Push-to-Talk (PTT) must be pressed to deliver PA announcements. The PA Annunciator flashes about once per second while the PTT is depressed. AUDIO PANEL & CNS EIS PA Key is Selected on the Audio Panel Figure 4-49 PA Key Selected for Cabin Announcements FLIGHT MANAGEMENT Clearance Recorder and Player The Audio Panel contains a digital clearance recorder that 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. HAZARD AVOIDANCE The PLAY Key controls the play function. Pressing the PLAY Key once plays the latest recorded memory block. The PLAY Annunciator flashes to indicate when play is in progress. The PLAY Annunciator turns off after the present memory block has finished playing. AFCS Pressing the MKR/MUTE Key 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 while audio is playing begins playing the previously recorded memory block. Each subsequent press of the PLAY Key selects the previously recorded memory block. ADDITIONAL FEATURES Powering off the unit automatically clears all recorded blocks. APPENDICES MKR/MUTE Key Stops Play PLAY Key Controls the Play Function INDEX Figure 4-50 Marker Mute and Play Keys 124 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS SYSTEM OVERVIEW Split COM NOTE: Split COM performance is affected by the distance between the COM antennas and the separation FLIGHT INSTRUMENTS of the tuned frequencies. If the selected COM1 and COM2 frequencies are too close together, interference may be heard during transmission on the other radio. During Split COM operation, both the pilot and the copilot can transmit simultaneously over separate radios. The pilot can still monitor NAV1, NAV2, ADF, DME, and MKR Audio as selected, but the copilot is only able to monitor COM2. EIS Pressing the COM 1/2 Key selects Split COM operation. The COM 1/2 Annunciator is illuminated indicating Split COM operation. COM1 and COM2 frequencies are displayed in green indicating that both transceivers are active. Split COM operation is cancelled by pressing the COM 1/2 Key again, at which time the annunciator is extinguished. AUDIO PANEL & CNS When Split COM operation is selected, COM1 is used by the pilot and COM2 is used by the copilot. The COM1 MIC Annunciator flashes when the pilot’s microphone PTT is pressed. The COM2 MIC Annunciator flashes when the copilot’s microphone PTT is pressed. FLIGHT MANAGEMENT COM1 Radio is Used by the Pilot HAZARD AVOIDANCE AFCS COM2 Radio is Used by the Copilot ADDITIONAL FEATURES Figure 4-51 Split COM Operation Entertainment Inputs APPENDICES 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. INDEX 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 125 SYSTEM OVERVIEW Audio Panel and CNS 4.6 Audio Panel Preflight Procedure FLIGHT INSTRUMENTS 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: When the MAN SQ Key is pressed, the ICS squelch can be set manually by the pilot and copilot. If EIS manual squelch is set to full open (SQ annunciated and the knobs turned counterclockwise) background noise is heard in the ICS system as well as during COM transmissions. AUDIO PANEL & CNS After powering up the G1000 System, the following steps aid in maximizing the use of the Audio Panel as well as preventing 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. FLIGHT MANAGEMENT Automatic/Manual Squelch HAZARD AVOIDANCE Pilot and Copilot ICS Isolation Keys Pilot Volume or Manual Squelch Copilot/Passenger Volume or Manual Squelch Squelch Annunciation AFCS Volume Annunciation ADDITIONAL FEATURES Figure 4-52 Audio Panel Controls Setting the Audio Panel during preflight: 1) Verify that the PILOT and COPLT Annunciators are extinguished. APPENDICES 2) Verify that the MAN SQ Annunciator is extinguished. 3) Turn the PILOT/PASS Knobs 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 PILOT/PASS Knob volume to the desired intercom level. INDEX Once this procedure has been completed, the pilot and copilot can change settings, keeping in mind the notes above. 126 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Audio Panel and CNS SYSTEM OVERVIEW 4.7 Abnormal Operation FLIGHT INSTRUMENTS Abnormal operation of the G1000 includes equipment failures of the G1000 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 pilot of a stuck microphone. EIS The COM1 MIC or COM2 MIC Key Annunciator on the Audio Panel flashes as long as the PTT Key remains stuck. AUDIO PANEL & CNS Figure 4-53 Stuck Microphone Alert FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE Emergency Channel Loaded Automatically Figure 4-54 COM Tuning Failure AFCS Audio Panel Fail-safe Operation ADDITIONAL FEATURES If there is a failure of the Audio Panel, a fail-safe circuit connects the pilot’s headset and microphone directly to the COM1 transceiver. Audio is not available on the speaker. Reversionary Mode APPENDICES The red DISPLAY BACKUP Button selects the Reversionary Mode. See the System Overview Section for more information on Reversionary Mode. INDEX Figure 4-55 Display Backup Button 190-00962-00 Rev B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 127 INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Audio Panel and CNS Blank Page 128 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Section 5 Flight Management FLIGHT INSTRUMENTS 5.1 Introduction The G1000 is an integrated flight, engine, communication, navigation and surveillance system. This section of the Pilot’s Guide explains flight management using the G1000. EIS The most prominent part of the G1000 are the two full color displays: a Primary Flight Display (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 flight management data on the PFD and MFD follows. AUDIO PANEL & CNS 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), Approach (LNAV, LNAV+V, L/VNAV, or LPV), or Missed Approach (MAPR)). FLIGHT MANAGEMENT nOTE: Check the Aircraft Flight Manual (AFM) to determine whether WAAS functionality is approved. HAZARD AVOIDANCE 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. Selecting the INSET Softkey again, then selecting the OFF Softkey removes the Inset Map. AFCS 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). ADDITIONAL FEATURES 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. APPENDICES 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. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 129 SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS Navigation Status Box Navigation Mode Inset Map AUDIO PANEL & CNS EIS Location of: - Direct To Window - Flight Plan Window - Procedures Window - Nearest Airports Window Figure 5-1 GPS Navigation Information on the PFD FLIGHT MANAGEMENT Navigation Status Box Map Orientation Navigation Page Title Navigation Map HAZARD AVOIDANCE - Aviation Data - Geographic Data - Topographic Data - Hazard Data Flight Plan Leg Aircraft Icon at Present Position ADDITIONAL FEATURES AFCS Active Flight Plan Leg Map Range INDEX APPENDICES Figure 5-2 GPS Navigation Information on the MFD Navigation Page 130 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Navigation Status Box The Navigation Status Box located at the top of the PFD contains two fields displaying the following information: FLIGHT INSTRUMENTS PFD Navigation Status Box The Navigation Status Box located at the top of the MFD contains four data fields, each displaying one of the following items: • Distance (DIS) and Bearing (BRG) to the next waypoint or flight plan annunciations (e.g., ‘TOD within 1 minute’) • Bearing (BRG) Symbol Description Active Leg • Distance (DIS) • Desired Track (DTK) AUDIO PANEL & CNS The symbols used in the PFD status bar are: EIS • Active flight plan leg (e.g., ‘D-> KICT’ or ‘KIXD > KCOS’) or flight plan annunciations (e.g., ‘Turn right to 021˚ in 8 seconds’) • Endurance (END) • Enroute Safe Altitude (ESA) Direct-to FLIGHT MANAGEMENT • Estimated Time of Arrival (ETA) • Estimated Time Enroute (ETE) Right Procedure Turn Left Procedure Turn • Fuel over Destination (FOD) • Ground Speed (GS) • Minimum Safe Altitude (MSA) Left Holding Pattern • True Air Speed (TAS) Vector to Final • Track Angle Error (TKE) Left DME Arc • Track (TRK) AFCS Right DME Arc HAZARD AVOIDANCE Right Holding Pattern • Fuel on Board (FOB) • Vertical Speed Required (VSR) • Crosstrack Error (XTK) ADDITIONAL FEATURES MFD Navigation Status Box APPENDICES 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. INDEX 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. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 131 SYSTEM OVERVIEW Flight Management 4) Turn the small FMS Knob to display and scroll through the data options list. 5) Select the desired data. FLIGHT INSTRUMENTS 6) Press the ENT Key. Pressing the DFLTS Softkey returns any field to its default setting. 5.2 Using Map Displays FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS Map displays are used extensively in the G1000 to provide situational awareness in flight. Most G1000 maps can display the following information: • Airports, NAVAIDs, airspaces, airways, land data • Icons for enabled map features (highways, cities, lakes, rivers, borders, etc.) with • Aircraft icon (representing present position) names • Nav range ring • Map Pointer information (distance and bearing to pointer, location of pointer, name, and other pertinent • Flight plan legs information) • User waypoints • Map range • Track vector • Wind direction and speed • Topography scale • Map orientation • Topography data HAZARD AVOIDANCE The information in this section applies to the following maps unless otherwise noted: • All Map Group Pages (MAP) • Flight Plan Pages (FPL) • All Waypoint Group Pages (WPT) • Direct-to Window • AUX - Trip Planning • PFD Inset Map • All Nearest Group Pages (NRST) • Procedure Loading Pages AFCS Map Orientation INDEX APPENDICES ADDITIONAL FEATURES 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 132 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW • 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. • Desired track up (DTK UP) aligns the top of the map display to the desired course. FLIGHT INSTRUMENTS • 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. EIS 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: AUDIO PANEL & CNS Changing the Navigation Map orientation: 1) With the Navigation Map Page displayed, press the MENU Key. The cursor flashes on the ‘Map Setup’ option. FLIGHT MANAGEMENT Map Setup Selection HAZARD AVOIDANCE 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. AFCS Map Group Selection Orientation Field ADDITIONAL FEATURES APPENDICES 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX Figure 5-5 Map Setup Menu Window - Map Group 133 SYSTEM OVERVIEW Flight Management 4) Turn the small FMS Knob to select the desired orientation. 5) Press the ENT Key to select the new orientation. FLIGHT INSTRUMENTS 6) Press the FMS Knob to return to the base page. Map Range AUDIO PANEL & CNS EIS 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 G1000 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. FLIGHT MANAGEMENT Range Overzoom HAZARD AVOIDANCE Figure 5-6 Map Range Auto Zoom AFCS Auto zoom allows the G1000 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). ADDITIONAL FEATURES If a terrain caution or warning occurs, any map page displaying TAWS/TERRAIN data automatically adjusts to the smallest map range clearly showing the highest priority alert. 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. APPENDICES 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 determines the minimum and maximum distance to display based upon the aircraft’s ground speed. INDEX • 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. 134 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW • 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. FLIGHT INSTRUMENTS • 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 this 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. EIS Manual Range Override Expiration Time AUDIO PANEL & CNS Auto Zoom: Off, MFD Only, PFD Only, All On Maximum Look Forward Time Minimum Look Forward Time FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 5-7 Map Setup Menu Window - Map Group, Auto Zoom Configuring automatic zoom: AFCS 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. ADDITIONAL FEATURES 4) Press the ENT Key. 5) Highlight the ‘AUTO ZOOM’ field. 6) Select ‘Off’, ‘MFD Only’, ‘PFD Only’, or ‘ALL On’. APPENDICES 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 ‘MAX LOOK FWD’ (zero to 999 minutes). 10) Press the FMS Knob to return to the Navigation Map Page. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 135 SYSTEM OVERVIEW Flight Management Map Panning Map panning allows the pilot to: FLIGHT INSTRUMENTS • 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 AUDIO PANEL & CNS EIS 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. FLIGHT MANAGEMENT Map Pointer Information AFCS HAZARD AVOIDANCE Map Pointer ADDITIONAL FEATURES 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 INDEX APPENDICES been no pointer movement for about 60 seconds, the map reverts back to centered on the aircraft position and the flashing pointer is removed. 136 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS Information about Point of Interest EIS AUDIO PANEL & CNS Map Pointer on POI FLIGHT MANAGEMENT Figure 5-9 Navigation Map - Map Pointer on Point of Interest HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 137 SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS 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. EIS Information about Airspace FLIGHT MANAGEMENT AUDIO PANEL & CNS Map Pointer on Airspace HAZARD AVOIDANCE 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. INDEX APPENDICES ADDITIONAL FEATURES AFCS 3) Press the Joystick to remove the Map Pointer and recenter the map on the aircraft’s current position. 138 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 3) Press 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. EIS NAVAID Information AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE GO BACK Softkey Figure 5-11 Navigation Map - Information Window - NAVAID AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 139 SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 2) Press the ENT Key to display an options menu. 3) ‘Review Airspace?’ should already be highlighted, if not select it. Press the ENT Key to display the Airspace Information Page for the selected airspace. EIS 4) Press the CLR or ENT Key to exit the Airspace Information Page. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS Airspace Information INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 5-12 Navigation Map - Information Window - Airspace 140 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Measuring Bearing and Distance FLIGHT INSTRUMENTS 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). EIS 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. AUDIO PANEL & CNS 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. Measurement Information FLIGHT MANAGEMENT 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 HAZARD AVOIDANCE Measurement Line AFCS ADDITIONAL FEATURES APPENDICES Figure 5-13 Navigation Map - Measuring Bearing and Distance INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 141 SYSTEM OVERVIEW Flight Management Topography FLIGHT INSTRUMENTS 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 AUDIO PANEL & CNS EIS Navigation Map Black Background TOPO Softkey Not Enabled TOPO Softkey Enabled FLIGHT MANAGEMENT TOPO Off TOPO On Figure 5-14 Navigation Map - Topographic Data Displaying/removing topographic data on all pages displaying navigation maps: HAZARD AVOIDANCE 1) Press the MAP Softkey (the INSET Softkey for the PFD Inset Map). 2) Press the TOPO Softkey. 3) Press 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. AFCS 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. ADDITIONAL FEATURES 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘TOPO DATA’ field. APPENDICES 6) Select ‘On’ or ‘Off’. INDEX 7) Press the FMS Knob to return to the Navigation Map Page. 142 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW FLIGHT INSTRUMENTS TOPO DATA Range EIS TOPO DATA On/Off AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 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). HAZARD AVOIDANCE 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. AFCS 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. ADDITIONAL FEATURES 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. APPENDICES 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 as shown following. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 143 SYSTEM OVERVIEW Flight Management Maximum Displayed Elevation FLIGHT INSTRUMENTS Minimum Displayed Elevation Aircraft Altitude (MSL) Range of Displayed Elevations AUDIO PANEL & CNS EIS Ground Elevation at Map Pointer Location (only visible when Map Pointer is displayed) Figure 5-16 Navigation Map - TOPO SCALE FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 4) Highlight the ‘TOPO SCALE’ field. 5) Select ‘On’ or ‘Off’. ADDITIONAL FEATURES AFCS 6) Press the FMS Knob to return to the Navigation Map Page. APPENDICES TOPO SCALE On/Off INDEX Figure 5-17 Navigation Map Setup Menu - TOPO SCALE Setup 144 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Map Symbols FLIGHT INSTRUMENTS 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 Symbol Default Maximum Range (nm) Range (nm) EIS (Text label size can be None, Small, Medium (Med), or Large (Lrg) Latitude/Longitude (LAT/LON) Off 2000 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 ADDITIONAL FEATURES 800 AFCS 300 HAZARD AVOIDANCE Interstate Highway (FREEWAY) FLIGHT MANAGEMENT AUDIO PANEL & CNS Highways and Roads APPENDICES Table 5-1 Land Symbol Information INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 145 SYSTEM OVERVIEW Flight Management Aviation Symbols The following items are configured on the aviation menu: Aviation Symbols FLIGHT INSTRUMENTS (Text label size can be None, Small, Medium (Med), or Large (Lrg) EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES 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) APPENDICES Symbol See Airports, NAVAIDs See Additional Features N/A INDEX Table 5-2 Aviation Symbol Information 146 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Symbol Setup All pages with maps can display land symbols (roads, lakes, borders, etc). Land symbols can be removed totally (turned off). FLIGHT INSTRUMENTS 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. EIS 3) Highlight the ‘LAND DATA’ field. 4) Select ‘On’ or ‘Off’. 5) Press the FMS Knob to return to the Navigation Map Page. AUDIO PANEL & CNS FLIGHT MANAGEMENT LAND DATA On/Off HAZARD AVOIDANCE Figure 5-18 Navigation Map Setup Menu - TOPO SCALE Setup AFCS 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. ADDITIONAL FEATURES 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. APPENDICES 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. INDEX 6) Select the desired range. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 147 SYSTEM OVERVIEW Flight Management 7) Press the ENT Key to accept the selected range. FLIGHT INSTRUMENTS 8) Press the FMS Knob to return to the Navigation Map Page. AUDIO PANEL & CNS EIS Text Label Size (None, Small Med, or Lrg) Maximum Display Range HAZARD AVOIDANCE FLIGHT MANAGEMENT Figure 5-19 Navigation Map Setup Menu - LAND GROUP Setup Maximum Display Range ADDITIONAL FEATURES AFCS Text Label Size (None, Small Med, or Lrg) APPENDICES 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 INDEX 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). 148 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS Declutter Level EIS DCLTR Softkey Navigation Map Page Menu Figure 5-21 Navigation Map - Declutter Level Indications AUDIO PANEL & CNS Decluttering the map: Press 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: FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 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. AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 149 SYSTEM OVERVIEW Flight Management Table 5-3 lists the items displayed at each declutter level. The ‘X’ represents map items displayed for the various levels of declutter. Item APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Flight Plan Route Lines Flight Plan Route Waypoints Rivers/Lakes Topography Data International Borders Track Vector Navigation Range Ring Fuel Range Ring Terrain Data Traffic Airways NEXRAD XM Lightning Data Airports Runway Labels Restricted MOA (Military) User Waypoints Latitude/Longitude Grid NAVAIDs Class B Airspaces/TMA Class C Airspaces/TCA Class D Airspaces Other Airspaces/ADIZ TFRs Obstacles Land/Country Text Cities Roads Railroads State/Province Boundaries River/Lake Names No Declutter 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 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 X X X X X X X X INDEX Table 5-3 Navigation Map Items Displayed by Declutter Level 150 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Airways FLIGHT INSTRUMENTS 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. EIS 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. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT HAZARD AVOIDANCE Low Altitude Airway (Victor Airway) AFCS ADDITIONAL FEATURES High Altitude Airway (Jet Route) APPENDICES Figure 5-22 Airways on MFD Navigation Page INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 151 SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS Displaying/removing airways: 1) Select the MAP Softkey. 2) Select the AIRWAYS Softkey. Both High and Low Altitude Airways are displayed (AIRWY ON). 3) Select the softkey again to display Low Altitude Airways only (AIRWY LO). EIS 4) Select the softkey again to display High Altitude Airways only (AIRWY HI). 5) Select the softkey again to remove High Altitude Airways. No airways are displayed (AIRWAYS). Or: AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 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 AFCS Figure 5-23 Navigation Map Setup Menu - AIRWAYS Setup The airway range is the maximum map range on which airways are displayed. ADDITIONAL FEATURES 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) Select the ‘Airway’ group. APPENDICES 4) Press the ENT Key. 5) Highlight the ‘LOW ALT AIRWAY’ or ‘HI ALT AIRWAY’ range field. 6) To change the range setting, turn the small FMS Knob to display the range list. 7) Select the desired range using the small FMS Knob. INDEX 8) Press the ENT Key. 9) Press the FMS Knob to return to the Navigation Map Page. 152 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW The following range items are configurable on the airways menu: Airway Type Symbol Low Altitude Airway (LOW ALT AIRWAY) 300 High Altitude Airway (HI ALT AIRWAY) FLIGHT INSTRUMENTS Default Maximum Range (nm) Range (nm) 200 500 500 Table 5-4 Airway Range Information EIS Track Vector AUDIO PANEL & CNS The Navigation Map can display a track vector that is useful in minimizing track angle error. The track vector is a solid light blue 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. FLIGHT MANAGEMENT Track Vector HAZARD AVOIDANCE Figure 5-24 Navigation Map -Track Vector Displaying/removing the track vector: AFCS 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. ADDITIONAL FEATURES 4) Press the ENT Key. 5) Highlight the ‘TRACK VECTOR’ field. APPENDICES 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. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 153 FLIGHT INSTRUMENTS SYSTEM OVERVIEW Flight Management Wind Vector On/Off EIS Nav Range Ring On/Off Track Vector - On/Off - Look Ahead Time AUDIO PANEL & CNS 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 FLIGHT MANAGEMENT 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 HAZARD AVOIDANCE 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 AFCS Information pages. Displaying/removing the wind vector: ADDITIONAL FEATURES 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. APPENDICES 4) Press the ENT Key. 5) Highlight the ‘WIND VECTOR’ field. 6) Select ‘On’ or ‘Off’. INDEX 7) Press the FMS Knob to return to the Navigation Map Page. 154 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 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). FLIGHT INSTRUMENTS Range (radius) EIS AUDIO PANEL & CNS Nav Range Ring FLIGHT MANAGEMENT Figure 5-27 Navigation Map - Nav Range Ring HAZARD AVOIDANCE 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: AFCS 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. ADDITIONAL FEATURES 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘NAV RANGE RING’ field. 6) Select ‘On’ or ‘Off’. APPENDICES 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. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 155 SYSTEM OVERVIEW Flight Management Fuel Range Ring FLIGHT INSTRUMENTS 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. Total Endurance Range AUDIO PANEL & CNS EIS Time to Reserve Fuel FLIGHT MANAGEMENT Range to Reserve Fuel HAZARD AVOIDANCE 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. AFCS 3) Select the ‘Map’ group. 4) Press the ENT Key. ADDITIONAL FEATURES 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. APPENDICES 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. INDEX 10) Press the FMS Knob to return to the Navigation Map Page. 156 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Field of View (SVS) FLIGHT INSTRUMENTS 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. EIS Lateral Field of View Boundaries AUDIO PANEL & CNS Figure 5-29 Navigation Map - Field of View FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘FIELD OF VIEW’ field. 6) Select ‘On’ or ‘Off’. AFCS 7) Press the ENT Key. 8) Press the FMS Knob to return to the Navigation Map Page. ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 157 SYSTEM OVERVIEW Flight Management 5.3 Waypoints FLIGHT INSTRUMENTS 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 CNS and Audio Panel section for details on autotuning. AUDIO PANEL & CNS EIS 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 in the G1000. As a waypoint identifier, facility name, or location is entered, the G1000’s 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 FLIGHT MANAGEMENT City Entry Field Facility Entry Field Entered Waypoint on Map Map Area Showing Entered Waypoint HAZARD AVOIDANCE - Waypoint Identifier - Type (symbol) - Facility Name - City ADDITIONAL FEATURES AFCS Waypoint Location APPENDICES Figure 5-30 Waypoint Information Window INDEX 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. 158 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Identifier with Duplicates FLIGHT INSTRUMENTS Duplicate Waypoints EIS AUDIO PANEL & CNS Duplicate Message FLIGHT MANAGEMENT Airports Figure 5-31 Waypoint Information Window - Duplicate Identifier HAZARD AVOIDANCE 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. AFCS 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. ADDITIONAL FEATURES 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. APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 159 SYSTEM OVERVIEW Flight Management Airport Information - ID/Facility/City - Usage Type/Region - Lat/Long/Elev - Fuel Available - Time Zone (UTC Offset) FLIGHT INSTRUMENTS Navigation Map Showing Selected Airport Runway Information EIS - Designation - Length/Width/Surface - Lighting Available COM/NAV Freq. Info. Airport/Runway Diagram AUDIO PANEL & CNS - Identification - Frequency - Availability - Additional Information FLIGHT MANAGEMENT Softkeys Figure 5-32 Airport Information Page The following descriptions and abbreviations are used on the Airport Information Page: HAZARD AVOIDANCE • Usage type: Public, Military, or Private • 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) AFCS • COM Availability: TX (transmit only), RX (receive only), PT (part time), i (additional information available) Selecting an airport for review by identifier, facility name, or location: 1) From the Airport Information Page, press the FMS Knob. ADDITIONAL FEATURES 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. APPENDICES 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. INDEX 4) To remove the flashing cursor, press the FMS Knob. 160 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW View a destination airport: From the Airport Information Page press the MENU Key. Select ‘View Destination Airport’. The Destination Airport is displayed. Navigation Frequencies ILS LOC EIS AUDIO PANEL & CNS 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 FLIGHT INSTRUMENTS The Airport Frequencies Box uses the descriptions and abbreviations listed in the following table: FLIGHT MANAGEMENT * May include Additional Information Table 5-5 Airport Frequency Abbreviations HAZARD AVOIDANCE 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 G1000 provides a NRST Softkey on the PFD, which gives the pilot quick access to nearest airport information (very useful if an immediate need to land is required). The Nearest Airports Window displays a list of 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. Airport Identifier/ Type AFCS Bearing/Distance to Airport Approach Available ADDITIONAL FEATURES Length of Longest Runway COM Freq. Info. - Identification - Frequency APPENDICES Additional Airports (within 200 nm) INDEX NRST Softkey Figure 5-33 Nearest Airports Window on PFD 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 161 SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS 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 EIS Airport Information - Usage/Time/Elev - Region Airport Information AUDIO PANEL & CNS - Lat/Long FLIGHT MANAGEMENT Figure 5-34 Airport Information Window on PFD HAZARD AVOIDANCE 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’. INDEX APPENDICES ADDITIONAL FEATURES AFCS 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 five 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. 162 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Nearest Airports - ID/Type - Bearing/Distance FLIGHT INSTRUMENTS Airport Information - Facility/City/Elevation Runway Information Nearest Airport - Designation/Surface - Length/Width EIS COM/NAV Freq. Info. - Identification - Frequency Navigation Map Showing Nearest Airport Window Selection Softkeys AUDIO PANEL & CNS Approaches Available FLIGHT MANAGEMENT LD APR Softkey (only available if an approach is highlighted) Figure 5-35 Nearest Airport Page Viewing information for a nearest airport on the PFD: HAZARD AVOIDANCE 1) Press the NRST Softkey to display the Nearest Airports Window. 2) Highlight the airport identifier with the FMS Knob and press the ENT Key to display the Airport Information Window. AFCS 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 to close the PFD Nearest Airports Window. ADDITIONAL FEATURES 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. APPENDICES 3) Press 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) 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX 5) Press the FMS Knob to remove the flashing cursor. 163 SYSTEM OVERVIEW Viewing runway information for a specific airport: FLIGHT INSTRUMENTS Flight Management 2) Turn the small FMS Knob to select the desired runway. 1) With the Nearest Airports Page displayed, press 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. 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. EIS 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. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 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. AFCS 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. APPENDICES ADDITIONAL FEATURES 5) Press the FMS Knob to remove the flashing cursor. Nearest Airport Criteria INDEX - Type of Runway Surface - Minimum Runway Length Figure 5-36 System Setup Page - Nearest Airport Selection Criteria 164 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Intersections Note: The VOR displayed on the Intersection Information Page is the nearest VOR, not necessarily the VOR FLIGHT INSTRUMENTS 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’. Navigation Map Showing Selected Intersection EIS Intersection Identifier Intersection Info AUDIO PANEL & CNS - Region - Lat/Long Nearest VOR Info - Identifier/Type (symbol) - Radial to VOR - Distance to VOR Selected Intersection FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 5-37 Intersection Information Page AFCS Select an intersection: 1) With the Intersection Information Page displayed, enter an identifier in the Intersection Box. 2) Press the ENT Key. ADDITIONAL FEATURES 3) Press the FMS Knob to remove the flashing cursor. Or: 1) With the Nearest Intersections Page displayed, press the FMS Knob APPENDICES 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. 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’. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 165 SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS The selected intersection is indicated by a white arrow. Up to eleven 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 AUDIO PANEL & CNS EIS Navigation Map Showing Nearest Intersection Intersection Lat/Long FLIGHT MANAGEMENT Reference VOR Info - Identifier/Type (symbol) - VOR Frequency - Bearing/Distance to VOR HAZARD AVOIDANCE Nearest Intersection INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 5-38 Nearest Intersections Page 166 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW NDBs FLIGHT INSTRUMENTS 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 Navigation Map Showing Selected NDB NDB Information EIS - Type - Region - Lat/Long AUDIO PANEL & CNS NDB Frequency Selected NDB Nearest Airport Info - Identifier/Type (symbol) - Bearing/Distance to Airport FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 5-39 NDB Information Page Note: Compass locator (LOM): 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. AFCS Select an NDB: ADDITIONAL FEATURES 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: APPENDICES 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. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 167 SYSTEM OVERVIEW 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’. FLIGHT INSTRUMENTS A white arrow before the NDB identifier indicates the selected NDB. Up to eleven 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 AUDIO PANEL & CNS EIS Navigation Map Showing Selected NDB Nearest NDB FLIGHT MANAGEMENT NDB Information - Facility Name/City - Type - Lat/Long HAZARD AVOIDANCE NDB Frequency INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 5-40 Nearest NDB Page 168 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW VORs FLIGHT INSTRUMENTS 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’s 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’. EIS VOR Identifier/Type - Facility Name - Nearest City AUDIO PANEL & CNS Navigation Map Showing Selected VOR VOR Information - Class/Magnetic Variation - Region - Lat/Long FLIGHT MANAGEMENT VOR Frequency Selected VOR Nearest Airport Info - Identifier/Type (symbol) - Bearing/Distance to Airport HAZARD AVOIDANCE Figure 5-41 VOR Information Page AFCS The VOR classes used in the VOR information box are: LOW ALTITUDE, HIGH ALTITUDE, and TERMINAL Select a VOR: ADDITIONAL FEATURES 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. APPENDICES 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. 190-00962-00 Rev. B INDEX 3) Press the FMS Knob to remove the flashing cursor. Or: Garmin G1000 Pilot’s Guide for the Diamond DA42NG 169 SYSTEM OVERVIEW Flight Management 1) With the Nearest VOR Page displayed, press the MENU Key. 2) Highlight ‘SELECT VOR WINDOW’, and press the ENT Key. FLIGHT INSTRUMENTS 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. EIS 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. AUDIO PANEL & CNS A white arrow before the VOR identifier indicates the selected VOR. Up to eleven 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 HAZARD AVOIDANCE FLIGHT MANAGEMENT Navigation Map Showing Nearest VOR VOR Information AFCS - Facility Name/City - Class/Magnetic Variation - Lat/Long VOR Frequency ADDITIONAL FEATURES Nearest VOR INDEX APPENDICES Figure 5-42 Nearest VOR Page 170 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW User Waypoints FLIGHT INSTRUMENTS The G1000 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 or bearing from two existing waypoints. Once a waypoint has been created, it can be renamed, deleted, or moved. User Wpt Identifier EIS User Wpt Comment Navigation Map Showing Selected User Waypoint User Wpt Info AUDIO PANEL & CNS - Region - Lat/Long Reference Wpt Info - Identifier - Radial/Distance Selected User Waypoint User Waypoint List FLIGHT MANAGEMENT - Identifier - Comment # User Wpts Used Softkeys HAZARD AVOIDANCE Displayed if User Wpt was created on map page Figure 5-43 User Waypoint Information Page AFCS Select 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. ADDITIONAL FEATURES 2) Press the ENT Key. 3) Press the FMS Knob to remove the flashing cursor. Or: 1) With the Nearest User Waypoint Page displayed, press the FMS Knob APPENDICES 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. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 171 SYSTEM OVERVIEW Flight Management Nearest User Wpt List - Identifier - Bearing/Distance from aircraft position FLIGHT INSTRUMENTS Navigation Map Showing Selected User Waypoint EIS User Waypoint Info - Comment - Lat/Long Reference Wpt Info AUDIO PANEL & CNS Selected User Waypoint - Identifier - Radial/Distance FLIGHT MANAGEMENT Figure 5-44 Nearest User Waypoint Page Creating User Waypoints User waypoints can be created from the User Waypoint Information Page in the following ways: HAZARD AVOIDANCE 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. AFCS 4) If desired, highlight the Information Box and enter the latitude and longitude for the waypoint or highlight the Reference Waypoints Box to enter a bearing and distance from another waypoint or the bearing from two other waypoints to define the new waypoint location. ADDITIONAL FEATURES Or: 1) Press the FMS Knob to activate the cursor. 2) Enter a user waypoint name (up to six characters). APPENDICES 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. INDEX 5) Highlight the Information Box and enter the latitude and longitude for the waypoint or highlight the Reference Waypoints Box to enter a bearing and distance from another waypoint or the bearing from two other waypoints to define the new waypoint location. 6) Press the ENT Key to accept the new waypoint. 7) Press the FMS Knob to remove the flashing cursor. 172 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS Figure 5-45 User Waypoint Information Page Menu AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 3) Enter a user waypoint name (up to six characters). 4) Press the ENT Key to accept the selected name. The first reference waypoint box is highlighted. AFCS 5) If desired, highlight the Information Box and enter the latitude and longitude for the waypoint or highlight the Reference Waypoints Box to enter a bearing and distance from another waypoint or the bearing from two other waypoints to define the new waypoint location. 6) Press the FMS Knob to remove the flashing cursor. 7) Press the GO BACK Softkey to return to the map page. ADDITIONAL FEATURES 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. APPENDICES 2) Move the cursor to the desired field. 3) Turn the small FMS Knob to make any changes. 4) Press the ENT Key to accept the changes. 5) Press the FMS Knob to remove the flashing cursor. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 173 SYSTEM OVERVIEW Renaming user waypoints: FLIGHT INSTRUMENTS Flight Management 2) Enter a new name. 1) Highlight a user waypoint in the User Waypoint List. Press the RENAME Softkey, or press the MENU Key and select ‘Rename User Waypoint’ 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. EIS 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. AUDIO PANEL & CNS 2) Press the MENU Key. 3) Select ‘Use Present Position’. 4) Press the ENT Key twice. The new waypoint’s location is saved. FLIGHT MANAGEMENT 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: HAZARD AVOIDANCE 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. AFCS 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. ADDITIONAL FEATURES 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 INDEX APPENDICES 4) Press the FMS Knob to remove the flashing cursor and return to the User Waypoint Information Page. 174 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Deleting User Waypoints Deleting a single user waypoint FLIGHT INSTRUMENTS 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: EIS 1) Highlight a User Waypoint in the User Waypoint List, or enter a waypoint in the User Waypoint field. 2) Press the MENU Key. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 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’ HAZARD AVOIDANCE 4) Press the ENT Key twice to confirm the selection. 5) Press the FMS Knob to remove the flashing cursor. AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 175 SYSTEM OVERVIEW Flight Management 5.4 Airspaces FLIGHT INSTRUMENTS The G1000 can display the following types of airspaces: Class B/TMA, Class C/TCA, Class D, Restricted, MOA (Military), Other Airspace, Air Defense Interdiction Zone (ADIZ), and Temporary Flight Restriction (TFR). Class D Airspace EIS MOA (Military) Class B Airspace HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS Restricted Area Alert Area AFCS Class C Airspace ADDITIONAL FEATURES ADIZ APPENDICES Warning Area Figure 5-46 Airspaces INDEX 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. 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 176 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Navigation Map Page. It simply turns on/off the warning provided when the aircraft is approaching or near an airspace. FLIGHT INSTRUMENTS 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. EIS 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. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 5) Press the FMS Knob to remove the flashing cursor. AFCS Airspace Alerts Box - Airspace Altitude Buffer - Alert On/Off (Default Settings Shown) ADDITIONAL FEATURES APPENDICES DFLTS Softkey Figure 5-47 System Setup Page - Airspace Alerts INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 177 SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 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’. EIS Airspace Alerts Info AUDIO PANEL & CNS - Name - Proximity (Ahead, Inside, Ahead < 2nm, Within 2nm) - Time till Intercept (only if Ahead or Ahead < 2nm) Airspace 1 Airspace/Agency Info - Airspace Type - Controlling Agency FLIGHT MANAGEMENT Airspace Vertical Limits - Ceiling - Floor Airspace 2 Associated Frequencies HAZARD AVOIDANCE - Type - Availability/Info - Frequency Softkeys Figure 5-48 Nearest Airspaces Page AFCS 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. ADDITIONAL FEATURES Selecting and viewing an airspace alert with its associated information: 1) Select the Nearest Airspace Page. APPENDICES 2) Press 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. INDEX 4) Press the FMS Knob to remove the flashing cursor. 178 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Pressing the PFD ALERTS Softkey displays the message window on the PFD. The following airspace alerts are displayed in the message window: Comments The aircraft is inside the airspace. FLIGHT INSTRUMENTS 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. EIS 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. Table 5-6 PFD Airspace Alert Messages AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 179 SYSTEM OVERVIEW Flight Management 5.5 Direct-to-Navigation FLIGHT INSTRUMENTS 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 G1000 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. EIS 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. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT Direct-to Point Info - Identifier/Symbol/Region - Facility Name - City VNV Constraints - Altitude at Arrival - Along Track Offset HAZARD AVOIDANCE Map of Selected Point Location of Destination - Bearing/Distance AFCS Desired Course ADDITIONAL FEATURES Figure 5-49 Direct-to Window - MFD APPENDICES Direct-to Point Info - Identifier/Symbol/City - Facility Name VNV Constraints - Altitude at Arrival - Along Track Offset Direct-to Point Info INDEX - Bearing/Distance - Desired Course Activation Command Figure 5-50 Direct-to Window - PFD 180 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 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: FLIGHT INSTRUMENTS 1) Press the Direct-to Key. The Direct-to Window is displayed (with the active flight plan wayoint as the default selection or a blank waypoint field if no flight plan is active). EIS 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. AUDIO PANEL & CNS 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 MANAGEMENT - Flight Plan Waypoints - Nearest Waypoints - Recent Waypoints - User Waypoints - Airway Waypoints (only available when active leg is part of an airway) HAZARD AVOIDANCE Figure 5-51 Waypoint Submenu Selecting an active flight plan waypoint as a direct-to destination: AFCS 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. ADDITIONAL FEATURES 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. APPENDICES 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. INDEX 4) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 5) Press the ENT Key again to activate the direct-to. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 181 SYSTEM OVERVIEW Flight Management Any NRST, RECENT, USER, or AIRWAY waypoint can be selected as a direct-to destination in the Direct-to Window. FLIGHT INSTRUMENTS 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 EIS 4) Turn the large FMS Knob clockwise to select the desired waypoint. 5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. AUDIO PANEL & CNS 6) Press the ENT Key again to activate the direct-to. FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 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 ENT again to activate the direct-to. Selecting a nearby airport as a direct-to destination: AFCS 1) Press the NRST Softkey on the PFD; or turn the FMS Knob to display the Nearest Airports Page. 2) Select the desired airport (the nearest one is already selected). ADDITIONAL FEATURES 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. APPENDICES 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. INDEX 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. 182 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 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: FLIGHT INSTRUMENTS 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 G1000 resumes navigating the flight plan along the closest leg. EIS Page Menu AUDIO PANEL & CNS - Cancel Direct-To Navigation FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 5-52 Direct-to Window - Cancelling Direct-to Navigation AFCS When navigating a direct-to, the G1000 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. ADDITIONAL FEATURES 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. APPENDICES 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: INDEX 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. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 183 SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS 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 directto destination are removed from the active flight plan upon successful activation of a direct-to destination that is part of the active flight plan. 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. Entering a VNV altitude and along-track offset for the waypoint: 1) Press the Direct-to Key to display the Direct-to Window. EIS 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. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 8) Press the ENT Key. The ‘Activate?’ field is highlighted. 9) Press the ENT Key to activate. Removing a VNV altitude constraint: HAZARD AVOIDANCE 1) Press the Direct-to Key to display the Direct-to Window. 2) Press the MENU Key. AFCS 3) With ‘Clear Vertical Constraints’ highlighted, press the ENT Key. Page Menu INDEX APPENDICES ADDITIONAL FEATURES - Clear Vertical Navigation Constraints Figure 5-53 Direct-to Window - Clearing Vertical Constraints 184 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 5.6 Flight Planning Flight Plan Leg Type FLIGHT INSTRUMENTS Flight planning on the G1000 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 G1000 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). Symbol EIS Active non-heading Leg Active heading Leg AUDIO PANEL & CNS Non-heading Leg in the current flight segment Heading Leg not in the current flight segment FLIGHT MANAGEMENT Non-heading leg not in the active flight segment Turn Anticipation Arc HAZARD AVOIDANCE Table 5-7 Flight Plan Leg Symbols AFCS 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 G1000 uses the waypoint information from the current database to define the waypoints. If the database is changed or updated, the G1000 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 System Messages) advising that one or more stored flight plans need to be edited. ADDITIONAL FEATURES APPENDICES 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. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX 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 re-loads 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 System Messages). 185 SYSTEM OVERVIEW Flight Management The following could cause the airway update to fail: • Airway identifier, entry waypoint or exit waypoint not found in the new database. FLIGHT INSTRUMENTS • 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: EIS • 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) AUDIO PANEL & CNS • Flight Plan Catalog Page on the MFD (create/modify a stored flight plan) FLIGHT MANAGEMENT Active FPL Waypoint List - Comment - Procedure Header - Waypoint Identifier - Airway Identifier - Desired Track to Waypoint - Distance to Waypoint - Waypoint Altitude Constraint HAZARD AVOIDANCE Active Flight Plan Leg Turn Anticipation Arc Vertical Navigation Profile - Active Vertical WPT Alt/ID - Vertical Speed Target - Flight Path Angle - Vertical Speed Target - Time to Top of Descent - Vertical Deviation AFCS Non-Active, Flight Plan Leg INDEX APPENDICES ADDITIONAL FEATURES Figure 5-54 Active Flight Plan Page 186 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Active Flight Plan Comment FLIGHT INSTRUMENTS Active Flight Plan Leg Active Flight Plan Waypoint List - Waypoint ID - Desired Track to Waypoint - Distance to Waypoint - Airway Identifier EIS Figure 5-55 Active Flight Plan Window on PFD AUDIO PANEL & CNS Catalog Contents - # Used - # Empty FLIGHT MANAGEMENT Flight Plan List - Comment HAZARD AVOIDANCE Selected Flight Plan Map Selected FPL Info AFCS - Departure Waypoint - Destination Waypoint - Total Flight Plan Distance - Enroute Safe Altitude Softkeys Figure 5-56 Flight Plan Catalog Page ADDITIONAL FEATURES 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 G1000 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). APPENDICES Creating an active flight plan: 1) Press the FPL Key. 2) Press the FMS Knob to activate the cursor (only on MFD). 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX 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, or airway waypoints). 187 SYSTEM OVERVIEW 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. 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. FLIGHT INSTRUMENTS 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. EIS 3) Press 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. AUDIO PANEL & CNS 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, 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. FLIGHT MANAGEMENT 6) Repeat step numbers 4 and 5 to enter each additional flight plan waypoint. INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE 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. 188 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Adding Waypoints to an Existing Flight Plan FLIGHT INSTRUMENTS 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 EIS - Memory Slot - Comment - Procedure Identifier - Waypoint Identifier - Airway Identifier - Desired Track to Waypoint - Distance to Waypoint - Waypoint Altitude Constraint AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Softkeys Figure 5-57 Stored Flight Plan Page AFCS ADDITIONAL FEATURES Flight Plan Full Message APPENDICES Figure 5-58 Active Flight Plan Page - FPL Full INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 189 SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 2) Highlight the desired flight plan. 3) Press 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. EIS 5) Enter the identifier, facility, or city of the new waypoint. 6) 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 AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS Window is displayed. Use the FMS Knob to select the correct waypoint. Figure 5-59 Duplicate Waypoints Window ADDITIONAL FEATURES 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). APPENDICES 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, or airway waypoints). INDEX 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. The active flight plan is modified as each waypoint is entered. 190 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 2) Press 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 EIS 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 G1000 also anticipates the desired airway and exit point based on loaded flight plan waypoints. AUDIO PANEL & CNS Airway Entry Waypoint FLIGHT MANAGEMENT Selected Airway Airways Available at TOP Airway Waypoint Sequence HAZARD AVOIDANCE Preview of Selected Airway AFCS ADDITIONAL FEATURES Figure 5-60 Select Airway Page - Selecting Airway Adding an airway to a flight plan: 1) Press the FPL Key. APPENDICES 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. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX 4) Turn the small FMS Knob one click clockwise and press 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). 191 SYSTEM OVERVIEW Flight Management 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. FLIGHT INSTRUMENTS 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 EIS Selected Airway Selected Exit Point AUDIO PANEL & CNS Preview of Selected Airway Selected Airway Exit Point HAZARD AVOIDANCE FLIGHT MANAGEMENT Airway Exit Points Available ADDITIONAL FEATURES AFCS Figure 5-61 Select Airway Page - Selecting Exit Point Inserted Airway Header INDEX APPENDICES - Airway Identifier: [airway identifier].[exit waypoint identifier] (e.g., V4.SLN) Figure 5-62 Active Flight Plan Page - Airway Inserted 192 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 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. EIS In the US, airways that are “one-way” for specified hours of operation are not uncommon. These airways are always bidirectional in the G1000 database. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 193 SYSTEM OVERVIEW Flight Management Adding Procedures to a Stored Flight Plan FLIGHT INSTRUMENTS The G1000 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. EIS Flight Plan Name AUDIO PANEL & CNS Flight Plan Waypoint List FLIGHT MANAGEMENT Softkeys Load Departure Load Arrival Load Approach Activate Flight Plan - INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Figure 5-63 Stored Flight Plan Page 194 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Departure (DP) FLIGHT INSTRUMENTS 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 EIS Selected Departure Departures Available at KMCI AUDIO PANEL & CNS Preview of Selected Departure Departure Waypoint Sequence FLIGHT MANAGEMENT Figure 5-64 Departure Loading Page - Selecting the Departure HAZARD AVOIDANCE Loading a departure procedure into a stored flight plan: 1) Select a stored flight plan from the Flight Plan Catalog Page. AFCS 2) Press 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) Press the LD DP Softkey; or press the MENU Key, select “Load Departure”, and press the ENT Key. The Departure Loading Page is displayed. ADDITIONAL FEATURES 4) Select a departure. Press the ENT Key. 5) Select a transition for the selected departure. Press the ENT Key. 6) Select a runway served by the selected departure, if required. Press the ENT Key. APPENDICES 7) Press the ENT Key to load the selected departure procedure. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 195 SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS Departure Airport Selected Departure Selected Runway AUDIO PANEL & CNS EIS Preview of Selected Departure Selected Departure End Point Selected Transition Departure Transition Points Available FLIGHT MANAGEMENT Figure 5-65 Departure Loading Page - Selecting Transition HAZARD AVOIDANCE Inserted Departure Header APPENDICES ADDITIONAL FEATURES AFCS - Departure Identifier: [departure airport]-[departure runway]. [departure transition]. [departure end point] (e.g., KMKC-ALL.WLDCT2.SLN) INDEX Figure 5-66 Stored Flight Plan Page - Departure Inserted 196 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Arrival (STAR) FLIGHT INSTRUMENTS 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 EIS Selected Arrival Arrivals Available at KCOS AUDIO PANEL & CNS Selected Runway Arrival Waypoint Sequence Preview of Selected Arrival FLIGHT MANAGEMENT Figure 5-67 Arrival Loading Page - Selecting the Arrival HAZARD AVOIDANCE Loading an arrival procedure into a stored flight plan: 1) Select a stored flight plan from the Flight Plan Catalog Page. AFCS 2) Press 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) Press the LD STAR Softkey; or press the MENU Key, select “Load Arrival”, and press the ENT Key. The Arrival Loading Page is displayed. ADDITIONAL FEATURES 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. APPENDICES 7) Press the ENT Key to load the selected arrival procedure. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 197 SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS Destination Airport Selected Arrival Selected Transition Transitions Available with DBRY1 Arrival Waypoint Sequence AUDIO PANEL & CNS EIS Preview of Selected Arrival FLIGHT MANAGEMENT Figure 5-68 Arrival Loading Page - Selecting the Transition HAZARD AVOIDANCE Inserted Arrival Header APPENDICES ADDITIONAL FEATURES AFCS - Arrival Identifier: [arrival airport]-[arrival transition]. [arrival].[arrival runway] (e.g., KCOS-TBE.DBRY1.ALL) INDEX Figure 5-69 Stored Flight Plan Page - Arrival Inserted 198 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Approach (APPR) FLIGHT INSTRUMENTS 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 EIS Selected Approach Approaches Available at KCOS AUDIO PANEL & CNS Barometric Minimums Preview of Selected Approach Approach Waypoint Sequence FLIGHT MANAGEMENT Figure 5-70 Approach Loading Page - Selecting the Approach HAZARD AVOIDANCE Loading an approach procedure into a stored flight plan: 1) Select a stored flight plan from the Flight Plan Catalog Page. AFCS 2) Press 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) Press the LD APR Softkey; or press the MENU Key, select “Load Approach”, and press the ENT Key. The Approach Loading Page is displayed. ADDITIONAL FEATURES 4) Select an approach. Press the ENT Key. 5) Select a transition for the selected approach. Press the ENT Key. 6) Press the ENT Key to load the selected approval procedure. APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 199 SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS Destination Airport Selected Approach Selected Transition Barometric Minimums Transitions Available with Selected Approach AUDIO PANEL & CNS EIS Preview of Selected Approach Approach Waypoint Sequence Load Approach? HAZARD AVOIDANCE FLIGHT MANAGEMENT Figure 5-71 Approach Loading Page - Selecting the Transition Inserted Approach Header ADDITIONAL FEATURES AFCS - Approach Identifier: [approach airport].[runway and approach type] (e.g., KCOS-RNAV 35RGPS LPV) INDEX APPENDICES Figure 5-72 Stored Flight Plan Page - Approach Inserted 200 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Flight Plan Storage FLIGHT INSTRUMENTS The G1000 can store up to 99 flight plans, numbered 1 through 99. The active flight plan is erased when the G1000 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. EIS 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. AUDIO PANEL & CNS 5) Press 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 MANAGEMENT Flight Plan Name (Comment) Preview of Selected Flight Plan Selected Flight Plan HAZARD AVOIDANCE Stored Flight Plan Info AFCS - Departure Airport - Destination Airport - Total Flight Plan Distance - Enroute Safe Altitude ADDITIONAL FEATURES Stored FPL Editing Softkeys Figure 5-73 Stored Flight Plan Information Storing an active flight plan from the Active Flight Plan Page or the Active Flight Plan Window: APPENDICES 1) Press the MENU Key. 2) Highlight ‘Store Flight Plan’. 3) Press the ENT Key. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX 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. 201 SYSTEM OVERVIEW Flight Management Sort Flight Plans FLIGHT INSTRUMENTS The stored flight plans can be sorted alphanumerically based on the flight plan name (comment) assigned to each flight plan. Sorting by comment (flight plan name): 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 ‘Sort By Comment’ and press the ENT Key. A confirmation window is displayed. EIS 4 ) With ‘OK’ highlighted, press the ENT Key to change flight plan ordering. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. AUDIO PANEL & CNS 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 and activates it. FLIGHT MANAGEMENT 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. HAZARD AVOIDANCE Activating a stored flight plan on the MFD: 4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. 2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan. 3) Press the ACTIVE Softkey; or press the MENU Key, highlight ‘Activate Flight Plan’, and press the ENT Key. The ‘Activate Stored Flight Plan?’ window is displayed. 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. AFCS 2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan. 3) Press 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. ADDITIONAL FEATURES 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 APPENDICES The G1000 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: INDEX 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. 202 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 3) Press 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. FLIGHT INSTRUMENTS 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 the G1000 memory. Deleting a stored flight plan: EIS 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. AUDIO PANEL & CNS 3) Press 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. FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 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 AFCS 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 ADDITIONAL FEATURES The G1000 allows deleting an active flight plan. Deleting the active flight plan suspends navigation by the G1000. 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). APPENDICES 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. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 203 SYSTEM OVERVIEW Flight Management Deleting Flight Plan Items FLIGHT INSTRUMENTS 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). EIS 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. AUDIO PANEL & CNS 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: FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 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: AFCS 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. ADDITIONAL FEATURES 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. APPENDICES 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. INDEX 4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. 204 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the flight plan to be edited. 4) Press 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. EIS 6) Press the CLR Key. The ‘Remove XXXXX?’ 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. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 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) Press the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored Flight Plan Page is displayed. HAZARD AVOIDANCE 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. AFCS Deleting an entire procedure from a stored flight plan: 1) Press the FPL Key to display the Active Flight Plan Page. ADDITIONAL FEATURES 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) Press the EDIT Softkey; or press the MENU Key, select ‘Edit Flight Plan’ and press the ENT Key. The Stored Flight Plan Page is displayed. APPENDICES 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. 190-00962-00 Rev. B INDEX 8) Press the FMS Knob to remove the flashing cursor. Or: Garmin G1000 Pilot’s Guide for the Diamond DA42NG 205 SYSTEM OVERVIEW Flight Management 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. FLIGHT INSTRUMENTS 3) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the flight plan to be edited. 4) Press 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. EIS 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. AUDIO PANEL & CNS Changing Flight Plan Comments (Names) The comment field (or name) of each flight plan can be changed to something that is useful for identification and sorting. FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 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: AFCS 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. ADDITIONAL FEATURES 4) Press 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. APPENDICES 7) Press the ENT Key to accept the changes. 8) Press the FMS Knob to remove the flashing cursor. Along Track Offsets INDEX 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 206 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW entered from 1 to 99 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. FLIGHT INSTRUMENTS 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. EIS 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. AUDIO PANEL & CNS FLIGHT MANAGEMENT Along Track Offset Waypoint and Distance from Flight Plan Waypoint Along Track Offset Waypoint and Distance HAZARD AVOIDANCE AFCS Figure 5-74 Along Track Offset ADDITIONAL FEATURES 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. APPENDICES 3) Press the ATK OFST Softkey (MFD only); or press the MENU Key, highlight ‘Create ATK Offset Waypoint’, and press the ENT Key. 4) Enter a positive or negative offset distance in the range of +/- 1 to 99 nm (limited by leg distances). 5) Press the ENT Key to create the offset waypoint. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX 6) Press the FMS Knob to remove the flashing cursor. 207 SYSTEM OVERVIEW Flight Management Parallel Track FLIGHT INSTRUMENTS 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. AUDIO PANEL & CNS EIS Note: Vertical navigation is unavailable while the Parallel Track feature is active. Selecting Parallel Track HAZARD AVOIDANCE FLIGHT MANAGEMENT Active Flight Plan prior to Parallel Track Figure 5-75 Active Flight Plan Window - Selecting Parallel Track AFCS Activating parallel track: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD) ADDITIONAL FEATURES 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. APPENDICES 4) Turn the small FMS Knob to enter a distance from 1-99 nm and press the ENT Key. ‘ACTIVATE PARALLEL TRACK’ is highlighted. INDEX 5) Press the ENT Key to activate parallel track. Press the FMS Knob or the CLR Key to cancel the parallel track activation. 208 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Offset Direction Offset Distance FLIGHT INSTRUMENTS Activation Prompt EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-76 Parallel Track Window HAZARD AVOIDANCE Parallel Track Waypoints Parallel Track Original Track AFCS - TIFTO-p - TOP-p - SLN-p - HYS-p - LAA-p Activating Parallel Track affects the entire active flight segment (e.g., enroute) ADDITIONAL FEATURES APPENDICES Figure 5-77 Parallel Track Active INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 209 SYSTEM OVERVIEW Flight Management EIS FLIGHT INSTRUMENTS 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. Subdued Prompt AUDIO PANEL & CNS (Unavailable) Unavailable Status Approach Active FLIGHT MANAGEMENT Invalid Geometry HAZARD AVOIDANCE Figure 5-78 Parallel Track Unavailable AFCS 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) ADDITIONAL FEATURES Cancel Prompt APPENDICES Active Status INDEX Figure 5-79 Cancelling Parallel Track 210 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Cancelling parallel track: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD) FLIGHT INSTRUMENTS 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. Activating a Flight Plan Leg EIS The G1000 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: AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 3) Press 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. HAZARD AVOIDANCE AFCS Current Active Leg Selected Destination Waypoint ADDITIONAL FEATURES APPENDICES Activate Leg Softkey Figure 5-80 Active Flight Plan Page - Selecting the Leg Destination Waypoint INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 211 FLIGHT INSTRUMENTS SYSTEM OVERVIEW Flight Management EIS New Active Flight Plan Leg AUDIO PANEL & CNS Confirmation Window Figure 5-81 Active Flight Plan Page - New Active Leg FLIGHT MANAGEMENT Inverting a Flight Plan Any flight plan may be inverted (reversed) for navigation back to the original departure point. Inverting the active flight plan: HAZARD AVOIDANCE 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’. AFCS 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: ADDITIONAL FEATURES 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 flight plan to be inverted. APPENDICES 4) Press the INVERT Softkey; or press the MENU Key, select ‘Invert & Activate Flight Plan’ and press the ENT Key. An ‘Invert and activate stored flight plan?’ confirmation window is displayed. 5) Select ‘OK’. INDEX 6) Press the ENT Key to invert and activate the stored flight plan. To cancel, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. 212 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Flight Plan Views FLIGHT INSTRUMENTS 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. EIS 2) Press the VIEW Softkey to display the CUM and LEG-LEG Softkeys. 3) Press the CUM Softkey to view cumulative waypoint distance, or press the LEG-LEG Softkey to view leg-to-leg waypoint distance. AUDIO PANEL & CNS 4) Press 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 FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES WIDE Softkey, NARROW Softkey, LEG-LEG Softkey, CUM Softkey Figure 5-82 Active Flight Plan - Leg to Leg vs. Cumulative Distance Switching between wide and narrow view: APPENDICES 1) Press the FPL Key on the MFD to display the Active Flight Plan Page. 2) Press the VIEW Softkey to display the WIDE and NARROW Softkeys. 3) Press the WIDE Softkey to display the wide view, or press the NARROW Softkey to display the narrow view. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX 4) Press the BACK Softkey to return to the top level active flight plan softkeys. 213 SYSTEM OVERVIEW Flight Management Active Flight Plan Wide View AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Active Flight Plan Narrow View WIDE Softkey, NARROW Softkey, LEG-LEG Softkey, CUM Softkey FLIGHT MANAGEMENT Figure 5-83 Active Flight Plan - Wide vs. Narrow View Collapsing Airways HAZARD AVOIDANCE The G1000 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 reflects 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. INDEX APPENDICES ADDITIONAL FEATURES AFCS The Active Flight Plan Page always keeps the following three waypoints visible: “From” waypoint, “To” waypoint, and the “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. 214 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Q3.FEPOT Airway FLIGHT INSTRUMENTS Collapsed View Expanded View EIS Figure 5-84 Expanded/Collapsed Airways AUDIO PANEL & CNS 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) FLIGHT MANAGEMENT 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 HAZARD AVOIDANCE ‘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) AFCS 2) Press the MENU Key, highlight ‘Closest Point of FPL’’, and press the ENT Key. A window appears with the reference waypoint field highlighted. ADDITIONAL FEATURES 3) Enter the identifier of the reference waypoint and press the ENT Key. The G1000 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. APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 215 SYSTEM OVERVIEW Flight Management 5.7 Vertical Navigation FLIGHT INSTRUMENTS Note: The G1000 supports vertical navigation for all lateral leg types except for CA, CI, FA, FM, HA, HM, PI, VA, VD, VI, VR, and VM. Vertical constraints are not retained in stored flight plans. EIS The G1000 system Vertical Navigation (VNV) feature provides vertical profile guidance during the enroute and teminal 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 Current Vertical Navigation Profile Enabled (valid data) AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS Disabled (fields dashed) ENBL VNV Softkey CNCL VNV Softkey ADDITIONAL FEATURES Figure 5-85 Enabling/Disabling Vertical Navigation Enabling VNV guidance: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. APPENDICES 2) Press 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: INDEX 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Press the CNCL VNV Softkey; or press the MENU Key, highlight ‘Cancel VNV’, and press the ENT Key. Vertical navigation is disabled. 216 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW FLIGHT INSTRUMENTS 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. AUDIO PANEL & CNS Current Vertical Navigation Profile EIS The G1000 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 After VNV Direct-to FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS VNV Direct-To Softkey VNV PROF Softkey ADDITIONAL FEATURES Figure 5-86 Vertical Navigation Direct-To Activating a vertical navigation direct-to: APPENDICES 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 (light blue number) to be used. If not, the first waypoint in the flight plan with a designated altitude constraint is selected. INDEX 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. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 217 SYSTEM OVERVIEW Flight Management 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. FLIGHT INSTRUMENTS 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. EIS 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. AUDIO PANEL & CNS 4) Press the FMS Knob to remove the flashing cursor. Altitude Constraints FLIGHT MANAGEMENT The G1000 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 HAZARD AVOIDANCE Cross AT or ABOVE 5,000 ft Large White Text Large Light Blue Text Cross AT 2,300 ft AFCS Small Light Blue Text Cross AT or BELOW 3,000 ft Small Light Blue Subdued Text ADDITIONAL FEATURES Altitude Constraint Examples Small White Text with Altitude Restriction Bar INDEX APPENDICES Figure 5-87 Waypoint Altitude Constraints 218 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management Light Blue Text Light Blue Subdued Text 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 EIS 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. FLIGHT INSTRUMENTS 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 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. SYSTEM OVERVIEW White Text AUDIO PANEL & CNS Table 5-8 Altitude Constraint Size and Color Coding FLIGHT MANAGEMENT Altitudes associated with approach procedures are “auto-designated”. This means the system automatically uses the altitudes loaded with the 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. HAZARD AVOIDANCE 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. AFCS 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. ADDITIONAL FEATURES 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. APPENDICES 3) Press the ENT Key. The altitude is now shown in blue, indicating it is usable for vertical guidance. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX 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 G1000 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. 219 SYSTEM OVERVIEW Flight Management An altitude constraint is invalid if: • Meeting the constraint requires the aircraft to climb FLIGHT INSTRUMENTS • 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 EIS • The altitude constraint is added to the FAF of an approach that provides vertical guidance (i.e., ILS or GPS WAAS approach) • The altitude constraint is added to a waypoint past the FAF. Entering/modifiying an altitude constraint: AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 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 G1000 displays the altitude restriction from the database provided no predicted altitude can be provided. The G1000 also provides a way to reinstate a published altitude constraint that has been edited. AFCS Deleting an altitude constraint provided by the navigation database: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. ADDITIONAL FEATURES 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: APPENDICES 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. INDEX 4) Select ‘REMOVE’ and press the ENT Key. The manually entered altitude is deleted (it is replaced by a system calculated altitude, if available). 220 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 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. EIS 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. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 5) Edit the value using the FMS Knobs, and press the ENT Key. 6) Press the FMS Knob to remove the flashing cursor. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 221 SYSTEM OVERVIEW Flight Management 5.8 Procedures FLIGHT INSTRUMENTS The G1000 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. AUDIO PANEL & CNS EIS 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. Departures FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 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’. AFCS 3) Press the ENT Key. The Departure Loading Page is displayed. 4) Select a departure from the list and press the ENT Key. 5) Select a runway (if required) and press the ENT Key. ADDITIONAL FEATURES 6) Select a transition (if required) and press the ENT Key. ‘LOAD?’ is highlighted. INDEX APPENDICES 7) Press the ENT Key to load the departure procedure. 222 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Available Procedure Actions Departure Airport FLIGHT INSTRUMENTS EIS Departure Preview AUDIO PANEL & CNS Loaded Procedures Departure Choices Selected Departure FLIGHT MANAGEMENT Figure 5-88 Departure Selection Loaded Departure HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Procedure Loading Page Selection Softkeys Figure 5-89 Departure Loading INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 223 SYSTEM OVERVIEW Viewing available departures at an airport: FLIGHT INSTRUMENTS Flight Management 2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and press the ENT Key. 1) From the Airport Information Page (first page in the WPT group), press the DP Softkey. The Departure Information Page is displayed, defaulting to the airport displayed on the Airport information Page. 3) Press the FMS Knob, then turn the large FMS Knob to highlight the Departure. The departure is previewed on the map. EIS 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. The departure is previewed on the map. AUDIO PANEL & CNS 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) Press the INFO Softkey to return to the Airport Information Page. FLIGHT MANAGEMENT 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: HAZARD AVOIDANCE 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. AFCS Or: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD) ADDITIONAL FEATURES 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. INDEX APPENDICES 4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT Key. 224 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Arrivals FLIGHT INSTRUMENTS 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: EIS 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. AUDIO PANEL & CNS 4) 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. Available Procedure Actions FLIGHT MANAGEMENT 8) Press the ENT Key to load the arrival procedure. Destination Airport HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Loaded Procedures Arrival Preview Arrival Choices APPENDICES Figure 5-90 Arrival Selection INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 225 SYSTEM OVERVIEW Flight Management Loaded Arrival AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Selected Arrival Procedure Loading Page Selection Softkeys FLIGHT MANAGEMENT Figure 5-91 Arrival Loading Viewing available arrivals at an airport: HAZARD AVOIDANCE 1) From the Airport Information Page (first page in the WPT group), press 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) Press the FMS Knob, then turn the large FMS Knob to highlight the Arrival. The arrival is previewed on the map. AFCS 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. ADDITIONAL FEATURES 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. INDEX APPENDICES 7) Press the INFO Softkey to return to the Airport Information Page. 226 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Removing an Arrival from the Active Flight Plan When plans change while flying IFR, arrivals can be easily removed from the Active Flight Plan. FLIGHT INSTRUMENTS 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. EIS 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) AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT Key. Approaches nOTE: Check the Aircraft Flight Manual (AFM) to determine whether WAAS functionality is approved. HAZARD AVOIDANCE NOTE: If certain GPS parameters (WAAS, RAIM, etc.) are not available, some published approach procedures for the desired airport may not be displayed in the list of available approaches. AFCS 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. ADDITIONAL FEATURES 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. APPENDICES 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX 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. 227 SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS The G1000 WAAS GPS allows for flying LNAV, LNAV/VNAV, and LPV approaches according to the published chart. LNAV+V is a standard LNAV approach with advisory vertical guidance provided for assistance in maintaining a constant vertical glidepath similar to an ILS glideslope on approach. This guidance is displayed on the G1000 PFD in the same location as the ILS glideslope using a magenta diamond. In all cases where LNAV+V is indicated by the system during an approach, LNAV minima are used. The active approach type is annunciated on the HSI as shown in the following table: AUDIO PANEL & CNS EIS 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 minima LPV GPS approach using published LPV minima Example on HSI Approach Type - LNAV - LNAV+V - L/VNAV - LPV Table 5-9 Approach Types 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. HAZARD AVOIDANCE 3) Select an approach from the list and press the ENT Key. 4) Select a transition (if required) and press the ENT Key. 5) Barometric Minimums AFCS a) 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: b) To skip setting minimums, press the ENT Key. ADDITIONAL FEATURES 6) Press the ENT Key with ‘LOAD?’ highlighted to load the arrival 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 INDEX APPENDICES 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. 228 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Available Procedure Actions Destination Airport FLIGHT INSTRUMENTS EIS Approach Preview AUDIO PANEL & CNS Loaded Procedures Approach Choices Selected Approach FLIGHT MANAGEMENT Figure 5-92 Approach Selection Loaded Approach HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Procedure Loading Page Selection Softkeys LOAD or ACTIVATE? Annunciation APPENDICES Figure 5-93 Approach Loading INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 229 SYSTEM OVERVIEW Viewing available approaches at an airport: FLIGHT INSTRUMENTS Flight Management 2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and press the ENT Key. 1) From the Airport Information Page (first page in the WPT group), press the APR Softkey. The Departure Information Page is displayed, defaulting to the airport displayed on the Airport information Page. 3) Press the FMS Knob, then turn the large FMS Knob to highlight the Approach. The approach is previewed on the map. EIS 4) Turn the small FMS Knob to view the available approaches. Press the ENT Key to select the approach. The cursor moves to the Runway box. The approach 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. The approach is previewed on the map. AUDIO PANEL & CNS 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 approach is previewed on the map. 7) Press the INFO Softkey to return to the Airport Information Page. FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 3) Press 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) Press 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. AFCS 6) Turn the FMS Knob to highlight the desired transition, and press the ENT Key. 7) Barometric Minimums ADDITIONAL FEATURES a) 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. The ‘LOAD?’ field is highlighted. Or: b) To skip setting minimums, press the ENT Key. The ‘LOAD?’ field is highlighted. INDEX APPENDICES 8) Press the ENT Key with ‘LOAD?’ highlighted to load the arrival 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. 230 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Activating an Approach A previously loaded approach can be activated from the Procedures Window. FLIGHT INSTRUMENTS 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. EIS 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. AUDIO PANEL & CNS 2) Highlight ‘ACTIVATE VECTOR-TO-FINAL’ and press the ENT Key. Loading and activating an approach using the MENU Key: FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 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) AFCS 2) Press the MENU Key, and highlight ‘Remove Approach’. 3) Press the ENT Key. A confirmation window is displayed listing the approach procedure. ADDITIONAL FEATURES 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. APPENDICES 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. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 231 SYSTEM OVERVIEW Flight Management Missed Approach Activating a missed approach in the active flight plan: FLIGHT INSTRUMENTS 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: EIS Press the Go-Around Button. Course To Altitude FLIGHT MANAGEMENT AUDIO PANEL & CNS 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 Jeppesen, 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. ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE 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. APPENDICES Course to Altitude Leg INDEX Figure 5-94 Course to Altitude 232 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 5.9 Trip Planning FLIGHT INSTRUMENTS The G1000 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 manually entered fuel data and the active flight plan (to estimate remaining fuel). Trip Planning EIS 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 AUDIO PANEL & CNS Trip Planning Page Mode - Automatic/Manual FLIGHT MANAGEMENT Preview of Selected Flight Plan/ Flight Plan Leg Trip Input Data (sensor/pilot) Trip Statistics Desired Track Distance Est. Time Enroute Est. Time of Arrival Enroute Safe Altitude Sunrise Time (local) Sunset Time (local) - HAZARD AVOIDANCE - Departure Time (local) - Ground Speed - Fuel Flow - Fuel On Board Aircraft - Calibrated Airspeed - Indicated Altitude - Barometric Pressure - Total Air Temperature Other Statistics - Density Altitude - True Airspeed (TAS) AFCS Fuel Statistics Efficiency Total Endurance Remaining Fuel Remaining Endurance Fuel Required Total Range - Softkeys ADDITIONAL FEATURES - Automatic/Manual Page Mode - Flight Plan/Waypoint Mode Figure 5-95 Trip Planning Page APPENDICES 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. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX • Indicated altitude (IND ALTITUDE) - The primary source is the barometric altitude, and the secondary source of information is GPS altitude. 233 SYSTEM OVERVIEW Trip Statistics FLIGHT INSTRUMENTS Flight Management 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. 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 a specific leg (NN) selected, the waypoints are the endpoints of the selected leg. EIS 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. AUDIO PANEL & CNS 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). FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE • 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. AFCS - 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 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. ADDITIONAL FEATURES - If in waypoint mode then the ETA is the ETE added to the departure time. - 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. APPENDICES • Enroute safe altitude (ESA) - The ESA is shown as nnnnnFT INDEX • Destination sunrise and sunset times (SUNRISE, SUNSET) - These times are shown as hours:minutes and are the local time at the destination. 234 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW Fuel Statistics FLIGHT INSTRUMENTS 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. EIS • 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 for trip. AUDIO PANEL & CNS • Fuel endurance remaining at end of selected leg (REM ENDUR) - This value is calculated by subtracting the time of fuel endurance by the amount of time to go. • Fuel required for trip (FUEL REQ) - This value is calculated by multiplying the time to go by the fuel flow. FLIGHT MANAGEMENT • 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. HAZARD AVOIDANCE • 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). AFCS Selected Flight Plan NN - Selected Leg(s) 00 is Active FPL 01-99 are Stored FPLs ADDITIONAL FEATURES 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 5-96 Trip Planning Page - Flight Plan Mode APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 235 SYSTEM OVERVIEW Flight Management Selected Flight Plan Selected Leg(s) Not Available Not Available FLIGHT INSTRUMENTS Selected Starting and Ending Waypoints Figure 5-97 Trip Planning Page - Waypoint Mode Selecting automatic or manual page mode: EIS Press 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: AUDIO PANEL & CNS Press 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: FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE Selecting waypoints for waypoint mode: 1) Press 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. AFCS 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. ADDITIONAL FEATURES 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: APPENDICES 1) Press 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. INDEX 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. 236 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 5.10 RAIM Prediction FLIGHT INSTRUMENTS 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 WAAS 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. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT RAIM PREDICTION Box - Prediction Waypoint - Arrival Time - Arrival Date - RAIM Status HAZARD AVOIDANCE AFCS RAIM Softkey SBAS Softkey (displays SBAS Selection) (displays RAIM PREDICTION) ADDITIONAL FEATURES Figure 5-98 RAIM Prediction APPENDICES 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. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX 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, or airway waypoints). 237 SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 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. EIS 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. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT Status of the RAIM computation for the selected waypoint, time, and date is displayed at the bottom of the RAIM PREDICTION Box as follows: HAZARD AVOIDANCE 7) Press the ENT Key with ‘COMPUTE RAIM?’ highlighted to begin the computation. • ‘RAIM AVAILABLE’ - RAIM is predicted to be available. • ‘COMPUTE RAIM?’ - RAIM has not been computed. • ‘COMPUTING AVAILABILITY’ - RAIM calculation is in progress. • ‘RAIM NOT AVAILABLE’ - RAIM is predicted to be unavailable. INDEX APPENDICES ADDITIONAL FEATURES AFCS The Satellite Based Augmentation System (SBAS) provides increased navigation accuracy when available. SBAS can be enabled or disabled manually on the GPS Status Page. 238 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW FLIGHT INSTRUMENTS SBAS Status SBAS SELECTION Box - WAAS Enable/Disable EIS AUDIO PANEL & CNS RAIM Softkey SBAS Softkey (displays SBAS Selection) (displays RAIM PREDICTION) FLIGHT MANAGEMENT Figure 5-99 SBAS Display - Active Enabling/Disabling SBAS: HAZARD AVOIDANCE 1) Select the AUX-GPS Status Page. 2) Press the FMS Knob. The SBAS SELECTION ‘WAAS’ field is highlighted. 3) Press the ENT Key to disable SBAS. Press the ENT Key again to enable SBAS. AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 239 SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS SBAS Status SBAS SELECTION Box AUDIO PANEL & CNS EIS - WAAS Enable/Disable RAIM Softkey SBAS Softkey (displays SBAS Selection) FLIGHT MANAGEMENT (displays RAIM PREDICTION) INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Figure 5-100 SBAS Display - Disabled 240 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 5.11 Navigating a Flight Plan FLIGHT INSTRUMENTS The following discussion is an example of navigating a flight plan with the WAAS capable GPS system while the G1000 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: Check the Aircraft Flight Manual (AFM) to determine whether WAAS functionality is approved. nOTE: The following example flight plan is for instructional purposes only. All database information depicted EIS should be considered not current. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 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 5-101 indicating the active departure leg. After takeoff, ATC assigns a heading of 240º. 2) Figure 5-101 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. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 5-101 Assigned Heading of 240º INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 241 SYSTEM OVERVIEW Flight Management FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 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 5-102. Figure 5-102 Assigned Heading of 290º HAZARD AVOIDANCE 4) Enter V4 into the flight plan. INDEX APPENDICES ADDITIONAL FEATURES AFCS a) Press the FMS Knob to activate the cursor. 242 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 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 5-103. When the V4 entry point (TOP) is inserted, it is placed immediately above the highlighted waypoint (SLN). FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-103 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 5-104. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 5-104 Entering V4 Entry Point INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 243 SYSTEM OVERVIEW Flight Management AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS d) Press the ENT Key. TOP is inserted into the flight plan as in Figure 5-105. FLIGHT MANAGEMENT Figure 5-105 TOP Inserted into the Flight Plan e) With SLN still highlighted as in Figure 5-105, turn the small FMS Knob clockwise. The Waypoint Information Page is displayed and the LD AIRWY Softkey is now available. APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE f) Press the LD AIRWY Softkey to display the list of available airways for TOP as seen in Figure 5-106. Figure 5-106 List of Available Airways for TOP INDEX g) Turn either FMS Knob to highlight V4 in the list as seen in Figure 5-106. 244 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW h) Press the ENT Key. The list of available exits for V4 is now displayed as in Figure 5-107. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-107 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 5-107. HAZARD AVOIDANCE j) Press the ENT Key. The selected airway and exit are displayed, and the prompt “LOAD?” highlighted as in Figure 5-108. AFCS ADDITIONAL FEATURES APPENDICES Figure 5-108 Ready to Load V4 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX k) Press the ENT Key. 245 SYSTEM OVERVIEW Flight Management AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS l) V4 is now loaded into the flight plan as shown in Figure 5-109. FLIGHT MANAGEMENT Figure 5-109 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. HAZARD AVOIDANCE b) Turn the large FMS Knob to highlight SLN. The TO waypoint of the leg is selected in order to activate the leg. AFCS c) Press the ACT LEG Softkey. The confirmation window is now displayed as in Figure 5-110. Note the TOP to SLN leg is actually part of V4. INDEX APPENDICES ADDITIONAL FEATURES Figure 5-110 Comfirm Active Leg 246 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW FLIGHT INSTRUMENTS d) Verify the displayed leg is the desired leg and press the ENT Key. Note in Figure 5-111, 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. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 5-111 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. AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 247 SYSTEM OVERVIEW Flight Management FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 7) As the CDI approaches center, the aircraft turns onto the active leg as seen in Figure 5-112. Figure 5-112 Turn on to Active Leg ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE 8) At SLN, Victor Airway 244 (V244) is intercepted. Turn prompts are displayed in the PFD Navigation Status Box as seen in Figure 5-113. INDEX APPENDICES Figure 5-113 Turn to Intercept V244 248 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 9) As seen in Figure 5-114, V244 is now the active flight plan leg. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-114 V244 Now Active Leg HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 249 SYSTEM OVERVIEW Flight Management FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 10) At Lamar VOR (LAA) V263 is intercepted. See Figure 5-115. Figure 5-115 HYS to LAA Leg Active HAZARD AVOIDANCE 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. ) Key. The Direct-to Window is now displayed as shown in Figure 5-116. INDEX APPENDICES ADDITIONAL FEATURES AFCS c) Press the Direct-to ( Figure 5-116 Direct To OPSHN 250 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW d) Turn the large FMS Knob to place the cursor in the VNV altitude field as shown in Figure 5-117. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-117 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 5-118. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 5-118 Enter VNV Offset Distance 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX 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 G1000 gives vertical guidance so the aircraft arrives at an altitude of 10,000 feet three miles prior to OPSHN. 251 SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS h) Press the ENT Key twice to activate the direct-to. Note, in Figure 5-119, the magenta arrow indicating the directto 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 AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS to 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 light blue meaning it is used by the system to determine vertical speed and deviation guidance. ADDITIONAL FEATURES Figure 5-119 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. INDEX APPENDICES a) Press the PROC Key to display the Procedures Window. 252 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW b) ‘SELECT APPROACH’ should be highlighted as shown in Figure 5-120. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-120 Proceudures Window c) Press the ENT Key. A list of available approaches for the destination airport is displayed as in Figure 5-121. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 5-121 List of Available Approaches d) Turn either FMS Knob to select the LPV approach for 35R as shown in Figure 5-121. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 253 SYSTEM OVERVIEW Flight Management AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS e) Press the ENT Key. A list of available transitions for the selected approach is displayed as in Figure 5-122. FLIGHT MANAGEMENT f) Turn either FMS Knob to select the desired transition. In this case, the Initial Approach Fix (IAF) at HABUK is used. HAZARD AVOIDANCE Figure 5-122 List of Available Transitions 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. g) Press the ENT Key. h) Barometric Minimums Or: INDEX APPENDICES ADDITIONAL FEATURES AFCS To skip setting minimums, press the ENT Key. Figure 5-123 Barometric Minimums Set 254 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW i) With ‘LOAD?’ highlighted, again press the ENT Key. The selected approach is added to the flight plan as seen in Figure 5-124. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-124 Loaded Approach HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 255 SYSTEM OVERVIEW Flight Management 13) Note the altitude constraints associated with each of the approach waypoints as seen in Figure 5-125. These altitudes are loaded from the database and are displayed as light blue text, indicating these values are “designated” for use in computing vertical deviation guidance. EIS FLIGHT INSTRUMENTS 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. ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS 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 5-125. 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. INDEX APPENDICES Figure 5-125 Vertical Guidance is Active to the FAF 256 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS a) Press the VNV PROF Softkey to place the cursor in the target vertical speed field (VS TGT) as shown in Figure 5-126. 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. EIS 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. AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS Figure 5-126 Adjusting the Descent ADDITIONAL FEATURES c) Press the ENT Key. APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 257 SYSTEM OVERVIEW Flight Management FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 15) As seen in Figure 5-127, 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 5-128. When the aircraft is within one minute of the TOD, it is annunciated as shown in Figure 5-128, and an aural alert ‘Vertical track’ will be heard. HAZARD AVOIDANCE Figure 5-127 Approaching Top of Descent (TOD) AFCS Target Altitude ADDITIONAL FEATURES Vertical Deviation Indicator (VDI) APPENDICES Required Vertical Speed Indicator (RVSI) INDEX Figure 5-128 VDI & RVSI Upon Reaching Top of Descent (TOD) 258 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 16) Upon reaching TOD, a descent vertical speed is established which places the VSI pointer in line with the RVSI as shown in Figure 5-129. FLIGHT INSTRUMENTS EIS Keep Vertical Deviation Indicator Centered AUDIO PANEL & CNS Align Actual Vertical Speed with Required Vertical Speed FLIGHT MANAGEMENT Figure 5-129 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 5-130. Upon reaching the offset waypoint for OPSHN, the aircraft is at 10,000 feet. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 5-130 Approaching Bottom of Descent (BOD) at OPSHN Offset Waypoint INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 259 SYSTEM OVERVIEW Flight Management AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 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 5-131. 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. INDEX APPENDICES ADDITIONAL FEATURES Figure 5-131 Turn to intercept OPSHN to FSHER Leg 260 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 19) After passing OPSHN, the next leg of the arrival turns magenta as shown in Figure 5-132. The magenta arrow in the flight plan list now indicates the OPSHN to FSHER leg of the arrival procedure is now active. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-132 Tracking the OPSHN to FSHER Leg HAZARD AVOIDANCE 20) The flight continues through the arrival procedure to PYNON (see Figure 5-133). 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. AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 261 APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Flight Management INDEX Figure 5-133 Approaching PYNON 262 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 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 5-134). FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-134 Approach is Now Active HAZARD AVOIDANCE 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 5-135. AFCS c) Press the ENT Key to activate the approach. ADDITIONAL FEATURES APPENDICES Figure 5-135 Manually Activate Approach INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 263 SYSTEM OVERVIEW Flight Management FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 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. INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Figure 5-136 Descending Turn to the Initial Approach Fix (IAF) 264 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 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 5-137) when the final approach course becomes active. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-137 Descending to the FAF HAZARD AVOIDANCE 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 5-137. AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 265 SYSTEM OVERVIEW Flight Management FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 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 5-138. Figure 5-138 Descending to the Missed Approach Point AFCS HAZARD AVOIDANCE 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 Jeppesen, 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. INDEX APPENDICES ADDITIONAL FEATURES 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. 266 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS A direct-to is initiated to MOGAL, which is the Missed Approach Hold Point (MAHP) as seen in Figure 5-139. The aircraft is climbing to 10,000 feet. The CDI flight phase now changes from LPV to MAPR as seen on the HSI. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 5-139 Missed Approach Active INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 267 SYSTEM OVERVIEW Flight Management FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 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 5-140. Figure 5-140 Establishing the Holding Pattern APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE 27) The aircraft maintains 10,000 feet while following the magenta line through the hold as in Figure 5-141. INDEX Figure 5-141 Hold Established 268 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Flight Management SYSTEM OVERVIEW 5.12 Abnormal Operation This section discusses the Dead Reckoning mode of operation and the subsequent indications. FLIGHT INSTRUMENTS 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 G1000 stops using GPS. EIS While in Enroute or Oceanic phase of flight, if the G1000 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 G1000 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. AUDIO PANEL & CNS It is important to note that estimated navigation data supplied by the G1000 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 by the G1000 through DR while there is no heading and/or airspeed data available should not be used for navigation. FLIGHT MANAGEMENT DR Mode is inherently less accurate than the standard GPS/WAAS Mode due to the lack of satellite measurements needed to determine a position. Changes in wind speed and/or wind direction compounds 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. HAZARD AVOIDANCE DR Mode is indicated on the G1000 by the appearance of the letters ‘DR’ superimposed in yellow over the ‘own aircraft’ symbol as shown in Figure 5-142. 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 5-142. 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/WAAS source data resumes automatically once a valid GPS solution is restored. AFCS 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 5-142. ADDITIONAL FEATURES Also, while the G1000 is in DR Mode, the autopilot does not couple to GPS, and both TAWS and Terrain Proximity are disabled. Additionally, the accuracy of all nearest information (airports, airspaces, and waypoints) is questionable. Finally, airspace alerts continue to function, but with degraded accuracy. APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 269 SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS Distance & Bearing EIS Dead Reckoning Annunciaion Wind Data GPS Navigation Lost Message AUDIO PANEL & CNS Current Track Indicator FLIGHT MANAGEMENT Bearing Pointer/ Distance Wind Data Nav Data Bar HAZARD AVOIDANCE All data except Active Leg, TAS, and DTK are in yellow AFCS Dead Reckoning Annunciation ADDITIONAL FEATURES Subdued Aircraft Symbol APPENDICES Figure 5-142 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°, INDEX or when a 65° bank angle is reached. 270 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW Section 6 Hazard Avoidance FLIGHT INSTRUMENTS Hazard avoidance features available for the G1000 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 XM® Satellite Weather (Optional) • L-3 STORMSCOPE® WX-500 Series II Weather Mapping Sensor (Optional) Terrain Avoidance EIS • Terrain Proximity • TERRAIN-SVS (Standard with SVS option) AUDIO PANEL & CNS Traffic • Traffic Information Service (TIS) • Avidyne TAS600® Traffic Advisory System (TAS) (Optional) FLIGHT MANAGEMENT 6.1 XM Satellite Weather Note: XM Satellite Weather data provides information for avoiding hazardous weather. Do not utilize XM Weather information to penetrate hazardous weather. HAZARD AVOIDANCE XM Satellite Weather is provided through the GDL 69A, a remote-mounted data-link satellite receiver. Received graphical weather information and associated text is displayed on the Multi Function Display (MFD) and the Primary Flight Display (PFD) Inset Map. The GDL 69A can also receive XM Satellite Radio® entertainment services. Both weather data and entertainment programming operate in the S-band frequency range to provide continuous reception capabilities at any altitude throughout North America. AFCS XM Satellite Radio services are subscription-based. For more information on specific service packages, visit www.xmradio.com. ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 271 SYSTEM OVERVIEW Hazard Avoidance Activating Services FLIGHT INSTRUMENTS XM Satellite Weather must be activated before it can be used. Service is activated by providing XM Satellite Radio with coded IDs unique to the installed GDL 69A. XM Satellite Radio and XM Satellite Weather services each have coded IDs. The Data and Audio Radio IDs must be provided to XM Satellite Radio to activate the weather service and entertainment subscriptions, respectively. These IDs are located on: • The label on the back of the Data Link Receiver • The XM Information Page on the MFD (Figure 6-1) EIS • 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 Audio and Data Radio IDs cannot be located. AUDIO PANEL & CNS XM Satellite Radio uses the coded IDs to send an activation signal that allows the G1000 to display weather data and/or entertainment programming provided through the GDL 69A. Activating XM Satellite Weather and XM Satellite Radio services: FLIGHT MANAGEMENT 1) Contact XM Satellite Radio by email (address listed on their website, www.xmradio.com) or by the customer service phone number listed on the website. Follow the instructions provided by XM Satellite Radio services. 2) Select the XM Page in the Auxiliary Page Group. 3) Press the INFO Softkey to display the XM Information Page. 4) Verify that the desired services are activated. HAZARD AVOIDANCE 5) Press the LOCK Softkey. 6) Turn the large FMS Knob to highlight ‘YES’. AFCS 7) To complete activation, press the ENT Key. Audio Radio ID (for XM Satellite Radio) ADDITIONAL FEATURES Data Radio ID (for XM Weather) INDEX APPENDICES Weather Products (Available Products for Service Class Indicated in Green) Select to Display XM Information page 272 Figure 6-1 XM Information Page Garmin G1000 Pilot’s Guide for the Diamond DA42NG Select to Lock Subscription Information 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW Using XM Satellite Weather Products The primary map for viewing XM Weather data is the Weather Data Link Page in the Map Page Group. This is the only G1000 map display capable of showing information for all available XM weather products. FLIGHT INSTRUMENTS Viewing the Weather Data Link 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 Page. EIS NEXRAD Weather Product Age AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE NEXRAD Weather Product Selected for Display NEXRAD Weather Product Display Enabled Figure 6-2 Weather Data Link Page AFCS ADDITIONAL FEATURES When a weather product is active on the Weather Data Link Page or the Navigation Map Page, the age of the data is displayed on the screen (Figure 6-2). The age of the product is based on the time difference between when the data was assembled on the ground and the current GPS time. Weather products are refreshed at specific intervals (defined in the Refresh Rate column in Table 6-1). APPENDICES If for any reason, a weather product is not refreshed within the 30-, 60-, or 90-minute Expiration Time intervals (see Table 6-1), the data is considered expired and is removed from the display. This ensures that the displayed data is consistent with what is currently being broadcast by XM Satellite Radio services. If more than half of the expiration time has elapsed, the color of the product age displayed changes to yellow. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 273 SYSTEM OVERVIEW Hazard Avoidance FLIGHT INSTRUMENTS Table 6-1 shows the weather product symbols, the expiration time and the refresh rate. The refresh rate represents the interval at which XM Satellite Radio broadcasts new signals that may or may not contain new weather data. It does not represent the rate at which weather data is updated or new content is received by the Data Link Receiver. Weather data is updated at intervals that are defined and controlled by XM Satellite Radio and its data vendors. Weather Product Symbol EIS Next-generation Radar (NEXRAD) Cloud Top (CLD TOP) AUDIO PANEL & CNS Echo Top (ECHO TOP) INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT XM Lightning (LTNG) Cell Movement (CELL MOV) SIGMETs/AIRMETs (SIG/AIR) Meteorological Aerodrome Report (METARs) City Forecast (CITY) Surface Analysis (SFC) Freezing Levels (FRZ LVL) Winds Aloft (WIND) County Warnings (COUNTY) Cyclone Warnings (CYCLONE) Radar Coverage no product image (RADAR CVRG) Temporary Flight Restrictions no product image (TFRs) Terminal Aerodrome Reports no product image (TAFs) Expiration Time (Minutes) Refresh Rate (Minutes) 30 5 60 15 30 7.5 30 5 30 12 60 12 90 12 60 12 60 12 60 12 60 12 60 5 60 12 30 5 60 12 60 12 Table 6-1 Weather Product Symbols and Data Timing 274 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW Cloud Top (CLD TOP) + Echo Top (ECHO TOP) + Nearest Page Group Flight Plan Pages + AUX - Trip Planning Page Weather Data Link Page + Weather Information Page Navigation Map Page + + + + + + + + + + Cell Movement (CELL MOV) + + + + + + + + + METARs + City Forecast (CITY) + Surface Analysis (SFC) + Freezing Levels (FRZ LVL) + Winds Aloft (WIND) + County Warnings (COUNTY) + Cyclone Warnings (CYCLONE) + Radar Coverage TFRs + + + + + + + AFCS TAFs + + HAZARD AVOIDANCE + FLIGHT MANAGEMENT SIGMETs/AIRMETs (SIG/AIR) AUDIO PANEL & CNS XM Lightning (LTNG) EIS NEXRAD FLIGHT INSTRUMENTS Weather Product PFD Inset Map Table 6-2 shows which XM products can be displayed (indicated with a ‘+’ symbol) on specific maps. Table 6-2 Weather Product Display Maps ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 275 SYSTEM OVERVIEW Hazard Avoidance FLIGHT INSTRUMENTS 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 Page). When a weather product is selected for display, the corresponding softkey label changes to gray to indicate the product is enabled. Unavailable weather products have subdued softkey labels (softkeys are disabled from selection). NEXRAD ECHO TOP CLD TOP ENGINE FRZ LVL CELL MOV WIND OFF COUNTY SIG/AIR METAR LEGEND MORE WX CHKLIST LEGEND CYCLONE BACK EIS SFC OFF LTNG HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS SFC Softkey label changes to reflect current selection. WIND Softkey label changes to reflect current selection. OFF CURRENT 12 HR 24 HR 36 HR 48 HR Select the BACK Softkey to move up one level. LEGEND BACK 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 and NEXT softkeys cycle through Winds Aloft altitude selection softkeys. Figure 6-3 Weather Data Link Weather Product Softkeys INDEX APPENDICES ADDITIONAL FEATURES AFCS The setup menus for the Navigation Map Page and the Weather Data Link 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 a means in addition to the softkeys for enabling/disabling display of weather products. 276 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW Setting up and customizing the Weather Data Link Page: 1) Select the Weather Data Link Page. 2) Press the MENU Key. FLIGHT INSTRUMENTS 3) With ‘Weather Setup’ highlighted, press the ENT Key (Figure 6-4). 4) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-5). 5) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings, etc.). 6) Press the ENT Key to select an option. EIS 7) Press the FMS Knob or CLR Key to return to the Weather Data Link Page with the changed settings. AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 6-4 Weather Data Link Page Menu AFCS Figure 6-5 Weather Data Link Page Setup Menu ADDITIONAL FEATURES Restoring default Weather Data Link Page settings: 1) Select the Weather Data Link Page. 2) Press the MENU Key. APPENDICES 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. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 277 SYSTEM OVERVIEW Hazard Avoidance Maps besides the Weather Data Link Page use settings based on those selected for the Navigation Map Page. Setting up and customizing weather data for the Navigation Map Page: FLIGHT INSTRUMENTS 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). EIS 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. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. ADDITIONAL FEATURES AFCS Figure 6-6 Navigation Map Page Menu Figure 6-8 Navigation Map Page Setup Menu, Weather Group INDEX APPENDICES Figure 6-7 Navigation Map Page Setup Menu 278 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW Each active weather product has an associated legend which can be displayed on the Weather Data Link Page. Viewing legends for displayed weather products FLIGHT INSTRUMENTS 1) Select the Weather Data Link Page. 2) Press 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. EIS 3) Turn the FMS Knob to scroll through the legends. 4) To remove the Legend Window, press the LEGEND Softkey, the ENT or the CLR Key, or press the FMS Knob. • METARs • Cell Movement • County Warnings • SIGMETs • TFRs FLIGHT MANAGEMENT • Echo Tops AUDIO PANEL & CNS Additional information about the following can be displayed by panning over the display on the map: • AIRMETs The map panning feature is enabled by pressing the RANGE Knob. The map range is adjusted by turning the RANGE Knob. If the map range is adjusted while panning is enabled, the map is re-centered on the Map Pointer. HAZARD AVOIDANCE Additional Information on Weather Feature Selected with Map Pointer AFCS ADDITIONAL FEATURES Flash Flood Warning Selected with Map Pointer APPENDICES INDEX Figure 6-9 Panning on the Weather Data Link Page 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 279 SYSTEM OVERVIEW NEXRAD FLIGHT INSTRUMENTS Hazard Avoidance WSR-88D, or NEXRAD (NEXt-generation RADar), is a network of 158 high-resolution Doppler radar systems that are operated by the National Weather Service (NWS). NEXRAD data provides centralized meteorological information for the continental United States and selected overseas locations. The maximum range of a single NEXRAD radar site is 250 nm. In addition to a wide array of services, the NEXRAD network provides important information about severe weather and air traffic safety. NOTE: NEXRAD cannot be displayed at the same time as terrain. ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS NEXRAD data is not real-time. The lapsed time between collection, processing, and dissemination of NEXRAD images can be significant and may not reflect the current radar synopsis. Due to the inherent delays and the relative age of the data, it should be used for long-range planning purposes only. Never use NEXRAD data or any radar data to penetrate hazardous weather. Rather, use it in an early-warning capacity of predeparture and enroute evaluation. Figure 6-10 NEXRAD Data on the Weather Data Link Page APPENDICES NEXRAD data can be displayed on the following maps: • PFD Inset Map • Trip Planning Page • Navigation Map Page • Nearest Pages • Weather Data Link Page • Flight Plan Pages INDEX • Airport Information Page 280 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW Displaying NEXRAD weather information: 1) Press the MAP Softkey (for the PFD Inset Map, press the INSET Softkey). This step is not necessary on the Weather Data Link Page. FLIGHT INSTRUMENTS 2) Press 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 Page. For the NEXRAD legend (Figure 6-11), press the LEGEND Softkey when NEXRAD is selected for display. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT No Radar Coverage Figure 6-11 NEXRAD Data with Legend HAZARD AVOIDANCE The display of radar coverage is always active when either NEXRAD or ECHO TOPS is selected. Areas where NEXRAD radar coverage and Echo Tops information is not currently available or is not being collected are indicated in grayish-purple. Radar capability exists in these areas, but it is not active or is off-line. Reflectivity AFCS 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. ADDITIONAL FEATURES 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. APPENDICES 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. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 281 SYSTEM OVERVIEW Hazard Avoidance NEXRAD Limitations NEXRAD radar images may have certain limitations: FLIGHT INSTRUMENTS • 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. AUDIO PANEL & CNS EIS • 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). AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT Block Area is 4 km2 ADDITIONAL FEATURES Figure 6-12 NEXRAD Data - Zoomed The following may cause abnormalities in displayed NEXRAD radar images: • Ground clutter • Strobes and spurious radar data APPENDICES • Sun strobes (when the radar antenna points directly at the sun) • Interference from buildings or mountains, which may cause shadows INDEX • Metallic dust from military aircraft, which can cause alterations in radar scans 282 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW NEXRAD Limitations (Canada) • Radar coverage extends to 55ºN. • Any precipitation displayed between 52ºN and 55ºN is displayed as mixed because it is unknown. FLIGHT INSTRUMENTS No Coverage Above 55ºN EIS AUDIO PANEL & CNS Precipitation Above 52ºN Displays as Mixed FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 6-13 NEXRAD Data - Canada AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 283 SYSTEM OVERVIEW Echo Tops FLIGHT INSTRUMENTS Hazard Avoidance Echo Tops data (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. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS Note: Display of Echo Tops is mutually exclusive with Cloud Tops and NEXRAD. Figure 6-14 Echo Tops Data AFCS Displaying Echo Tops information: 1) Select the Weather Data Link Page. 2) Press the ECHO TOP Softkey. APPENDICES ADDITIONAL FEATURES To display the Echo Tops legend (Figure 6-15), press 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 activated, NEXRAD and Cloud Tops data are removed. INDEX No Radar Coverage Figure 6-15 ECHO TOPS Legend 284 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW The display of radar coverage is always active when either NEXRAD or ECHO TOPS is selected. Areas where NEXRAD radar coverage and Echo Tops information is not currently available or is not being collected are indicated in grayish-purple. Radar capability exists in these areas, but it is not active or is off-line. FLIGHT INSTRUMENTS Cloud Tops Note: Cloud Tops and Echo Tops cannot be displayed at the same time. Cloud Tops data (Figure 6-16) depicts cloud top altitudes as determined from satellite imagery. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 6-16 Cloud Tops Data AFCS Displaying Cloud Tops information: 1) Select the Weather Data Link Page. ADDITIONAL FEATURES 2) Press the CLD TOP Softkey. To display the Cloud Tops legend (Figure 6-17), press 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, Echo Tops data is removed. APPENDICES INDEX Figure 6-17 Cloud Tops Legend 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 285 SYSTEM OVERVIEW Hazard Avoidance XM Lightning Note: GDL 69/69A XM® Satellite Weather Lightning and L-3 STORMSCOPE® WX-500 Lightning are FLIGHT INSTRUMENTS mutually exclusive. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS Lightning data (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. HAZARD AVOIDANCE Lightning Strikes Figure 6-18 Lightning Data ADDITIONAL FEATURES AFCS XM Lightning data displays on the following maps: • PFD Inset Map • Trip Planning Page • Navigation Map Page • Nearest Pages • Weather Data Link Page • Flight Plan Pages Displaying XM Lightning information: APPENDICES 1) Press the MAP Softkey (for the PFD Inset Map, press the INSET Softkey). This step is not necessary on the Weather Data Link Page. 2) Press the XM LTNG Softkey (LTNG Softkey on the Weather Data Link Page). INDEX To display the XM Lightning legend on the Weather Data Link Page (Figure 6-19), press the LEGEND Softkey when XM Lightning is selected for display. Figure 6-19 Lightning Legend 286 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW Cell Movement FLIGHT INSTRUMENTS Cell Movement data (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. EIS AUDIO PANEL & CNS Storm Cells FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 6-20 Cell Movement Data On most applicable maps, Cell Movement data is selected for display along with NEXRAD. On the Weather Data Link Page, Cell Movement data can be selected independently. Cell Movement data can be displayed on the following maps: • AUX - Trip Planning Page •Navigation Map • Nearest Pages AFCS • PFD Inset Map Displaying Cell Movement information: ADDITIONAL FEATURES 1) Press the MAP Softkey (for the PFD Inset Map, press the INSET Softkey). This step is not necessary on the Weather Data Link Page. APPENDICES 2) Press the NEXRAD Softkey (CEL MOV Softkey on the Weather Data Link Page). For Cell Movement to be displayed on maps other than the Weather Data Link Page, Cell Movement must be turned on in the Navigation Map Setup Menu (see “Setting Up XM Satellite Weather”). To display the Cell Movement legend on the Weather Data Link Page, (Figure 6-21), press the LEGEND Softkey when Cell Movement is selected for display. INDEX Figure 6-21 Cell Movement Legend 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 287 SYSTEM OVERVIEW Hazard Avoidance SIGMETs and AIRMETs FLIGHT INSTRUMENTS SIGMET (SIGnificant METeorological Information) and AIRMET (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. Instructions for Viewing SIGMET/ AIRMET Text EIS Airmet Ice Airmet IFR FLIGHT MANAGEMENT AUDIO PANEL & CNS AIRMET Turbulence HAZARD AVOIDANCE Figure 6-22 SIGMET/AIRMET Data Displaying SIGMETs and AIRMETs: 1) Select the Weather Data Link Page. 2) Press the SIG/AIR Softkey. AFCS 3) To view the text of the SIGMET or AIRMET, press the RANGE Knob and move the Map Pointer over the icon. 4) Press the ENT key. Figure 6-23 shows sample SIGMET text. INDEX APPENDICES ADDITIONAL FEATURES To display the SIGMET and AIRMET legend (Figure 6-24), press the LEGEND Softkey when SIGMETs and AIRMETs are selected for display. Figure 6-23 Sample SIGMET Text 288 Figure 6-24 SIGMET/AIRMET Legend Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW METARs and TAFs NOTE: Atmospheric pressure as reported for METARs is given in hectopascals (hPa), except for in the United FLIGHT INSTRUMENTS 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 aviation database service area. EIS METARs (METeorological Aerodrome Reports) typically contain information about the temperature, dewpoint, wind, precipitation, cloud cover, cloud 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. AUDIO PANEL & CNS Instructions for Viewing METAR and TAF Text FLIGHT MANAGEMENT HAZARD AVOIDANCE Selected Airport AFCS ADDITIONAL FEATURES Figure 6-25 METAR Flags on the Weather Data Link 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. APPENDICES METAR and TAF text are displayed on the Weather Information Page. METAR data is displayed first in a decoded fashion, then as raw text. TAF information is displayed only in its raw form when it is available Displaying METAR and TAF text: 1) On the Weather Data Link Page, press the METAR Softkey. INDEX 2) Press the RANGE Knob and pan to the desired airport. 3) Press the ENT Key. The Weather Information Page is shown with METAR and TAF text. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 289 SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS Hazard Avoidance 5) Press the FMS Knob or the CLR Key to return to the Weather Data Link Page. Or: 1) Select the Weather Information Page. a) Turn the large FMS Knob to select the Waypoint Page Group. b) Press the WX Softkey to select the Weather Information Page. EIS 2) Press the FMS Knob to display the cursor. 3) Use the FMS Knob to enter the desired airport and press the ENT Key. FLIGHT MANAGEMENT AUDIO PANEL & CNS 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 HAZARD AVOIDANCE METAR Symbol AFCS TAF Text for the Selected Airport ADDITIONAL FEATURES Figure 6-26 METAR and TAF Text on the Weather Information Page To display the METAR legend on the Weather Data Link Page (Figure 6-27), press the LEGEND Softkey when METARs are selected for display. INDEX APPENDICES The METAR flag color is determined by the information in the METAR text. A gray METAR flag is displayed when the METAR text does not contain adequate information. Figure 6-27 METAR Legend 290 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW Surface Analysis and City Forecast Note: Surface Analysis and City Forecast data are displayed only within the installed Aviation Database FLIGHT INSTRUMENTS service area. Surface Analysis and City Forecast information (Figure 6-28) is available for current and forecast weather conditions. Forecasts are available for intervals of 12, 24, 36, and 48 hours. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 6-28 Current Surface Analysis Data Displaying Surface Analysis and City Forecast information: AFCS 1) Select the Weather Data Link Page. 2) Press the MORE WX Softkey. 3) Press the SFC Softkey. ADDITIONAL FEATURES 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), press the LEGEND Softkey when Surface Analysis and City Forecast are selected to be displayed. APPENDICES INDEX Figure 6-29 City Forecast and Surface Analysis Legend 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 291 SYSTEM OVERVIEW Hazard Avoidance Freezing Levels HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Freezing Level data (Figure 6-30) shows the color-coded contour lines for the altitude and location at which the first isotherm is found. 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 appears at the next update. Figure 6-30 Freezing Level Data Displaying Freezing Level information: AFCS 1) Select the Weather Data Link Page. 2) Press the MORE WX Softkey. 3) Press the FRZ LVL Softkey. APPENDICES ADDITIONAL FEATURES To display the Freezing Level legend (Figure 6-31), press the LEGEND Softkey when Freezing Level data is selected to be displayed. INDEX Figure 6-31 Freezing Level Legend 292 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW Winds Aloft Winds Aloft data (Figure 6-32) shows the forecasted wind speed and direction at the surface and at selected altitudes. Altitude can be displayed in 3,000-foot increments up to 42,000 feet MSL. FLIGHT INSTRUMENTS Displaying Winds Aloft data: 1) Select the Weather Data Link Page. 2) Press the MORE WX Softkey. 3) Press the WIND Softkey. EIS 4) Select the desired altitude level: SFC (surface) up to 42,000 feet. Press the NEXT or PREV Softkey to cycle through the altitude softkeys. The WIND Softkey label changes to reflect the altitude selected. AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS Figure 6-32 Winds Aloft Data at 27,000 Feet ADDITIONAL FEATURES To display the Winds Aloft legend (Figure 6-33), press the LEGEND Softkey when Winds Aloft is selected for display. APPENDICES Figure 6-33 Winds Aloft Data with Legend INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 293 SYSTEM OVERVIEW Hazard Avoidance County Warnings FLIGHT INSTRUMENTS County data (Figure 6-34) provides specific public awareness and protection weather warnings from the National Weather Service (NWS). This can include information on fires, tornadoes, severe thunderstorms, flood conditions, and other natural disasters. AUDIO PANEL & CNS EIS Additional Information on Flood Warning Selected with Map Pointer HAZARD AVOIDANCE FLIGHT MANAGEMENT Flood Warning Figure 6-34 County Flood Warning AFCS Displaying County Warning information: 1) Select the Weather Data Link Page. 2) Press the MORE WX Softkey. ADDITIONAL FEATURES 3) Press the COUNTY Softkey. APPENDICES To display the County Warnings legend (Figure 6-35), press the LEGEND Softkey when County Warnings are selected to be displayed. INDEX Figure 6-35 County Warnings Legend 294 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW Cyclone The Cyclone weather product (Figure 6-36) shows the current location of cyclones (hurricanes) and their projected tracks. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS Cyclone FLIGHT MANAGEMENT Figure 6-36 Cyclone Data Selected for Display HAZARD AVOIDANCE Displaying cyclone (hurricane) track information: 1) Select the Weather Data Link Page. 2) Press the MORE WX Softkey. AFCS 3) Press the CYCLONE Softkey. To display the Cyclone legend (Figure 6-37), press the LEGEND Softkey when Cyclones are selected to be displayed. ADDITIONAL FEATURES Figure 6-37 Cyclone Legend APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 295 SYSTEM OVERVIEW Hazard Avoidance 6.2 WX-500 Stormscope FLIGHT INSTRUMENTS NOTE: The Stormscope system is not intended for hazardous thunderstorm penetration. Weather information on the G1000 MFD is approved for weather avoidance only. Refer to the WX-500 User’s Guide for a detailed description of Stormscope operation. Note: L-3 STORMSCOPE® WX-500 Lightning and GDL 69/69A XM® Satellite Weather Lightning are EIS mutually exclusive. The following pages can display Stormscope data: AUDIO PANEL & CNS • Stormscope Page • Navigation Map • AUX - Trip Planning Page • Nearest Pages HAZARD AVOIDANCE FLIGHT MANAGEMENT To display Stormscope data on the Navigation Map, AUX - Trip Planning Page, or any of the Nearest Pages, press the MAP Softkey, then press the STRMSCP Softkey. These pages can also display cell or strike data using the yellow lightning strike symbology shown in Table 6-3. Table 6-3 Lightning Age and Symbols AFCS Setting Up Stormscope on the Navigation Map Setting up Stormscope options on the Navigation Map: ADDITIONAL FEATURES 1) On the Navigation Map Page, press the MENU Key. 2) With ‘Map Setup’ selected (Figure 6-38), press the ENT Key. 3) Turn the small FMS Knob to display the group selection window. Turn the small FMS Knob to select ‘Weather’ (Figure 6-39), and press the ENT Key. APPENDICES 4) Turn the large FMS Knob to highlight and move between the product selections. 5) When an item is highlighted, turn the small FMS Knob to select the option. 6) Press the ENT Key. INDEX 7) Press the FMS Knob to return to the Navigation Map Page (Figure 6-40). 296 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW The following options are available (Figure 6-39): • STRMSCP LTNG – Turns the display of Stormscope data on or off. FLIGHT INSTRUMENTS • STRMSCP MODE – Selects the CELL or STRIKE mode of lightning activity. Cell mode identifies clusters or cells of electrical activity. Strike mode indicates the approximate location of lightning strikes. • STRMSCP SMBL – Selects the range at which Stormscope data displays. Stormscope data is removed when a map range greater than the STRMSCP SMBL value is selected. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 6-38 Page Menu HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 6-39 Map Setup Menu INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 297 SYSTEM OVERVIEW Hazard Avoidance Cell and Strike Mode on the Navigation Map FLIGHT INSTRUMENTS On the Navigation Map, cell mode identifies cells of lightning activity (Figure 6-40). Stormscope identifies clusters of electrical activity that indicate cells. Strike mode indicates the approximate location of lightning strikes. Selecting the ‘cell’ or ‘strike’ mode on the Navigation Map: 1) Press the MENU Key. 2) With ‘Map Setup’ selected, press the ENT Key. 3) Select the ‘Weather’ group. EIS 4) Press the ENT Key. The cursor flashes on ‘STRMSCP LTNG’. 5) Turn the large FMS Knob to select ‘STRMSCP MODE’. AUDIO PANEL & CNS 6) Turn the small FMS Knob to change between ‘CELL’ and ‘STRIKE’ options. When an item is selected, press the ENT Key. ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT 7) Press the FMS knob to return to the Navigation Map Page. Figure 6-40 Navigation Map Page with Stormscope Lightning Data APPENDICES If heading input is lost, strikes and/or cells must be cleared manually after the execution of each turn (Figure 6-41). This is to ensure that the strike and/or cell positions are depicted accurately in relation to the nose of the aircraft. Manually clearing Stormscope data on the Navigation Map: INDEX 1) Press the MENU Key. 2) Select ‘Clear Stormscope Lightning’ (Figure 6-41). 3) Press the ENT Key. 298 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW FLIGHT INSTRUMENTS Figure 6-41 Navigation Map Page Options Menu EIS Zoom Range on the Navigation Map AUDIO PANEL & CNS Stormscope lightning data can be displayed up to 800 nm zoom range (in North up mode) on the Navigation Map Page. However, in the track up mode at the 500 nm range, a portion of Stormscope lightning data can be behind the aircraft and therefore not visible on the Navigation Map. Since the range for Stormscope data is 400 nm diameter total (200 nm in front and 200 nm behind), the 500 nm range in North up mode shows all the data. FLIGHT MANAGEMENT At a map range of less than 25 nm, Stormscope lightning data is not displayed, but can still be present. The presence of Stormscope lightning data is indicated by the annunciation ‘LTNG < 25 nm’ in the upper right corner (Figure 6-42). HAZARD AVOIDANCE Figure 6-42 Lightning Display Range Annunciation AFCS Selecting a Stormscope range on the Navigation Map: 1) Press the MENU Key. ADDITIONAL FEATURES 2) Select ‘MAP SETUP’. 3) Select the ‘Weather’ group. 4) Press the ENT Key. APPENDICES 5) Turn the large FMS Knob to select ‘STRMSCP SMBL’. 6) Turn the small FMS Knob to select the maximum display range. 7) Press the ENT Key. 8) Press the FMS Knob to return to the Navigation Map Page. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX To change the display range on the Navigation Map Page, turn the RANGE Knob clockwise to zoom out or counter-clockwise to zoom in. 299 SYSTEM OVERVIEW Hazard Avoidance Selecting the Stormscope Page Stormscope lightning data can be displayed at the ranges of 25 nm, 50 nm, 100 nm, and 200 nm. FLIGHT INSTRUMENTS Adjusting the Stormscope Map Range: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Stormscope Page. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 3) To change the map range, turn the RANGE Knob clockwise to zoom out or counter-clockwise to zoom in. AFCS Figure 6-43 Stormscope Page Changing between ‘cell’ and ‘strike’ mode on the Stormscope Page: 1) Select the Stormscope Page. ADDITIONAL FEATURES 2) Press the MODE Softkey. The CELL and STRIKE softkeys are displayed. 3) Press the CELL Softkey to display ‘CELL’ data or press the STRIKE Softkey to display ‘STRIKE’ data. ‘CELL’ or ‘STRIKE’ is displayed in the mode box in the upper left corner of the Stormscope Page. APPENDICES Changing the viewing mode between 360˚ and 120˚ on the Stormscope Page: INDEX 4) Press the BACK Softkey to return to the main Stormscope page. 3) Press the BACK Softkey to return to the main Stormscope page. 1) Select the Stormscope Page. 2) Press the VIEW Softkey. The 360 and ARC softkeys are displayed. Press the 360 Softkey to display a 360˚ viewing area or press the ARC Softkey to display a 120˚ viewing area. 300 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW 6.3 Terrain Proximity FLIGHT INSTRUMENTS Warning: Do not use Terrain Proximity information for primary terrain avoidance. Terrain Proximity is intended only to enhance situational awareness. NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75° North or 60° South. EIS G1000 Terrain Proximity is a terrain awareness system that does not comply with TSO-C151b certification standards. It increases situational awareness and aids in reducing controlled flight into terrain (CFIT). Do not confuse Terrain Proximity with Terrain Awareness and Warning System (TAWS). TAWS is more sophisticated and robust, and it is TSO-C151b certified. Terrain Proximity does not provide warning annunciations or voice alerts. It only provides color indications on map displays when terrain and obstacles are within a certain altitude threshold from the aircraft. Although the terrain and obstacle color map displays are the same, TAWS uses more sophisticated algorithms to assess aircraft distance from terrain and obstacles. AUDIO PANEL & CNS Terrain Proximity requires the following components to operate properly: • Valid 3-D GPS position FLIGHT MANAGEMENT • Valid terrain/obstacle database HAZARD AVOIDANCE Terrain Proximity displays altitudes of terrain and obstructions relative to the aircraft position and altitude with reference to a database that may contain inaccuracies. Terrain and obstructions are shown only if they are in the database. Terrain and obstacle information should be used as an aid to situational awareness. They should never be used to navigate or maneuver around terrain. Note that all obstructions may not be available in the terrain and obstacle database. No terrain and obstacle information is shown without a valid 3-D GPS position. AFCS The G1000 GPS receiver provides the horizontal position and altitude. GPS altitude is derived from satellite position. GPS altitude is then converted to a mean sea level (MSL)-based altitude (GPS-MSL altitude) and is used to determine terrain and obstacle proximity. GPS-MSL altitude accuracy is affected by satellite geometry, but is not subject to variations in pressure and temperature that normally affect pressure altitude sensors. GPS-MSL altitude does not require local altimeter settings to determine MSL altitude. It is a widely-used MSL altitude source. ADDITIONAL FEATURES Terrain and obstacle databases are referenced to MSL. Using the GPS position and altitude, the Terrain Proximity feature portrays a 2-D picture of the surrounding terrain and obstacles relative to the position and altitude of the aircraft. GPS position and GPS-MSL altitude are used to calculate and predict the aircraft’s flight path in relation to the surrounding terrain and obstacles. In this way, the pilot can view predicted dangerous terrain and obstacle conditions. APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 301 SYSTEM OVERVIEW Hazard Avoidance Displaying Terrain Proximity Data FLIGHT INSTRUMENTS The symbols and colors in Figure 6-44 and Table 6-4 are used to represent obstacles and aircraft altitude when the Terrain Proximity Page is selected for display. Terrain Proximity uses black, yellow, and red to represent terrain information relative to aircraft altitude. The color of each obstacle is associated with the altitude of the aircraft. Terrain Above Aircraft Altitude Red terrain is above or within 100 ft below the aircraft altitude Aircraft Altitude EIS 100 ft Threshold 1000 ft AUDIO PANEL & CNS Yellow terrain is between 100 ft and 1000 ft below the aircraft altitude Black terrain is more than 1000 ft below the aircraft altitude FLIGHT MANAGEMENT Figure 6-44 Terrain Altitude/Color Correlation for Terrain Proximity Unlighted Obstacle Lighted Obstacle < 1000’ AGL > 1000’ AGL < 1000’ AGL > 1000’ AGL Obstacle Location HAZARD AVOIDANCE 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 AFCS Table 6-4 Terrain Proximity Terrain/Obstacle Colors and Symbology ADDITIONAL FEATURES Terrain and obstacle information can be displayed on the following pages: • PFD Inset Map • Trip Planning Page • Navigation Map Page • Flight Plan Page • Terrain Proximity Page Displaying terrain and obstacle information (maps other than the Terrain Proximity Page): APPENDICES 1) Press the MAP Softkey (for the PFD Inset Map, press the INSET Softkey). 2) Press the TERRAIN Softkey to display terrain and obstacle data. When Terrain Proximity is selected on maps other than the Terrain Proximity Page, an icon to indicate the feature is enabled for display and a legend for Terrain Proximity colors are shown (Figure 6-48). INDEX 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 302 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW obstacle data are decluttered from the display. If a map range larger than the map range setting is selected, the data is removed from the map. FLIGHT INSTRUMENTS Terrain data can be selected for display independently of obstacle data; however, obstacles recognized by Terrain Proximity as yellow or red are shown when terrain is selected for display and the map range is within the setting limit. Maps besides the Terrain Proximity 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. EIS Customizing terrain and obstacle display on the Navigation Map Page: 1) Select the Navigation Map Page. AUDIO PANEL & CNS 2) Press the MENU Key. 3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-45). 4) Turn the small FMS Knob to select the ‘Map’ Group and press the ENT Key (Figure 6-46). FLIGHT MANAGEMENT 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-47). • TERRAIN DATA – Turns the display of terrain data on or off and sets maximum range at which terrain is shown • OBSTACLE DATA – Turns the display of obstacle data on or off 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). HAZARD AVOIDANCE 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. AFCS ADDITIONAL FEATURES Figure 6-45 Navigation Map Page Menu APPENDICES INDEX Figure 6-46 Navigation Map Page Setup Menu 190-00962-00 Rev. B Figure 6-47 Navigation Map Page Setup Menu, Map Group Garmin G1000 Pilot’s Guide for the Diamond DA42NG 303 SYSTEM OVERVIEW Hazard Avoidance Additional information about obstacles can be displayed by panning over the display on the map. The map panning feature is enabled by pressing the RANGE Knob. The map range is adjusted by turning the RANGE Knob. If the map range is adjusted while panning is enabled, the map is re-centered on the Map Pointer. Red Terrain Area (Above or Within 100’ Below Aircraft Altitude) Red Lighted Obstacles (Above or Within 100’ Below Aircraft Altitude) EIS FLIGHT INSTRUMENTS Additional Information on Obstacle Selected with Map Pointer Yellow Terrain Area (Between 100’ and 1000’ Below Aircraft Altitude) AUDIO PANEL & CNS Lighted Obstacle Selected with Map Pointer FLIGHT MANAGEMENT Terrain Display Enabled Terrain Legend HAZARD AVOIDANCE Figure 6-48 Terrain Information on the Navigation Map Page Terrain Proximity Page AFCS The Terrain Proximity Page is specialized to show terrain and obstacle data in relation to the aircraft’s current altitude, without clutter from the basemap. Aviation data (airports, VORs, and other NAVAIDs) can be displayed for reference. ADDITIONAL FEATURES 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 RANGE Knob from 1 to 200 nm, as indicated by the map range rings (or arcs). Displaying the Terrain Proximity Page: 1) Turn the large FMS Knob to select the Map Page Group. APPENDICES 2) Turn the small FMS Knob to select the Terrain Proximity Page. 3) To change the view, a) Press the VIEW Softkey. b) Press the 360 or ARC Softkey to select the desired view. INDEX Or: a) Press the MENU Key. b) Select ‘View 120º’ or ‘View 360º’ (choice dependent on current state) and press the ENT Key to change the view. 304 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW Showing/hiding aviation information on the Terrain Proximity 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. FLIGHT INSTRUMENTS Map Orientation Red Terrain (Above or Within 100’ Below the Aircraft Altitude) Current Aircraft GPS-derived MSL Altitude EIS Yellow Terrain (Between 100’ and 1000’ Below the Aircraft Altitude) Map Range Rings AUDIO PANEL & CNS Black Terrain (More than 1000’ Below the Aircraft Altitude) FLIGHT MANAGEMENT Terrain Legend Figure 6-49 Terrain Proximity Page HAZARD AVOIDANCE AFCS Map Range Arcs Yellow Terrain (Between 100’ and 1000’ Below the Aircraft Altitude) ADDITIONAL FEATURES Black Terrain (Terrain More than 1000’ Below the Aircraft Altitude) Red Terrain (Above or Within 100’ Below the Aircraft Altitude) APPENDICES Terrain Legend Figure 6-50 Terrain Proximity Page (ARC View) INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 305 SYSTEM OVERVIEW Hazard Avoidance 6.4 TERRAIN-SVS FLIGHT INSTRUMENTS Warning: Do not use TERRAIN-SVS information for primary terrain avoidance. TERRAIN-SVS is intended only to enhance situational awareness. NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75° North or 60° South. EIS NOTE: TERRAIN-SVS is standard when the Synthetic Vision System (SVS) option is installed. AUDIO PANEL & CNS G1000 TERRAIN-SVS is a terrain awareness system available with the Synthetic Vision System (SVS). SVS functionality is offered as an optional enhancement. TERRAIN-SVS is integrated within SVS to provide visual and auditory alerts to indicate the presence of threatening terrain relevant to the projected flight path. For detailed information regarding SVS, refer to the Synthetic Vision System (SVS) section of the G1000 Pilot’s Guide. FLIGHT MANAGEMENT TERRAIN-SVS does not comply with TSO-C151b certification standards. It increases situational awareness and aids in reducing controlled flight into terrain (CFIT). Do not confuse TERRAIN-SVS with Terrain Awareness and Warning System (TAWS). TAWS is more sophisticated and robust, and it is TSO-C151b certified. Although the terrain and obstacle color map displays are the same, TAWS uses more sophisticated algorithms to assess aircraft distance from terrain and obstacles. TERRAIN-SVS does not provide the following: HAZARD AVOIDANCE • Premature Descent Alerting (PDA) • Excessive Descent Rate (EDR) • Negative Climb Rate (NCR) • Descent to 500 Feet Callout (DFC) AFCS TERRAIN-SVS requires the following components to operate properly: • Valid 3-D GPS position • Valid terrain/obstacle database ADDITIONAL FEATURES TERRAIN-SVS displays altitudes of terrain and obstructions relative to the aircraft position and altitude with reference to a database that may contain inaccuracies. Terrain and obstructions are shown only if they are in the database. Terrain and obstacle information should be used as an aid to situational awareness. They should never be used to navigate or maneuver around terrain. APPENDICES Note that all obstructions may not be available in the terrain and obstacle database. No terrain and obstacle information is shown without a valid 3-D GPS position. INDEX The G1000 GPS receiver provides the horizontal position and altitude. GPS altitude is derived from satellite position. GPS altitude is then converted to a mean sea level (MSL)-based altitude (GPS-MSL altitude) and is used to determine terrain and obstacle proximity. GPS-MSL altitude accuracy is affected by satellite geometry, but is not subject to variations in pressure and temperature that normally affect pressure altitude sensors. GPS-MSL altitude does not require local altimeter settings to determine MSL altitude. It is a widely-used MSL altitude source. 306 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW FLIGHT INSTRUMENTS Terrain and obstacle databases are referenced to MSL. Using the GPS position and altitude, the TERRAIN-SVS feature portrays a 3-D picture of the surrounding terrain and obstacles relative to the position and altitude of the aircraft. GPS position and GPS-MSL altitude are used to calculate and predict the aircraft’s flight path in relation to the surrounding terrain and obstacles. In this way, the pilot can view predicted dangerous terrain and obstacle conditions. Displaying TERRAIN-SVS Data EIS TERRAIN-SVS 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 Figure 6-51 and Table 6-5 are used to represent terrain, obstacles, and potential impact points. AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 6-51 Terrain Altitude/Color Correlation for TERRAIN-SVS HAZARD AVOIDANCE Unlighted Obstacle Lighted Obstacle Potential < 1000’ AGL > 1000’ AGL < 1000’ AGL > 1000’ AGL Impact Points Obstacle Location WARNING: Red obstacle is above or within 100’ below current aircraft altitude AFCS CAUTION: Yellow obstacle is between 100’ and 1000’ below current aircraft altitude ADDITIONAL FEATURES Table 6-5 TERRAIN-SVS Obstacle Colors and Symbology TERRAIN-SVS information can be displayed on the following maps: • Trip Planning Page • Navigation Map Page • Flight Plan Pages APPENDICES • PFD Inset Map • TERRAIN-SVS Page INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 307 SYSTEM OVERVIEW Hazard Avoidance Displaying terrain and obstacle information (maps other than the TERRAIN-SVS Page): 1) Press the MAP Softkey (for the PFD Inset Map, select the INSET Softkey). FLIGHT INSTRUMENTS 2) Press the TERRAIN Softkey to display terrain and obstacle data. AUDIO PANEL & CNS EIS When TERRAIN-SVS is selected on maps other than the TERRAIN-SVS Page, an icon to indicate the feature is enabled for display and a legend for TERRAIN-SVS terrain colors are shown (Figure 6-52). Figure 6-52 TERRAIN-SVS Icon and Legend FLIGHT MANAGEMENT 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 a map range larger than the map range setting is selected, the data is removed from the map. HAZARD AVOIDANCE 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. AFCS Maps besides the TERRAIN-SVS 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. ADDITIONAL FEATURES 2) Press the MENU Key. 3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-53). 4) Turn the small FMS Knob to select the ‘Map’ Group and press the ENT Key (Figure 6-54). APPENDICES 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-55). • TERRAIN DATA – Turns the display of terrain data on or off and sets maximum range at which terrain is shown • OBSTACLE DATA – Turns the display of obstacle data on or off 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). INDEX 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. 308 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS Figure 6-53 Navigation Map Page Menu AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 6- 54 Navigation Map Page Setup Menu Figure 6-55 Navigation Map Page Setup Menu, Map Group HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 309 SYSTEM OVERVIEW Hazard Avoidance TERRAIN-SVS Page FLIGHT INSTRUMENTS The TERRAIN-SVS 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. 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 TERRAIN-SVS 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 RANGE Knob from 1 to 200 nm, as indicated by the map range rings (or arcs). EIS Displaying the TERRAIN-SVS Page: 1) Turn the large FMS Knob to select the Map Page Group. AUDIO PANEL & CNS 2) Turn the small FMS Knob to select the TERRAIN-SVS Page. Changing the TERRAIN-SVS Page view: 1) Press the VIEW Softkey. FLIGHT MANAGEMENT 2) Press the 360 or ARC Softkey to select the desired view. Or: 1) Press the MENU Key. 2) Select ‘View 120º’ or ‘View 360º’ (choice dependent on current state) and press the ENT Key to change the view HAZARD AVOIDANCE Showing/hiding aviation information on the TERRAIN-SVS Page: 1) Press the MENU Key. INDEX APPENDICES ADDITIONAL FEATURES AFCS 2) Select ‘Show Aviation Data’ or ‘Hide Aviation Data’ (choice dependent on current state) and press the ENT Key. 310 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW FLIGHT INSTRUMENTS Red Terrain (Warning - Terrain Above or Within 100’ Below the Aircraft Altitude) Yellow Terrain (Caution - Terrain Between 100’ and 1000’ Below the Aircraft Altitude) EIS Black Terrain (Terrain More than 1000’ Below the Aircraft Altitude) Map Range Rings AUDIO PANEL & CNS Terrain Legend Alert Window FLIGHT MANAGEMENT Figure 6-56 TERRAIN-SVS Page Yellow Terrain (Caution - Terrain Between 100’ and 1000’ Below the Aircraft Altitude) HAZARD AVOIDANCE Red Terrain (Warning - Terrain Above or Within 100’ Below the Aircraft Altitude) AFCS Black Terrain (Terrain More than 1000’ Below the Aircraft Altitude) Map Range Arc ADDITIONAL FEATURES Terrain Legend APPENDICES Alert Window Figure 6-57 TERRAIN-SVS Page (ARC View) INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 311 SYSTEM OVERVIEW Hazard Avoidance TERRAIN-SVS Alerts FLIGHT INSTRUMENTS Alerts are issued when flight conditions meet parameters that are set within TERRAIN-SVS software algorithms. TERRAIN-SVS alerts typically employ a CAUTION or a WARNING alert severity level, or both. When an alert is issued, visual annunciations are displayed and aural alerts are simultaneously issued. Table 6-6 shows TERRAIN-SVS alert types with corresponding annunciations and aural messages. EIS When an alert is issued, annunciations appear on the PFD and MFD. The TERRAIN-SVS Alert Annunciation is shown to the upper left of the Altimeter on the PFD and below the Terrain Legend on the MFD. If the TERRAIN-SVS Page is not displayed at the time, a pop-up alert appears on the MFD. To acknowledge the popup alert: • Press the CLR Key (returns to the currently viewed page), or • Press the ENT Key (accesses the TERRAIN-SVS Page) HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS Alert Annunciation Pop-up Alert APPENDICES ADDITIONAL FEATURES AFCS Figure 6-58 TERRAIN-SVS Alert Annunciations Terrain Display Enabled Terrain Legend INDEX Alert Annunciation Figure 6-59 Navigation Map Page (After TERRAIN-SVS Pop-up Alert Acknowledgment) 312 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance MFD Pop-Up Alert SYSTEM OVERVIEW PFD/MFD Alert Annunciation Alert Type Aural Message “Warning; Terrain, Terrain” Imminent Terrain Impact Warning (ITI) “Warning; Terrain, Terrain” Reduced Required Obstacle Clearance Warning (ROC) “Warning; Obstacle, Obstacle” Imminent Obstacle Impact Warning (IOI) “Warning; Obstacle, Obstacle” Imminent Terrain Impact Caution (ITI) “Caution; Terrain, Terrain” Reduced Required Obstacle Clearance Caution (ROC) “Caution; Obstacle, Obstacle” Imminent Obstacle Impact Caution (IOI) “Caution; Obstacle, Obstacle” AUDIO PANEL & CNS “Caution; Terrain, Terrain” EIS Reduced Required Terrain Clearance Caution (RTC) FLIGHT INSTRUMENTS Reduced Required Terrain Clearance Warning (RTC) FLIGHT MANAGEMENT Table 6-6 TERRAIN-SVS Alerts Summary Forward Looking Terrain Avoidance HAZARD AVOIDANCE 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 Table 6-7. When an RTC alert is issued, a potential impact point is displayed on the TERRAIN-SVS Page. AFCS 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 TERRAIN-SVS Page. The alert is annunciated when the projected vertical flight path is calculated to come within minimum clearance altitudes in Table 6-7. ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 313 SYSTEM OVERVIEW Hazard Avoidance Flight Phase FLIGHT INSTRUMENTS Enroute Terminal Approach Departure Minimum Clearance Altitude (ft) Level Flight Descending 700 500 350 300 150 100 100 100 Table 6-7 FLTA Alert Minimum Terrain and Obstacle Clearance Values EIS FLTA alerts are automatically inhibited when the aircraft is below 200 feet AGL while within 0.5 nm of the approach runway or below 125 feet AGL while within 1.0 nm of the runway threshold. FLIGHT MANAGEMENT AUDIO PANEL & CNS PDA and FLTA aural and visual alerts can be manually inhibited. Discretion should be used when inhibiting TERRAIN-SVS and the system should be enabled when appropriate. When TERRAIN-SVS is inhibited, the alert annunciation ‘TER INHB’ is shown on the PFD and MFD (Figure 6-60). Figure 6-60 TERRAIN-SVS Alerting Disabled (TERRAIN-SVS Inhibited) Annunciation Inhibiting/enabling TERRAIN-SVS alerting: HAZARD AVOIDANCE 1) Select the TERRAIN-SVS Page. 2) Press the INHIBIT Softkey to inhibit or enable TERRAIN-SVS (choice dependent on current state). Or: a) Press the MENU Key. AFCS b) Select ‘Inhibit TERRAIN-SVS’ or ‘Enable TERRAIN-SVS’ (choice dependent on current state) and press the ENT Key. INDEX APPENDICES ADDITIONAL FEATURES If TERRAIN-SVS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS 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. 314 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW System Status During power-up, TERRAIN-SVS conducts a self-test of its aural and visual annunciations. An aural alert is issued at test completion. PFD/MFD Alert Annunciation Aural Message None System Test in Progress System Test Pass FLIGHT INSTRUMENTS Alert Type None “Terrain System Test OK” “Terrain System Failure” Terrain System Test Fail EIS Table 6-8 TERRAIN-SVS System Test Status Annunciations AUDIO PANEL & CNS TERRAIN-SVS continually monitors several system-critical items such as database validity, hardware status, and GPS status. If the terrain/obstacle database is not available, the aural message “Terrain System Failure” is generated along with the ‘TER FAIL’ alert annunciation. PFD/MFD Alert Annunciation No GPS position Excessively degraded GPS signal GPS signal re-established Aural Message HAZARD AVOIDANCE Alert Type FLIGHT MANAGEMENT TERRAIN-SVS 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 ‘TER N/A’ is generated in the annunciation window and on the TERRAIN-SVS Page. The aural message “Terrain System Not Available” is generated. When the GPS signal is re-established and the aircraft is within the database coverage area, the aural message “Terrain System Available” is generated. “Terrain System Not Available” None “Terrain System Available” AFCS Table 6-9 TERRAIN-SVS Status Annunciations ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 315 SYSTEM OVERVIEW Hazard Avoidance 6.5 Traffic Information Service (TIS) FLIGHT INSTRUMENTS WARNING: The Traffic Information Service (TIS) is intended for advisory use only. TIS is intended to help the pilot locate traffic visually. It is the responsibility of the pilot to see and maneuver to avoid traffic. NOTE: TIS is available only when the aircraft is within the service volume of a TIS-capable terminal radar EIS site. Aircraft without an operating transponder are invisible to both Traffic Advisory Systems (TAS) and TIS. Aircraft without altitude reporting capability are shown without altitude separation data or climb descent indication. AUDIO PANEL & CNS NOTE: TIS is disabled if a Traffic Advisory System (TAS) is installed. FLIGHT MANAGEMENT Traffic Information Service (TIS) is designed to help 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 is updated every 5 seconds. The G1000 displays up to eight traffic targets within a 7.5-nm radius, from 3000 feet below to 3500 feet above the requesting aircraft. Traffic is displayed according to TCAS symbology (Table 6-10). TIS Symbol Description Non-Threat Traffic HAZARD AVOIDANCE Traffic Advisory (TA) Traffic Advisory Off Scale AFCS Table 6-10 TIS Traffic Symbols ADDITIONAL FEATURES 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 is generated. A TA which is detected, but is outside the range of the map, is indicated with a message in the lower left corner of the map and a half TA symbol at the relative bearing of the intruder. APPENDICES 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 6-55) or in a banner at the lower left corner of maps other than the Traffic Map Page on which traffic can be displayed. INDEX 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 an up/down arrow (for speeds greater than 500 fpm 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. 316 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW Displaying TRAFFIC Data Traffic information can be displayed on the following maps (when TIS is operating): • Trip Planning Page • Navigation Map Page • Nearest Pages • Traffic Map Page • Active Flight Plan Page FLIGHT INSTRUMENTS • PFD Inset Map Displaying traffic information (maps other than the Traffic Map Page): EIS 1) Press the MAP Softkey. 2) Press the TRAFFIC Softkey. AUDIO PANEL & CNS When traffic is selected on maps other than the Traffic Map Page, an icon is shown to indicate the feature is enabled for display. FLIGHT MANAGEMENT Traffic Advisory HAZARD AVOIDANCE AFCS Traffic Display Enabled Traffic Status Banner ADDITIONAL FEATURES Figure 6-61 TIS Traffic on the Navigation Map Page Displaying traffic information (PFD Inset Map): APPENDICES 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. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX 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 317 SYSTEM OVERVIEW Hazard Avoidance is removed from the map. Maps besides the Traffic Map Page use settings based on those selected for the Navigation Map Page. FLIGHT INSTRUMENTS 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 6-62). 4) Turn the small FMS Knob to select the ‘Traffic’ Group and press the ENT Key (Figure 6-63). EIS 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-64). • TRAFFIC – Turns the display of traffic data on or off AUDIO PANEL & CNS • TRAFFIC MODE – Selects the traffic mode for display; select from: - All Traffic - Displays all traffic - TA/PA - Displays Traffic Alerts and Proximity Advisories - TA ONLY - Displays Traffic Alerts only FLIGHT MANAGEMENT • 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.). HAZARD AVOIDANCE 7) Press the ENT Key to select an option. INDEX APPENDICES ADDITIONAL FEATURES AFCS 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. 318 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW FLIGHT INSTRUMENTS Figure 6-62 Navigation Map Page Menu EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 6-63 Navigation Map Page Setup Menu Figure 6-64 Navigation Map Page Setup Menu, Traffic Group HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 319 SYSTEM OVERVIEW Hazard Avoidance Traffic Map Page FLIGHT INSTRUMENTS 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. Aircraft orientation on this map is always heading up unless there is no valid heading. Map range is adjustable with the RANGE Knob from 2 to 12 nm, as indicated by the map range rings. EIS 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 G1000 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. AUDIO PANEL & CNS 2) Turn the small FMS Knob to select the Traffic Map Page. 3) Confirm TIS is in Operating Mode: Press the OPERATE Softkey to begin displaying traffic. FLIGHT MANAGEMENT Or: a) Press the MENU Key. b) Select ‘Operate Mode’ (shown if TIS is in Standby Mode) and press the ENT Key. HAZARD AVOIDANCE Traffic Mode Annunciation “TIS Not Available” Voice Alert Status Non-Threat Traffic1200’ Above, Descending ADDITIONAL FEATURES AFCS “Non-Bearing” Traffic (System Unable to Determine Bearing) Distance is 8.0 nm, 1100’ Above, Descending Range Marking Rings APPENDICES Traffic Advisory 400’ Below, Climbing Traffic Status Banner INDEX Figure 6-65 Traffic Map Page Select to Mute “TIS Not Available” Voice Alert 320 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS • 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. EIS 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. AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Inset Map Displays When TA is Detected Figure 6-66 Traffic Annunciation (PFD) AFCS A “Traffic Not Available” (TNA) voice alert is generated when the TIS service becomes unavailable or is out of range. TIS may be unavailable in the radar coverage area due to the following: ADDITIONAL FEATURES • 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. APPENDICES • 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. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX The “Traffic 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. 321 SYSTEM OVERVIEW Hazard Avoidance Muting the “Traffic Not Available” voice alert: 1) Select the Traffic Map Page. FLIGHT INSTRUMENTS 2) Press 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. EIS System Status AUDIO PANEL & CNS The G1000 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, an annunciation is shown in the center of the Traffic Map Page. Traffic Map Page Annunciation NO DATA FLIGHT MANAGEMENT DATA FAILED FAILED 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 HAZARD AVOIDANCE Description TIS is unavailable or out of range * Contact a service center or Garmin dealer for corrective action INDEX APPENDICES ADDITIONAL FEATURES AFCS Table 6-11 TIS Failure Annunciations 322 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW FLIGHT INSTRUMENTS System Test has Failed EIS Data Not Received from Transponder AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 6-67 TIS Power-up Test Failure Traffic Mode Annunciation (Traffic Map Page) TIS Operating OPERATING STANDBY (also shown in white in center of page) TIS Failed* FAIL ADDITIONAL FEATURES TIS Standby Traffic Display Enabled Icon (Other Maps) AFCS Mode HAZARD AVOIDANCE 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. APPENDICES * See Table 6-13 for additional failure annunciations Table 6-12 TIS Modes INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 323 SYSTEM OVERVIEW Hazard Avoidance Switching between TIS modes: 1) Select the Traffic Map Page. FLIGHT INSTRUMENTS 2) Press 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. AUDIO PANEL & CNS Traffic Status Banner Annunciation FLIGHT MANAGEMENT EIS 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 6-13). TA X.X ± XX ↕ TA OFF SCALE HAZARD AVOIDANCE AGE MM:SS TRFC COAST AFCS TRFC RMVD ADDITIONAL FEATURES 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 data 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 INDEX APPENDICES Table 6-13 TIS Traffic Status Annunciations 324 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW 6.6 AVIDYNE TAS600 (Optional) FLIGHT INSTRUMENTS WARNING: The Traffic Advisory System (TAS) is intended for advisory use only. TAS is intended to help the pilot locate traffic visually. It is the responsibility of the pilot to see and maneuver to avoid traffic. NOTE: Refer to the Avidyne TAS600 Series Pilot’s Guide for a detailed discussion of the Avidyne TAS600. EIS NOTE: TIS is disabled if a traffic advisory system (TAS) is installed. TAS Symbology TAS Symbol AUDIO PANEL & CNS Traffic Advisory System (TAS) is designed to help in detection and avoidance of other aircraft. TAS uses an onboard interrogator-processor and the Mode S transponder for the air-to-air traffic data link. Traffic is displayed according to TCAS symbology using four different symbols. Description FLIGHT MANAGEMENT Non-Threat Traffic Proximity Advisory (PA) HAZARD AVOIDANCE Traffic Advisory (TA) Traffic Advisory Off Scale AFCS Table 6-14 TAS Symbol Description A Non-threat 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. ADDITIONAL FEATURES A Proximity Advisory indicates that the intruding aircraft is within ±1200 feet and is within 5 nm range, but is still not considered a threat. APPENDICES A Traffic Advisory (TA) alerts the crew to a potentially hazardous intruding aircraft. Closing rate, distance, and vertical separation meet TA criteria. 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. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 325 SYSTEM OVERVIEW Hazard Avoidance Displaying Traffic Data FLIGHT INSTRUMENTS Traffic information is displayed on the following maps: • PFD Inset Map • Trip Planning Page • Navigation Map Page • Nearest Pages • Traffic Map Page • Active Flight Plan Page Displaying traffic on the Traffic Map Page: EIS 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. AUDIO PANEL & CNS 3) Turn the RANGE Knob clockwise to display a larger area or counter-clockwise to display a smaller area. Operating Mode Altitude Mode FLIGHT MANAGEMENT Traffic Display Range HAZARD AVOIDANCE Off Scale Traffic, 200’ Above, Descending ADDITIONAL FEATURES “Non-Bearing” Traffic (Bearing Undetermined), Distance 8.0 nm, 1100’ Above, Descending AFCS Traffic Advisory, Aircraft is 400’ Below, Climbing Proximity Advisory, 1000’ Above, Descending Figure 6-68 Traffic Map Page APPENDICES The Traffic Map Page shows surrounding TAS traffic data in relation to the aircraft’s current position and altitude, without basemap clutter. Aircraft orientation is always heading up unless there is no valid heading. Map range is adjustable with the RANGE Knob from 2 to 24 nm, as indicated by the map range rings. The traffic mode and altitude display mode are annunciated in the upper left corner. Displaying traffic information (maps other than the Traffic Map Page): 1) Select the MAP Softkey. INDEX 2) Select the TRAFFIC Softkey to display traffic data. 326 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW When traffic is selected on maps other than the Traffic Map Page, a traffic icon is shown to indicate TAS is enabled for display. FLIGHT INSTRUMENTS Traffic Advisory Proximity Traffic EIS AUDIO PANEL & CNS Non-Threat Traffic TA Off Scale Banner FLIGHT MANAGEMENT Non-Bearing Traffic Advisories Figure 6-69 TAS Traffic on Navigation Map HAZARD AVOIDANCE Displaying traffic information (PFD Inset Map): 1) Select the INSET Softkey. 2) Select the TRAFFIC Softkey to display traffic data on the inset map (TRFC-1). 3) Select the softkey again to display the traffic-only inset (TRFC-2). AFCS 4) Select the softkey again to remove traffic data. ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 327 SYSTEM OVERVIEW Hazard Avoidance Altitude Display FLIGHT INSTRUMENTS The Pilot can select the volume of airspace in which traffic is displayed. Traffic Advisories (TAs) outside of these limits will still be shown. Refer to the TAS600 Series Pilot’s Guide for specific display thresholds. Changing the altitude display mode: 1) On the Traffic Page, select the ALT MODE Softkey. AUDIO PANEL & CNS EIS 2) Select one of the following Softkeys: • BELOW • NORMAL • ABOVE • UNREST (unrestricted) 3) To return to the Traffic Page, select the BACK Softkey. Or: 1) Press the MENU Key. HAZARD AVOIDANCE FLIGHT MANAGEMENT 2) Turn the small FMS Knob to select one of the following: • BELOW • NORMAL • ABOVE • UNREST (unrestricted) 3) Select the ENT Softkey. Traffic Map Page Display Range AFCS The display range on the Traffic Map Page can be changed at any time. Map range is adjustable with the RANGE Knob from 2 to 24 nm, as indicated by the map range rings. Changing the display range on the Traffic Page: ADDITIONAL FEATURES 1) Turn the RANGE Knob. APPENDICES 2) The following range options are available: • 2 nm • 2 and 6 nm • 6 and 12 nm • 12 and 24 nm INDEX 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. 328 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW Customizing the traffic display on the Navigation Map Page: 1) Select the Navigation Map Page. 2) Press the MENU Key. FLIGHT INSTRUMENTS 3) With Map Setup highlighted, press the ENT Key (Figure 6-70). 4) Turn the small FMS Knob to select the Traffic Group and press the ENT Key (Figure 6-71). 5) Turn the large FMS Knob or press the ENT Key to scroll through the selections (Figure 6-72). • TRAFFIC – Turns the display of traffic data on or off - All Traffic - Displays all traffic - TA/PA - Displays Traffic Alerts and Proximity Advisories - TA ONLY - Displays Traffic Alerts only AUDIO PANEL & CNS EIS • TRAFFIC MODE – Selects the traffic mode for display; select from: • 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 FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE AFCS Figure 6-70 Navigation Map Page Menu ADDITIONAL FEATURES APPENDICES Figure 6-71 Navigation Map Page Setup Menu Figure 6-72 Navigation Map Page Setup Menu, Traffic Group INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 329 SYSTEM OVERVIEW Hazard Avoidance TAS Alerts FLIGHT INSTRUMENTS NOTE: Refer to the TAS600 documentation for information on alerts generated by the TAS equipment. When the number of TAs on the Traffic Map Page increases from one scan to the next, the following occur: • A “Traffic” voice alert is generated followed by the clock position, relative altitude and range of the TA. • A TRAFFIC Annunciation appears at the top right of the airspeed on the PFD, flashing for 5 seconds and remaining displayed until no TAs are detected in the area. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS • The PFD Inset Map is automatically displayed with TA traffic. HAZARD AVOIDANCE Inset Map Displays When TA is Detected Figure 6-73 Traffic Annunciation (PFD) TAS Voice Alerts AFCS To listen to an update of Traffic Advisories select the MUTE Softkey twice. Muting the TAS voice alert in progress: 1) Select the Traffic Map Page. INDEX APPENDICES ADDITIONAL FEATURES 2) Select the MUTE Softkey while the voice alert is playing. Subsequent voice alerts will be heard. 330 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Hazard Avoidance SYSTEM OVERVIEW System Status NOTE: Refer to the TAS600 documentation for information on the operating mode. FLIGHT INSTRUMENTS The traffic mode is annunciated in the upper left corner of the Traffic Map Page. Traffic Mode Annunciation (Traffic Map Page) Mode Traffic Display Enabled Icon (Other Maps) OPERATING TAS Operating EIS FAIL TAS Failed* AUDIO PANEL & CNS * See Table 6-17 for additional failure annunciations Table 6-15 TAS Modes If the unit fails, an annunciation as to the cause of the failure is shown in the center of the Traffic Map Page. FAILED Description Data is not being received from the TAS unit Data is being received from the TAS unit, but the unit is self-reporting a failure Incorrect data format received from the TAS unit HAZARD AVOIDANCE DATA FAILED FLIGHT MANAGEMENT Traffic Map Page Annunciation NO DATA Table 6-16 TAS Failure Annunciations AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 331 SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS Traffic Status Banner Annunciation EIS TA OFF SCALE AUDIO PANEL & CNS TA X.X ± XX ↕ TRFC FAIL NO TRFC 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) TAS unit has failed (unit is self-reporting a failure or sending incorrectly formatted data) Data is not being received from the TAS unit FLIGHT MANAGEMENT *Shown as symbol on Traffic Map Page **Shown in center of Traffic Map Page INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Table 6-17 TAS Traffic Status Annunciations 332 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW Section 7 Automatic Flight Control System FLIGHT INSTRUMENTS Note: The approved Aircraft Flight Manual Supplement (AFMS) always supersedes the information in this Pilot’s Guide. Note: A failure of the primary (#1) Integrated Avionics Unit (IAU) results in loss of the flight director. Any IAU failure results in loss of the autopilot and manual electric trim. • GSA 80 AFCS Yaw Damper Servo (1) • GDU 1045 Multi-Function Display (MFD) • GSA 81 AFCS Servo (3) • GIA 63W Integrated Avionics Units (2) • GSM 85 Servo Mounts (4) AUDIO PANEL & CNS • GDU 1040 Primary Flight Display (PFD) EIS The GFC 700 is a digital Automatic Flight Control System (AFCS), fully integrated within the G1000 System avionics architecture. The System Overview section provides a block diagram (Figure 1-1) to support this system description. GFC 700 AFCS functionality in Diamond DA42NG aircraft is distributed across the following Line Replaceable Units (LRUs): FLIGHT MANAGEMENT The GFC 700 AFCS can be divided into these main operating functions: • Flight Director (FD) — Flight director operation takes place within the primary (#1) IAU. Flight director commands are displayed on the PFD. The flight director provides: – Command Bars showing pitch/roll guidance HAZARD AVOIDANCE – Pitch/roll mode selection and processing – Autopilot communication AFCS • Autopilot (AP) — Autopilot operation occurs within the pitch, roll, and pitch trim servo and provides servo monitoring and automatic flight control in response to flight director steering commands, AHRS attitude and rate information, and airspeed. • Yaw Damper (YD) — The yaw servo is self-monitoring and provides Dutch roll damping and turn coordination in response to yaw rate, roll angle, vertical acceleration, and airspeed. ADDITIONAL FEATURES • Manual Electric Trim (MET) — The pitch trim servo provides manual electric trim capability when the autopilot is not engaged. APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 333 SYSTEM OVERVIEW Automatic Flight Control System 7.1 AFCS Controls FLIGHT INSTRUMENTS The following dedicated AFCS keys are located on the bezel of the MFD: AP Key FD Key Engages/disengages the autopilot 2 Activates/deactivates the flight director only Pressing once turns on the flight director in the default pitch and roll modes. Pressing again deactivates the flight director and removes the Command Bars. If the autopilot is engaged, the key is disabled. 3 NAV Key Selects/deselects Navigation Mode 4 ALT Key Selects/deselects Altitude Hold Mode 5 VS Key Selects/deselects Vertical Speed Mode 6 FLC Key Selects/deselects Flight Level Change Mode 7 YD Key Engages/disengages the yaw damper 8 HDG Key Selects/deselects Heading Select Mode 9 APR Key Selects/deselects Approach Mode 10 VNV Key Selects/deselects Vertical Path Tracking Mode for Vertical Navigation flight control 11 NOSE UP/NOSE Control the mode reference in Pitch Hold, Vertical Speed, and Flight Level Change modes DN Keys FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 1 AFCS HAZARD AVOIDANCE 1045 1 7 2 8 3 9 4 10 5 ADDITIONAL FEATURES 11 6 INDEX APPENDICES Figure 7-1 Dedicated MFD AFCS Controls 334 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW The following AFCS controls are located in the cockpit separately from the MFD: AP DISC Switch (Autopilot Disconnect) Disengages the autopilot and interrupts pitch trim operation FLIGHT INSTRUMENTS This switch may be used to mute the aural autopilot disconnect alert. The AP DISC Switch is located on each control stick. While pressed, allows manual control of the aircraft while the autopilot is CWS Button (Control Wheel Steering) engaged and synchronizes the flight director’s Command Bars with the current aircraft pitch (if not in Glideslope Mode) and roll (if in Roll Hold Mode) EIS Upon release of the CWS Button, the flight director may establish new reference points, depending on the current pitch and roll modes. CWS operation details are discussed in the flight director modes section. GA Button (Go Around) AUDIO PANEL & CNS The CWS Button is located on the top of the left control stick. Disengages the autopilot and selects flight director Go Around Mode FLIGHT MANAGEMENT If an approach procedure is loaded 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. The GA Button is located on the left throttle handle. AP TRIM Switch (Autopilot Trim) Used to command manual electric trim (MET) HAZARD AVOIDANCE 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. The AP TRIM ARM switch can be used to disengage the autopilot and to acknowledge an autopilot disconnect alert and mute the associated aural tone. AFCS Manual trim commands are generated only when both sides of the switch are operated simultaneously. If either side of the switch is active separately for more than three seconds, MET function is disabled and ‘PTRM’ is displayed as the AFCS Status Annunciation on the PFD. The function remains disabled until both sides of the switch are inactivated. ADDITIONAL FEATURES The AP TRIM Switch is located on the left control stick. APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 335 SYSTEM OVERVIEW Automatic Flight Control System 7.2 Flight Director Operation FLIGHT INSTRUMENTS The flight director function provides pitch and roll commands to the AFCS and displays them on the PFD. With the flight director activated, the aircraft can be hand-flown to follow the path shown by the Command Bars. Maximum commanded pitch (-15°/+20°) and roll (22°) 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 EIS An initial press of a key listed in Table 7-1 (when the flight director is not active) activates the flight director in the listed modes. The flight director may be turned off and the Command Bars removed from the display by pressing the FD Key again. The FD Key is disabled when the autopilot is engaged. AUDIO PANEL & CNS Control Pressed ALT Key VS Key VNV Key Lateral Roll Hold (default) Roll Hold (default) Roll Hold (default) Takeoff (on ground) Go Around (in air) Roll Hold (default) Roll Hold (default) Roll Hold (default) NAV Key Navigation** APR Key Approach** HDG Key Heading Select FLIGHT MANAGEMENT FD Key AP Key CWS Button AFCS HAZARD AVOIDANCE GA Button ADDITIONAL FEATURES Modes Selected ROL ROL ROL TO GA ROL ROL ROL GPS VOR LOC BC GPS VOR LOC HDG Vertical Pitch Hold (default) PIT Pitch Hold (default) PIT Pitch Hold (default) PIT Takeoff (on ground) TO Go Around (in air) GA Altitude Hold ALT Vertical Speed VS Vertical Path Tracking* VPTH Pitch Hold (default) PIT Pitch Hold (default) PIT Pitch Hold (default) PIT *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. INDEX APPENDICES Table 7-1 Flight Director Activation 336 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW AFCS Status Box Lateral Modes Active Vertical Modes Active Mode Reference EIS Armed Yaw Autopilot Damper Status Status FLIGHT INSTRUMENTS Flight director mode annunciations are displayed on the PFD when the flight director is active. Autopilot status is displayed 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 annunciated in white and active in green. Armed AFCS Status Box AUDIO PANEL & CNS Selected Altitude FLIGHT MANAGEMENT Command Bars HAZARD AVOIDANCE GPS is Selected Navigation Source AFCS Figure 7-2 PFD AFCS Display ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 337 SYSTEM OVERVIEW Automatic Flight Control System Command Bars FLIGHT INSTRUMENTS Upon activation of the flight director, Command Bars are displayed on the PFD as a single magenta cue. The Command Bars move together vertically to indicate pitch commands and bank left or right to indicate roll commands. The Command Bars do not override the aircraft symbol. If the attitude information 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 either pitch exceeds +30˚/-20˚ or bank exceeds 65˚. EIS Command Bars AUDIO PANEL & CNS Aircraft Symbol Figure 7-3 Command Bars FLIGHT MANAGEMENT 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 mode(s). HAZARD AVOIDANCE Armed modes are annunciated in white and active in green 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 green active mode field and flashing for 10 seconds. ADDITIONAL FEATURES AFCS 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 and annunciator light indicate loss of sensor (ADC) or navigation data (VOR, LOC, GPS, VNV, WAAS) 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. If after 10 seconds no action is taken, the flashing annunciation stops. APPENDICES Figure 7-4 Loss of VOR Signal INDEX The flight director is automatically disabled if the attitude information required to compute the default flight director modes becomes invalid or unavailable. 338 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW 7.3 Vertical Modes Pitch Hold Flight Level Change VNV Target Altitude Capture Glidepath*** -15° to +20° 0.5° nnnn fpm -3000 to +1500 fpm 100 fpm nnn kt 90 to 180 kt 1 kt PIT * ALTS ALT Key ALT nnnnn ft VS Key VS FLC Key FLC VNV Key VPTH ** ALTV APR Key GA Button GP GS GA 6° ADDITIONAL FEATURES Go Around (default) AFCS Glideslope Reference Change Increment HAZARD AVOIDANCE Vertical Path Tracking Reference Range FLIGHT MANAGEMENT Vertical Speed Holds aircraft pitch attitude; may be used to climb/descend to the Selected Altitude Captures the Selected Altitude Holds current Altitude Reference Holds aircraft vertical speed; may be used to climb/descend to the Selected Altitude Holds aircraft airspeed while aircraft is climbing/descending to the Selected Altitude Captures and tracks descent legs of an active vertical profile Captures the Vertical Navigation (VNV) Target Altitude Captures and tracks the WAAS glidepath on approach Captures and tracks the ILS glideslope on approach Disengages the autopilot and commands a constant pitch angle and wings level Control Annunciation AUDIO PANEL & CNS Selected Altitude Capture Altitude Hold Description EIS Vertical Mode FLIGHT INSTRUMENTS Table 7-2 lists the 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 NOSE UP/NOSE DN Keys can be used to change the vertical mode reference while operating under Pitch Hold, Vertical Speed, or Flight Level Change Mode. Increments of change and acceptable ranges of values for each of these references using the NOSE UP/NOSE DN Keys are also listed in the table. * ALTS is armed automatically when PIT, VS, FLC, or GA is active, and under VPTH when the Selected Altitude is to be captured instead of the VNV Target Altitude. APPENDICES ** ALTV is armed automatically under VPTH when the VNV Target Altitude is to be captured instead of the Selected Altitude. ***GP is available in installations with GIA 63W IAUs when WAAS is available. Table 7-2 Flight Director Vertical Modes INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 339 SYSTEM OVERVIEW Automatic Flight Control System Pitch Hold Mode (PIT) FLIGHT INSTRUMENTS When the flight director is activated (the FD Key is pressed), Pitch Hold Mode is selected by default. Pitch Hold Mode is indicated as the active pitch mode by the green annunciation ‘PIT’. 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. EIS 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 AUDIO PANEL & CNS When operating in Pitch Hold Mode, the pitch reference can be adjusted by: • Using the NOSE UP/NOSE DN Keys • Pressing the CWS Button, hand-flying the aircraft to establish a new pitch reference, then releasing the CWS Button FLIGHT MANAGEMENT Pitch Hold Mode Active Selected Altitude Capture Mode Armed ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Selected Altitude Command Bars Maintain Desired Pitch Reference INDEX APPENDICES Figure 7-5 Pitch Hold Mode 340 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW Selected Altitude Capture Mode (ALTS) Selected Altitude Capture Mode is automatically armed with activation of the following modes: • Go Around • Vertical Speed • Vertical Path Tracking (if the Selected Altitude is to be captured instead of the VNV Target Altitude) • Flight Level Change FLIGHT INSTRUMENTS • Pitch Hold The white ‘ALTS’ annunciation indicates Selected Altitude Capture Mode is armed (see Figure 7-5 for example). The ALT Knob is used to set the Selected Altitude (shown above the Altimeter) until Selected Altitude Capture Mode becomes active. EIS AUDIO PANEL & CNS As the aircraft nears the Selected Altitude, the flight director automatically transitions to Selected Altitude Capture Mode with Altitude Hold Mode armed (Figure 7-6). This automatic transition is indicated by the green ‘ALTS’ annunciation flashing for up to 10 seconds and the appearance of the white ‘ALT” annunciation. The Selected Altitude is shown as the Altitude Reference beside the ‘ALTS’ annunciation. FLIGHT MANAGEMENT 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 (shown as the Altitude Reference). As Altitude Hold Mode becomes active, the white ‘ALT’ annunciation moves to the active pitch mode field and flashes green for 10 seconds to indicate the automatic transition. Altitude Reference (in this case, equal to Selected Altitude) HAZARD AVOIDANCE Flash up to 10 sec, Indicating Automatic Transition Figure 7-6 Automatic Mode Transitions During Altitude Capture AFCS Changing the Selected Altitude ADDITIONAL FEATURES NOTE: Pressing the CWS Button while in Selected Altitude Capture Mode does not cancel the mode. Use of the ALT 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. APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 341 SYSTEM OVERVIEW Automatic Flight Control System Altitude Hold Mode (ALT) FLIGHT INSTRUMENTS Altitude Hold Mode can be activated by pressing the ALT Key; the flight director maintains the current aircraft altitude (to the nearest 10 feet) as the Altitude Reference. The flight director’s Altitude Reference, shown in the AFCS Status Box, is independent of the Selected Altitude, displayed above the Altimeter. Altitude Hold Mode active is indicated by a green ‘ALT’ annunciation in the AFCS Status Box. Altitude Hold Mode is automatically armed when the flight director is in Selected Altitude Capture Mode (see Figure 7-6). Selected Altitude Capture Mode automatically transitions to Altitude Hold Mode when the altitude error is less than 50 feet. In this case, the Selected Altitude becomes the flight director’s Altitude Reference. EIS Changing the Altitude Reference NOTE: Turning the ALT Knob while in Altitude Hold Mode changes the Selected Altitude, but not the flight AUDIO PANEL & CNS director’s Altitude Reference, and does not cancel the mode. With the CWS Button depressed, 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. FLIGHT MANAGEMENT Altitude Hold Mode Active Altitude Reference HAZARD AVOIDANCE Selected Altitude ADDITIONAL FEATURES AFCS Selected Altitude Bug Command Bars Hold Pitch Attitude to Maintain Altitude Reference INDEX APPENDICES Figure 7-7 Altitude Hold Mode 342 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW Vertical Speed Mode (VS) FLIGHT INSTRUMENTS In Vertical Speed Mode, the flight director acquires and maintains a Vertical Speed Reference. 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 along with the Vertical Speed Reference. The Vertical Speed Reference is also displayed above the Vertical Speed Indicator. A Vertical Speed Reference Bug corresponding to the Vertical Speed Reference is shown on the indicator. EIS Changing the Vertical Speed Reference AUDIO PANEL & CNS The Vertical Speed Reference (shown both in the AFCS Status Box and above the Vertical Speed Indicator) may be changed by: • Using the NOSE UP/NOSE DN Keys • Pressing the CWS Button, hand-flying the aircraft to attain a new Vertical Speed Reference, then releasing the CWS Button Vertical Speed Reference FLIGHT MANAGEMENT Vertical Speed Mode Active Selected Altitude Capture Mode Armed HAZARD AVOIDANCE Selected Altitude Vertical Speed Reference AFCS ADDITIONAL FEATURES Vertical Speed Reference Bug Command Bars Indicate Climb to Attain Vertical Speed Reference APPENDICES Figure 7-8 Vertical Speed Hold Mode INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 343 SYSTEM OVERVIEW Flight Level Change Mode (FLC) FLIGHT INSTRUMENTS Flight Level Change Mode is selected by pressing the FLC Key. This mode acquires and maintains the Airspeed Reference 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, and altitude. EIS Automatic Flight Control System The Airspeed Reference is set to the current airspeed upon mode activation. Flight Level Change Mode is indicated by a green ‘FLC’ annunciation beside the Airspeed Reference in the AFCS Status Box. The Airspeed Reference is also displayed directly above the Airspeed Indicator, along with a bug corresponding to the Airspeed Reference along the tape. NOTE: The Selected Altitude should be set before selecting Flight Level Change Mode. AUDIO PANEL & CNS 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 MANAGEMENT Changing the Airspeed Reference The Airspeed Reference (shown in both the AFCS Status Box and above the Airspeed Indicator) may be adjusted by: • Using the NOSE UP/NOSE DN Keys HAZARD AVOIDANCE • Pressing the CWS Button, hand-flying the aircraft to a new airspeed, then releasing the CWS Button to establish the new Airspeed Reference Selected Airspeed Altitude Capture Reference Mode Armed AFCS Flight Level Change Mode Active ADDITIONAL FEATURES Airspeed Reference APPENDICES Airspeed Reference Bug INDEX Command Bars Indicate Climb to Attain Selected Altitude Figure 7-9 Flight Level Change Mode (IAS) 344 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW Vertical Navigation Modes (VPTH, ALTV) Note: VNV is disabled when parallel track or dead reckoning mode is active. FLIGHT INSTRUMENTS 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 any time that VNV flight planning is available. Refer to the Flight Management Section for more information on VNV flight plans. Conditions for availability include, but are not limited to: EIS • The selected navigation source is GPS. • A VNV flight plan (with at least one altitude-constrained waypoint) or vertical direct-to is active. AUDIO PANEL & CNS • 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. FLIGHT MANAGEMENT HAZARD AVOIDANCE 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 vertical direct-to. 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 pitch mode key is pressed while Vertical Path Tracking Mode is selected, Vertical Path AFCS Tracking Mode reverts to armed. NOTE: Pressing the CWS Button while Vertical Path Tracking Mode is active does not cancel the mode. The ADDITIONAL FEATURES autopilot guides the aircraft back to the descent path upon release of the CWS Button. APPENDICES 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. INDEX Figure 7-10 Vertical Path Tracking Armed Annunciations 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 345 SYSTEM OVERVIEW 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 5 minutes of descent path interception by: FLIGHT INSTRUMENTS • Pressing the VNV Key • Adjusting the Selected Altitude EIS If acknowledgment is not received within 1 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. AUDIO PANEL & CNS In conjunction with the “TOD [top of descent] within 1 minute” annunciation in the Navigation Status Box and the “Vertical track” voice message, VNV indications (VNV Target Altitude, vertical deviation, and vertical speed required) appear on the PFD in magenta (Figure 7-11). FLIGHT MANAGEMENT Altitude Hold Mode Active Vertical Path Tracking Armed, (Flashing Indicates Acknowledgment Required) HAZARD AVOIDANCE Selected Altitude Below VNV Target VNV Target Altitude AFCS Vertical Deviation Indicator Required Vertical Speed Bug ADDITIONAL FEATURES GPS is Selected Navigation Source Terminal Phase of Flight INDEX APPENDICES Figure 7-11 Vertical Path Capture 346 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW When a descent leg is captured (i.e., vertical deviation becomes valid), Vertical Path Tracking becomes active and tracks the descent profile. An altitude capture mode (‘ALTS’ or ‘ALTV’) is armed as appropriate. VNV Target Altitude Capture Armed FLIGHT INSTRUMENTS Vertical Path Tracking Active VNV Target Altitude EIS Terminal Phase of Flight Command Bars Indicate Descent to Maintain Required Vertical Speed FLIGHT MANAGEMENT GPS is Selected Navigation Source AUDIO PANEL & CNS Required Vertical Speed Indication (RVSI) Vertical Deviation Indicator (VDI) HAZARD AVOIDANCE Figure 7-12 Vertical Path Tracking Mode AFCS If the Altimeter’s 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. ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 347 SYSTEM OVERVIEW Automatic Reversion to Pitch Hold Mode FLIGHT INSTRUMENTS Automatic Flight Control System • Vertical deviation exceeds 200 feet during an overspeed condition. Several situations can occur while Vertical Path Tracking Mode is active which cause the flight director to revert to Pitch Hold Mode: • Vertical deviation experiences a discontinuity 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). EIS • A display enters Reversionary Mode (this does not apply to an active vertical direct-to). AUDIO PANEL & CNS 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 FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE Figure 7-13 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 INDEX APPENDICES ADDITIONAL FEATURES AFCS Pressing the VNV Key twice re-arms Vertical Path Tracking for immediate profile re-capture. 348 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW VNV Target Altitude Capture Mode (ALTV) Note: Armed VNV Target Altitude and Selected Altitude capture modes are mutually exclusive. However, FLIGHT INSTRUMENTS Selected Altitude Capture Mode is armed implicitly (not annunciated) whenever VNV Target Altitude Capture Mode is armed. EIS 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 vertical direct-to, 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 7-11). AUDIO PANEL & CNS 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 green ‘ALTV’ annunciation flashing for up to 10 seconds and the appearance of the white ‘ALT’ annunciation. The VNV Target Altitude is shown as the Altitude Reference beside the ‘ALTV’ annunciation and remains displayed above the Vertical Speed Indicator. The Required Vertical Speed Indication (RVSI) is removed once VNV Target Altitude Capture Mode becomes active. FLIGHT MANAGEMENT HAZARD AVOIDANCE 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 green for 10 seconds to indicate the automatic transition. The flight director automatically arms Vertical Path Tracking, allowing upcoming descent legs to be captured and subsequently tracked. Altitude Reference (In This Case, Equal To VNV Altitude Target) AFCS Flash up to 10 sec, Indicating Automatic Transition ADDITIONAL FEATURES Figure 7-14 Automatic Mode Transitions During Altitude Capture Changing the VNV Target Altitude APPENDICES NOTE: Pressing the CWS Button while in VNV Target Altitude Capture Mode does not cancel the mode. INDEX 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). 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 349 SYSTEM OVERVIEW Automatic Flight Control System Glidepath Mode (GP) (WAAS only) FLIGHT INSTRUMENTS NOTE: Refer to the Aircraft Flight Manual (AFM) to determine whether WAAS functionality is approved. 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. EIS Glidepath Mode is available only in installations with GIA 63W IAUs when WAAS is available. Glidepath Mode is used to track the WAAS-based glidepath. When Glidepath Mode is armed, ‘GP’ is annunciated in white in the AFCS Status Box. Selecting Glidepath Mode: AUDIO PANEL & CNS 1) Ensure a GPS approach with vertical guidance (LPV, LNAV/VNAV, LNAV+V) 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). FLIGHT MANAGEMENT NOTE: Some RNAV (GPS) approaches provide a vertical descent angle as an aid in flying a stabilized HAZARD AVOIDANCE 3) Press the APR Key. WARNING: When flying an LNAV approach (with vertical descent angle) with the autopilot coupled, the 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. aircraft will not level off at the MDA even if the MDA is set in the altitude preselect. AFCS Upon reaching the glidepath, the flight director transitions to Glidepath Mode and begins to capture and track the glidepath. Figure 7-15 Glidepath Mode Armed Once the following conditions have been met, the glidepath can be captured: ADDITIONAL FEATURES • 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 INDEX APPENDICES • Automatic sequencing of waypoints has not been suspended (no ‘SUSP’ annunciation on the HSI) 350 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW GPS Approach Mode Active Glidepath Mode Active FLIGHT INSTRUMENTS EIS Command Bars Indicate Descent on Glidepath Figure 7-16 Glidepath Mode FLIGHT MANAGEMENT LNAV/VNAV Approach Active AUDIO PANEL & CNS GPS is Selected Navigation Source Glidepath Indicator HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 351 SYSTEM OVERVIEW Automatic Flight Control System Glideslope Mode (GS) NOTE: Pressing the CWS Button while Glideslope Mode is active does not cancel the mode. The autopilot FLIGHT INSTRUMENTS 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 (annunciated as ‘GS’ in white), LOC Approach Mode is armed as the lateral flight director mode. Selecting Glideslope Mode: EIS 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). 3) Press the APR Key. AUDIO PANEL & CNS Or: 1) Ensure that GPS is the selected navigation source (use the CDI Softkey to cycle through navigation sources). 2) Ensure a LOC/ILS approach is loaded into the active flight plan. FLIGHT MANAGEMENT 3) Ensure the corresponding LOC frequency is tuned. 4) Press the APR Key. HAZARD AVOIDANCE Figure 7-17 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. Approach Mode Active Glideslope Mode Active APPENDICES ADDITIONAL FEATURES AFCS Active ILS Frequency Tuned INDEX NAV2 (localizer) is Selected Navigation Source Command Bars Indicate Descent on Localizer/Glideslope Path Figure 7-18 Glideslope Mode 352 Garmin G1000 Pilot’s Guide for the Diamond DA42NG Glideslope Indicator 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW Go Around Mode (GA) FLIGHT INSTRUMENTS Pushing the GA Switch engages the flight director in a wings-level, pitch-up attitude, allowing the execution of a missed approach or a go around. This mode is a coupled pitch and roll mode and is annunciated as ‘GA’ in both the active pitch and roll mode fields. Go Around Mode disengages the autopilot and arms Selected Altitude Capture Mode automatically. Subsequent autopilot engagement is allowed. Attempts to modify the aircraft attitude (i.e., with the CWS Button or NOSE UP/NOSE DN Keys) result in reversion to Pitch and Roll Hold modes. Go Around Mode Active EIS AUDIO PANEL & CNS Autopilot Disconnect Annunciation Flashes Yellow for 5 sec FLIGHT MANAGEMENT HAZARD AVOIDANCE Command Bars Indicate Climb Figure 7-19 Go Around Mode AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 353 SYSTEM OVERVIEW Automatic Flight Control System 7.4 Lateral Modes FLIGHT INSTRUMENTS The GFC 700 offers the lateral modes listed in Table 7-3. Refer to the vertical modes section for information regarding Go Around Mode. Lateral Mode Description Holds the current aircraft roll attitude or rolls the wings level, (default) depending on the commanded bank angle Captures and tracks the HDG Selected Heading Key EIS Roll Hold Heading Select AUDIO PANEL & CNS Control Annunciation Navigation, GPS Navigation, VOR Enroute Capture/Track FLIGHT MANAGEMENT Navigation, LOC Capture/Track (No Glideslope) Navigation Backcourse Capture/Track Captures and tracks the selected navigation source (GPS, VOR, LOC) HAZARD AVOIDANCE HDG 22º GPS 22º 22º Capture 10º Track 22º Capture 10º Track Captures and tracks a localizer signal for backcourse approaches BC GPS Approach, VOR Capture/Track Approach, LOC Capture/Track (Glideslope Mode automatically armed) AFCS 22º LOC Approach, GPS Go Around ROL VOR NAV Key Captures and tracks the selected navigation source (GPS, VOR, LOC) Disengages the autopilot and commands a constant pitch angle and wings level APR Key VAPP LOC GA Button Maximum Roll Command Limit GA 22º Capture 10º Track 22º 22º Capture 10º Track 22º Capture 10º Track Wings Level The GFC 700 limits turn rate to 3 degrees per second (standard rate turn). ADDITIONAL FEATURES Table 7-3 Flight Director Lateral Modes INDEX APPENDICES The CWS Button does not change lateral references for Heading Select, Navigation, Backcourse, or Approach modes. The autopilot guides the aircraft back to the Selected Heading/Course upon release of the CWS Button. 354 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW Roll Hold Mode (ROL) Note: If Roll Hold Mode is activated as a result of a mode reversion, the flight director rolls the wings FLIGHT INSTRUMENTS level. When the flight director is activated, 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 conditions listed in Table 7-4. EIS Figure 7-20 Roll Hold Mode Annunciation Flight Director Response Rolls wings level Maintains current aircraft roll attitude Limits bank to 22° AUDIO PANEL & CNS Bank Angle < 6° 6 to 22° > 22° FLIGHT MANAGEMENT Table 7-4 Roll Hold Mode Responses Changing the Roll Reference HAZARD AVOIDANCE The roll reference can be changed by pressing the CWS Button, establishing the desired bank angle, then releasing the CWS Button. AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 355 SYSTEM OVERVIEW Automatic Flight Control System Heading Select Mode (HDG) FLIGHT INSTRUMENTS 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 Knob synchronizes the Selected Heading to the current heading. EIS The Selected Heading is adjusted using the HDG 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. AUDIO PANEL & CNS 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 340° at a time result in turn reversals. Altitude Hold Mode Active FLIGHT MANAGEMENT Heading Select Mode Active Selected Heading Bug AFCS HAZARD AVOIDANCE Selected Heading ADDITIONAL FEATURES Command Bars Track Selected Heading INDEX APPENDICES Figure 7-21 Heading Select Mode 356 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW 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 INSTRUMENTS flight director to enter Navigation Mode. NOTE: When intercepting a flight plan leg, the flight director gives commands to capture the active leg at approximately a 45° angle to the track between the waypoints defining the active leg. The flight director does not give commands fly to the starting waypoint of the active leg. EIS NOTE: When making a backcourse approach, set the Selected Course to the localizer front course. AUDIO PANEL & CNS 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 glideslope capture is not required. FLIGHT MANAGEMENT Backcourse Navigation Mode is selected when the localizer front course is greater than 105° from the aircraft heading. Backcourse Navigation Mode captures and tracks a localizer signal in the backcourse direction. The annunciation ‘BC’ in the AFCS Status Box indicates Backcourse Navigation Mode. HAZARD AVOIDANCE 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 roll mode. Figure 7-22 GPS Navigation Mode Armed AFCS 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 when the automatic navigation source switch takes place. If the APR Key is pressed prior to the automatic navigation source switch, LOC Navigation Mode is armed. ADDITIONAL FEATURES 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) APPENDICES • Navigation source manually switched (with the CDI Softkey) • During a LOC/ILS approach the FAF is crossed while in GPS Navigation Mode after the automatic navigation source switch from GPS to LOC INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 357 SYSTEM OVERVIEW Automatic Flight Control System Changing the Selected Course FLIGHT INSTRUMENTS The Selected Course is controlled using the CRS Knob (while in VOR, LOC, or OBS Mode). 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. Pitch Hold Mode Active FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS GPS Navigation Mode Active HAZARD AVOIDANCE GPS is Selected Navigation Source Command Bars Indicate Left Turn to Track GPS Course and Climb to Intercept Selected Altitude Selected Course Figure 7-23 Navigation Mode Pitch Hold Mode Active INDEX APPENDICES ADDITIONAL FEATURES AFCS Backcourse Mode Active LOC2 is Selected Navigation Source Command Bars Hold Pitch Attitude Figure 7-24 Backcourse Mode 358 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW 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 INSTRUMENTS 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. EIS VOR Approach Mode (VAPP) provides greater sensitivity for signal tracking than VOR Navigation Mode. Selecting VOR Approach Mode: AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT When GPS Approach Mode is armed, Glidepath Mode is also armed. Selecting GPS Approach Mode: HAZARD AVOIDANCE 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. AFCS Figure 7-25 GPS Approach Mode Armed ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 359 SYSTEM OVERVIEW 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°. FLIGHT INSTRUMENTS 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. EIS Or: AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT If the following occurs, the flight director reverts to Roll Hold Mode (wings rolled level): • Approach Mode is active and a Vectors-To-Final is activated • Approach Mode is active and Navigation source is manually switched HAZARD AVOIDANCE • 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 AFCS The Selected Course is controlled using the CRS Knob (while in VOR, LOC, or OBS Mode). 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. ADDITIONAL FEATURES intercepting and flying a dme arc APPENDICES 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. INDEX 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. 360 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW 7.5 Autopilot and Yaw Damper Operation NOTE: Refer to the AFM for specific instructions regarding emergency procedures. FLIGHT INSTRUMENTS The autopilot and yaw damper operate 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 servo to relieve any sustained effort required by the pitch servo. The yaw damper reduces Dutch roll tendencies and coordinates turns. EIS Flight Control AUDIO PANEL & CNS Pitch and roll commands are provided to the servos, based on the active flight director modes. Servo motor control limits the maximum servo speed and torque. The servo mounts are equipped with slip-clutches set to certain values. This allows the servos to be overridden in case of an emergency. Pitch Axis and Pitch Trim FLIGHT MANAGEMENT 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. The pitch servo measures the output effort (torque) and provides this signal to the pitch trim servo. The pitch trim servo commands the motor to reduce the average pitch servo effort. HAZARD AVOIDANCE When the autopilot is not engaged, the pitch trim servo may be used to provide manual electric trim. This allows the aircraft to be trimmed using a control stick switch rather than the trim wheel. Manual trim commands are generated only when both halves of the MEPT Switch are operated simultaneously. Trim speeds are scheduled with airspeed to provide more consistent response. Roll Axis AFCS 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 ADDITIONAL FEATURES 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. APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 361 SYSTEM OVERVIEW Automatic Flight Control System Engaging the Autopilot and Yaw Damper NOTE: Autopilot engagement/disengagement is not equivalent to servo engagement/disengagement. Use FLIGHT INSTRUMENTS the CWS Button to disengage the pitch and roll servos while the autopilot remains active. EIS When the AP Key is pressed, the autopilot, yaw damper, and flight director are activated (if not already engaged). 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 (if not already engaged). 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. AUDIO PANEL & CNS Autopilot Engaged Figure 7-26 Autopilot and Yaw Damper Engaged FLIGHT MANAGEMENT Control Wheel Steering HAZARD AVOIDANCE 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. CWS activity has no effect on yaw damper engagement. The ‘AP’ annunciation is temporarily replaced by ‘CWS’ in white for the duration of CWS maneuvers. In most scenarios, releasing the CWS Button reengages the autopilot with a new reference. Refer to the flight director modes section for CWS behavior in each mode. AFCS Control Wheel Steering INDEX APPENDICES ADDITIONAL FEATURES Figure 7-27 CWS Annunciation 362 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW Disengaging the Autopilot and Yaw Damper FLIGHT INSTRUMENTS The autopilot is manually disengaged by pushing the AP DISC Switch, GA Button, AP TRIM ARM Switch, or the AP Key on the MFD. Manual disengagement is indicated by a five-second flashing yellow ‘AP’ annunciation and a two-second autopilot disconnect aural alert. After manual disengagement, the autopilot disconnect aural alert may be cancelled by pushing the AP TRIM ARM or AP DISC Switch (AP DISC Switch also cancels the flashing ‘AP’ annunciation). The YD Key or AP DISC Switch can be used to disengage the yaw damper. The ‘YD’ annunciation turns yellow and flashes for five seconds upon disengagement. EIS Figure 7-28 Manual Autopilot Disengagement AUDIO PANEL & CNS Automatic autopilot disengagement is indicated by a flashing red ‘AP’ annunciation and by the autopilot disconnect aural alert, which continue until acknowledged by pushing the AP DISC or AP TRIM ARM Switch. Automatic disengagement occurs due to: • Invalid sensor data • Inability to compute default flight director modes (FD also disengages automatically) • Stall Warning FLIGHT MANAGEMENT • System failure HAZARD AVOIDANCE Figure 7-29 Automatic Autopilot Disengagement AFCS Automatic yaw damper disengagement occurs when autopilot disengagement is caused by a failure in a parameter also affecting the yaw damper. This means that the yaw damper can remain operational in some cases where the autopilot automatically disengages. The yaw damper also disengages upon a localized failure in the yaw damper system. ADDITIONAL FEATURES Figure 7-29 Automatic Autopilot Disengagement APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 363 SYSTEM OVERVIEW Automatic Flight Control System 7.6 Example Flight Plan FLIGHT INSTRUMENTS 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. EIS This scenario-based set of procedures (based on the example flight plan found in the Flight Management Section) shows various GFC 700 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. 0 24 27 24 27 24 30 21 18 15 18 9 24 21 12 15 27 12 6 Lamar VOR (LAA) Topeka VOR (TOP) 21 Hays VOR (HYS) 9 V 244 Salina VOR (SLN) 12 3 V4 18 V 244 9 6 0 33 KMKC 27 30 6 KCOS HAZARD AVOIDANCE 3 30 3 6 0 33 3 30 33 9 FLIGHT MANAGEMENT 33 0 15 AUDIO PANEL & CNS Airway V4 is flown to Salina VOR (SLN) using VOR navigation, then airway V244 is flown using GPS navigation. The ILS approach for runway 35L and LPV (WAAS) approach for runway 35R are shown and a missed approach is executed. 12 21 15 18 AFCS Figure 7-30 Flight Plan Overview Departure ADDITIONAL FEATURES Climbing to the Selected Altitude and flying an assigned heading: 1) Before takeoff, set the Selected Altitude to 12,000 feet using the ALT Knob. 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). APPENDICES a) Press the VS Key to activate Vertical Speed Mode. INDEX The Vertical Speed Reference may be adjusted after Vertical Speed Mode is selected using the NOSE UP/ NOSE DN Keys or pushing the CWS Button while hand-flying the aircraft to establish a new Vertical Speed Reference. 364 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW b) Press the AP Key to engage the autopilot in a climb using Vertical Speed Mode. FLIGHT INSTRUMENTS 3) Use the HDG 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. EIS 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 10 seconds. AUDIO PANEL & CNS At 50 feet from the Selected Altitude, the green ‘ALT’ annunciation flashes for up to 10 seconds; the autopilot transitions to Altitude Hold Mode and levels the aircraft. FLIGHT MANAGEMENT HD GM od HAZARD AVOIDANCE e 3 AFCS Selected Altitude of 12,000 MSL ALT Mode 4 1 2 VS ADDITIONAL FEATURES KMKC e Mod APPENDICES Figure 7-31 Departure INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 365 SYSTEM OVERVIEW Automatic Flight Control System Intercepting a VOR Radial FLIGHT INSTRUMENTS 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: EIS a) Tune the VOR frequency. b) Press the CDI Softkey to set the navigation source to VOR. AUDIO PANEL & CNS c) Use the CRS Knob to set the Selected Course to 255°. Note that at this point, the flight director is still in Heading Select Mode and the autopilot continues to fly 290°. FLIGHT MANAGEMENT d) Press the NAV Key. This arms VOR Navigation Mode and the white ‘VOR’ annunciation appears to the left of the active lateral mode. HAZARD AVOIDANCE 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 3 Hd 29 g 0o 30 AFCS 33 V4 6 o 255 Salina VOR (SLN) 24 VO R 9 ADDITIONAL FEATURES 27 3 NA V Mo de 2 HD G 12 M od e, VO R Ar m ed 15 21 18 APPENDICES 1 INDEX Figure 7-32 Intercepting a VOR Radial 366 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW Flying a Flight Plan/GPS Course Note: Changing the navigation source cancels Navigation Mode and causes the flight director to revert FLIGHT INSTRUMENTS 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: EIS 1) Transition from VOR to GPS Navigation Mode: a) Press the CDI Softkey until GPS is the selected navigation source. AUDIO PANEL & CNS b) Press the NAV Key to activate GPS Navigation Mode. The autopilot guides the aircraft along the active flight plan leg. 0 33 30 3 V4 6 3 o 075 30 e V Mod PS NA 6 27 G o AFCS 12 21 18 12 15 24 9 Hays VOR (HYS) Salina VOR (SLN) V 244 2 24 27 076 1 d AV Mo VOR N 9 o 260 e HAZARD AVOIDANCE 0 33 FLIGHT MANAGEMENT 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. 15 ADDITIONAL FEATURES 21 18 Figure 7-33 Transition to GPS Flight Plan APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 367 SYSTEM OVERVIEW Descent FLIGHT INSTRUMENTS Automatic Flight Control System • 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. While flying the arrival procedure, the aircraft is cleared for descent in preparation for the approach to KCOS. Three methods are presented for the descent: • 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. EIS • 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. AUDIO PANEL & CNS Flight Level Change descent: 1) Select Flight Level Change Mode: a) Using the ALT Knob, set the Selected Altitude to 10,000 feet. HAZARD AVOIDANCE FLIGHT MANAGEMENT b) Press the FLC Key to activate Flight Level Change Mode. The annunciation ‘FLC’ appears next to the Airspeed Reference, which defaults to the current aircraft airspeed. Selected Altitude Capture Mode is armed automatically. 2) Use the NOSE UP/NOSE DN Keys 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. AFCS 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 10 seconds. APPENDICES ADDITIONAL FEATURES The green ‘ALT’ annunciation flashes for up to 10 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 INDEX Selected Altitude of 10,000 MSL ALT Mode Figure 7-34 FLC Descent 368 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS b) Using the ALT Knob, set the Selected Altitude below the flight plan’s VNV Target Altitude of 10,000 feet. EIS If the Selected Altitude is not at least 75 ft below the VNV Target Altitude, the flight director captures the Selected Altitude rather than the VNV Target Altitude once Vertical Path Tracking Mode becomes active (ALTS is armed rather than ALTV). • Press the VNV Key • Turn the ALT Knob to adjust the Selected Altitude AUDIO PANEL & CNS 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 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. FLIGHT MANAGEMENT HAZARD AVOIDANCE 3) As the aircraft nears the VNV Target Altitude, the flight director transitions to VNV Target Altitude Capture Mode, indicated by the green ‘ALTV’ annunciation flashing for up to 10 seconds. AFCS The green ‘ALT’ annunciation flashes for up to 10 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. ALT Mode TOD ADDITIONAL FEATURES 1 Cruise Altitude of 12,000 MSL 2 APPENDICES VPT HM ode 3 BOD VNAV Target Altitude of 10,000 MSL ALT Mode Selected Altitude (set below VNAV Target Altitude) INDEX 3 nm OPSHN Figure 7-35 VPTH Descent 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 369 SYSTEM OVERVIEW 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: FLIGHT INSTRUMENTS a) Using the ALT 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. EIS 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. AUDIO PANEL & CNS 2) Reduce power to allow descent in Flight Level Change Mode. The autopilot maintains the Airspeed Reference. FLIGHT MANAGEMENT 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 10 seconds. HAZARD AVOIDANCE The green ‘ALT’ annunciation flashes for up to 10 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. AFCS 4) When the next TOD is reached, Vertical Path Tracking becomes active (may require acknowledgment to allow descent path capture). ADDITIONAL FEATURES 5) As the aircraft nears the VNV Target Altitude, the flight director transitions to VNV Target Altitude Capture Mode, indicated by the green ‘ALTV’ annunciation flashing for up to 10 seconds. The green ‘ALT’ annunciation flashes for up to 10 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. INDEX APPENDICES 370 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW VP TH M od e ALT Mode 1 FL C VNAV Target Altitude of 10,000 MSL Pla nn M od e Selected Altitude of 9,400 MSL FLIGHT INSTRUMENTS Planned TOD 2 BOD 3 ed De sce nt Pa th ALT Mode TOD 4 VP TH Mo 5 BOD ALT Mode EIS VNAV Target Altitude of 9,000 MSL de Selected Altitude OPSHN HABUK AUDIO PANEL & CNS 3 nm Figure 7-36 Non-path Descent FLIGHT MANAGEMENT Approach Flying an ILS approach: 1) Transition from GPS Navigation Mode to Heading Select Mode. HAZARD AVOIDANCE 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 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. AFCS 2) Arm LOC Approach and Glideslope modes. ADDITIONAL FEATURES 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. APPENDICES 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. 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. INDEX • Use the GA Button to execute a missed approach. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 371 SYSTEM OVERVIEW Automatic Flight Control System KCOS FLIGHT INSTRUMENTS LOC APR/ GS Mode 3 PETEY 2 HD G od M e 1 AUDIO PANEL & CNS GPS NAV Mode EIS PYNON FLIGHT MANAGEMENT Figure 7-37 ILS Approach to KCOS NOTE: Refer to the AFM to determine whether WAAS functionality is approved. Support for WAAS precision HAZARD AVOIDANCE approaches is available only in installations with GIA 63Ws when WAAS is available. 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). AFCS b) Select the Runway 35R LPV approach for KCOS. Load and activate the approach into the flight plan. ADDITIONAL FEATURES 2) Press the APR Key once clearance for approach has been received. GPS Approach Mode is activated and Glidepath Mode is armed. APPENDICES 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. INDEX • Use the GA Button to execute a missed approach. 372 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW FLIGHT INSTRUMENTS KCOS 4 EIS AUDIO PANEL & CNS 3 GPS APR/ GP Mode CEGIX 2 FALUR HABUK FLIGHT MANAGEMENT PYNON 1 HAZARD AVOIDANCE GPS NAV Mode AFCS Figure 7-38 LPV Approach to KCOS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 373 SYSTEM OVERVIEW 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 FLIGHT INSTRUMENTS re-size automatically and the aircraft may not precisely track the holding pattern as depicted on the PFD and MFD. Flying a missed approach: EIS 1) Push the GA Button 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 GA Button is pushed, the missed approach is activated and the autopilot disconnects, indicated by the ‘AP’ annunciation flashing yellow for 5 seconds. AUDIO PANEL & CNS Flashes 5 sec FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE b) Press the NAV Key to have the autopilot fly to the hold. 3) Use the ALT Knob to set a Selected Altitude to hold. AFCS To hold the current airspeed during the climb, press the FLC Key. ADDITIONAL FEATURES 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 10 seconds. APPENDICES The green ‘ALT’ annunciation flashes for up to 10 seconds upon reaching 50 feet from the Selected Altitude; the autopilot transitions to Altitude Hold Mode and levels the aircraft. INDEX 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. 374 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS 4 FLIGHT MANAGEMENT GPS NAV Mode AUDIO PANEL & CNS MOGAL 3 2 HAZARD AVOIDANCE GA Mode KCOS 1 AFCS Figure 7-39 Go Around/Missed Approach ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 375 SYSTEM OVERVIEW Automatic Flight Control System 7.7 AFCS Annunciations and Alerts FLIGHT INSTRUMENTS AFCS Status Alerts The annunciations in Table 7-5 (listed in order of increasing priority) can appear on the PFD above the Airspeed and Attitude indicators. Only one annunciation may occur at a time, and messages are prioritized by criticality. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS AFCS Status Annunciation INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Figure 7-40 AFCS Status Annunciation 376 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Automatic Flight Control System Rudder Mistrim Right Rudder Mistrim Left Aileron Mistrim Left Elevator Mistrim Down Pitch Trim Failure Yaw Damper Failure Roll servo providing sustained force in indicated direction Pitch servo providing sustained force in the indicated direction If AP engaged, take control of the aircraft and disengage AP If AP disengaged, move AP TRIM switches separately to unstick YD control failure Roll axis control failure; AP inoperative Pitch Failure Pitch axis control failure; AP inoperative AP and MET are unavailable; FD may still be available Performing preflight system test; aural alert sounds at completion Do not press the AP DISC Switch during servo power-up and preflight system tests. Doing so may cause the preflight system test to fail or never to start. Cycle power to the servos if this occurs. HAZARD AVOIDANCE Preflight Test FLIGHT MANAGEMENT Roll Failure System Failure AUDIO PANEL & CNS (or Stuck AP TRIM Switch) Yaw servo providing sustained force in the indicated direction EIS Elevator Mistrim Up Description FLIGHT INSTRUMENTS Aileron Mistrim Right Annunciation SYSTEM OVERVIEW Alert Condition Preflight system test failed; aural alert sounds at failure Table 7-5 AFCS Status Alerts AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 377 SYSTEM OVERVIEW Overspeed Protection FLIGHT INSTRUMENTS 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. EIS Automatic Flight Control System When an autopilot overspeed condition occurs, the Airspeed Reference appears in a box above the Airspeed Indicator, flashing a yellow ‘MAXSPD’ annunciation. Engine power should be reduced and/or the pitch reference adjusted to slow the aircraft. The annunciation disappears when the overspeed condition is resolved. AUDIO PANEL & CNS Note: Overspeed protection is not active in Altitude Hold, Glideslope or Glidepath Modes. FLIGHT MANAGEMENT Airspeed Indicator INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Figure 7-41 Overspeed Annunciation 378 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW Section 8 Additional Features FLIGHT INSTRUMENTS NOTE: With the availability of SafeTaxi, ChartView, or FliteCharts in electronic form, it is still advisable to carry another source of charts on board the aircraft. Additional features of the G1000 include the following: • Synthetic Vision System (SVS) • SafeTaxi® diagrams EIS • ChartView and FliteCharts® electronic charts • XM Radio entertainment AUDIO PANEL & CNS • Scheduler • Electronic Checklists (Optional) FLIGHT MANAGEMENT The optional Synthetic Vision System (SVS) provides a three-dimensional forward view of terrain features on the PFD. SVS 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. HAZARD AVOIDANCE The optional ChartView and FliteCharts 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. AFCS The optional XM Radio entertainment audio feature of the GDL 69A Data Link Receiver handles more than 170 channels of music, news, and sports. XM 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, Change oil, or Altimeter-Transponder Check in the Alerts Window on the PFD. ADDITIONAL FEATURES Optional checklists help to quickly find the proper procedure on the ground or during flight. APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 379 SYSTEM OVERVIEW Additional Features 8.1 Synthetic Vision System (SVS) (Optional) FLIGHT INSTRUMENTS WARNING: Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance. SVS 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. FLIGHT MANAGEMENT The SVS 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. HAZARD AVOIDANCE AUDIO PANEL & CNS EIS The optional Synthetic Vision System (SVS) is a visual enhancement to the G1000 Integrated Flight Deck. SVS 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. SVS information is shown on the Primary Flight Display (PFD), or on the Multifunction Display (MFD) in Reversionary Mode (Figure 8‑80). 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 SVS. Loss of any of the required data, including temporary loss of the GPS signal, will cause SVS to be disabled until the required data is restored. The Terrain-SVS is integrated within SVS 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. AFCS 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 Terrain–SVS terrain or obstacle data displayed by the SVS. • Pathways • Airport Signs • Flight Path Marker • Runway Display • Horizon Heading Marks • Terrain Alerting • Traffic Display • Obstacle Alerting INDEX APPENDICES ADDITIONAL FEATURES The following SVS enhancements appear on the PFD: 380 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-1 Synthetic Vision Imagery SVS Operation HAZARD AVOIDANCE SVS 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 SVS is enabled, the pitch scale increments are reduced to 10 degrees up and 7.5 degrees down. AFCS SVS 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 SVS 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 SVS feature may be activated. ADDITIONAL FEATURES 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. APPENDICES • 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. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 381 SYSTEM OVERVIEW Additional Features FLIGHT INSTRUMENTS PFD SYN VIS BACK Pressing the BACK Softkey returns to the top-level softkeys. BACK EIS PATHWAY SYN TERR HRZN HDG APTSIGNS AUDIO PANEL & CNS Pressing the BACK Softkey returns to the previous level of softkeys. Figure 8-2 SVS Softkeys Activating and deactivating SVS: FLIGHT MANAGEMENT 1) Press the PFD Softkey. 2) Press the SYN VIS Softkey. 3) Press the SYN TERR Softkey. The SVS display will cycle on or off with the SYN TERR Softkey. HAZARD AVOIDANCE 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. AFCS Activating and deactivating Horizon Headings: 1) Press the PFD Softkey. 2) Press the SYN VIS Softkey. ADDITIONAL FEATURES 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. APPENDICES 2) Press the SYN VIS Softkey. INDEX 3) Press the APTSIGNS Softkey. Display of airport signs will cycle on or off with the APTSIGNS Softkey. 382 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW SVS Features FLIGHT INSTRUMENTS Selected Altitude Airport Runway Pathways Color Matches CDI Indicating NAV Source Flight Path Marker Airplane Symbol EIS Zero Pitch Line (ZPL) with Compass Heading Marks AUDIO PANEL & CNS Synthetic Terrain FLIGHT MANAGEMENT HAZARD AVOIDANCE SVS Softkeys Figure 8-3 SVS on the Primary Flight Display NOTE: Pathways and terrain features are not a substitute for standard course and altitude deviation information provided by the CDI, VSI, and VDI. AFCS Pathways ADDITIONAL FEATURES 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 higher of either the selected altitude or the VNAV altitude programmed for the active leg in the flight plan (Figure 8-4). APPENDICES 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX 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. 383 SYSTEM OVERVIEW Additional Features FLIGHT INSTRUMENTS Selected Altitude FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS Programmed Altitudes HAZARD AVOIDANCE Figure 8-4 Programmed and Selected Altitude AFCS Pathways provide supplemental glidepath 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. Departure and Enroute APPENDICES ADDITIONAL FEATURES 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 SVS 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. INDEX Pathways are displayed along the flight plan route at the highest of either the selected altitude or the programmed altitude for the leg. 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. 384 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW Descent and Approach FLIGHT INSTRUMENTS 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. EIS When an approach providing vertical guidance is activated, Pathways are shown level at the selected altitude or at the next programmed crossing altitude, Pathways are shown level at the selected altitude or at the next programmed crossing altitude, whichever is higher, 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. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 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 HAZARD AVOIDANCE Climbs NOT displayed by pathway Non-programmed descents NOT displayed by pathway TOD AFCS Selected Altitude for Step Down Programmed descent displayed by pathway ADDITIONAL FEATURES APPENDICES Selected Altitude or Programmed Altitude (whichever is higher) Figure 8-5 SVS Pathways, Enroute and Descent INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 385 SYSTEM OVERVIEW Additional Features Missed Approach FLIGHT INSTRUMENTS 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. AUDIO PANEL & CNS EIS 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 HAZARD AVOIDANCE FLIGHT MANAGEMENT Descent displayed by pathway Selected Altitude or Programmed Altitude (whichever is higher) MAP Climbs NOT displayed by pathway Turn Segment NOT displayed by pathway APPENDICES ADDITIONAL FEATURES AFCS MAHP INDEX Figure 8-6 SVS Pathways, Approach, Missed Approach, and Holding 386 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW Flight Path Marker FLIGHT INSTRUMENTS 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. EIS 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). AUDIO PANEL & CNS 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 the Terrain-SVS system. However, decisions regarding terrain and/or obstacle avoidance should not be made using only the FPM. FLIGHT MANAGEMENT HAZARD AVOIDANCE Flight Path Marker (FPM) AFCS Wind Vector ADDITIONAL FEATURES APPENDICES Figure 8-7 Flight Path Marker and Pathways Zero Pitch Line 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX The Zero Pitch Line is drawn completely across the display and represents the aircraft attitude with respect to the horizon. It may not align with the terrain horizon, particularly when the terrain is mountainous or when the aircraft is flown at high altitudes. 387 SYSTEM OVERVIEW Additional Features Horizon Heading FLIGHT INSTRUMENTS 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 SVS display or may appear as a EIS partial symbol. AUDIO PANEL & CNS 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 1000 feet laterally of the aircraft will not be displayed on the SVS 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 SVS display. For more details refer to the traffic system discussion in the Hazard Avoidance section. FLIGHT MANAGEMENT Airport Signs HAZARD AVOIDANCE 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. AFCS Traffic Airport Sign without Identifier (Between 8 nm and 15 nm) INDEX APPENDICES ADDITIONAL FEATURES Airport Sign with Identifier (Between 4.5 nm and 8 nm) Figure 8-8 Airport Signs 388 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW Runways WARNING: Do not use SVS runway depiction as the sole means for determining the proximity of the aircraft FLIGHT INSTRUMENTS to the runway or for maintaining the proper approach path angle during landing. EIS 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. AUDIO PANEL & CNS FLIGHT MANAGEMENT Other Runway on Airport Runway Selected for Approach HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Figure 8-9 Airport Runways APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 389 SYSTEM OVERVIEW Additional Features Terrain-SVS Alerting FLIGHT INSTRUMENTS Terrain alerting on the synthetic terrain display is triggered by Forward-looking Terrain Avoidance (FLTA) alerts, and corresponds to the red and yellow X symbols on the Inset Map and MFD map displays. For more detailed information regarding Terrain-SVS, refer to the Hazard Avoidance Section. EIS 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 SVS field of view to the left or right of the aircraft. AUDIO PANEL & CNS TERRAIN Annunciation FLIGHT MANAGEMENT Terrain Caution HAZARD AVOIDANCE Potential Impact Point INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 8-10 Terrain Alert 390 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW FLIGHT INSTRUMENTS 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. 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. EIS TERRAIN Annunciation AUDIO PANEL & CNS Obstacle Warning FLIGHT MANAGEMENT HAZARD AVOIDANCE Potential Impact Point Figure 8-11 Obstacle AFCS Field of View ADDITIONAL FEATURES 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: APPENDICES 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. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 391 EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Additional Features AUDIO PANEL & CNS Field of View FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 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. ADDITIONAL FEATURES AFCS The following figure compares the PFD forward looking depiction with the MFD plan view and FIELD OF VIEW turned on. APPENDICES Lines Depict PFD Field of View INDEX SVS View on the PFD Field of View on the MFD Figure 8-13 PFD and MFD Field of View Comparison 392 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW 8.2 SafeTaxi FLIGHT INSTRUMENTS SafeTaxi is an enhanced feature that 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. EIS 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. • User Waypoint Information Page • Weather Datalink Page • Trip Planning Page • Airport Information Page • Nearest Pages • Intersection Information Page • Active and Stored Flight Plan Pages FLIGHT MANAGEMENT • Inset Map (PFD) AUDIO PANEL & CNS 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: • VOR Information Page • Navigation Map Page • NDB Information Page HAZARD AVOIDANCE 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. AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 393 FLIGHT INSTRUMENTS SYSTEM OVERVIEW Additional Features Taxiway Identification EIS Aircraft Position AUDIO PANEL & CNS Airport Features FLIGHT MANAGEMENT Airport Hot Spot Outline DCLTR Softkey Removes Taxiway Markings Figure 8-14 SafeTaxi Depiction on the Navigation Map Page AFCS HAZARD AVOIDANCE The DCLTR Softkey (declutter) label advances to DCLTR-1, DCLTR -2, and DCLTR-3 each time the softkey is pressed for easy recognition of decluttering level. Pressing the DCLTR Softkey removes the taxiway markings and airport feature labels. Pressing the DCLTR-1 Softkey removes VOR station ID, the VOR symbol, and intersection names if within the airport plan view. Pressing the DCLTR-2 Softkey removes the airport runway layout, unless the airport in view is part of an active route structure. Pressing the DCLTR-3 Softkey cycles back to the original map detail. Refer to Map Declutter Levels in the Flight Management Section. Configuring SafeTaxi range: 1) While viewing the Navigation Map Page, press the MENU Key to display the PAGE MENU. INDEX APPENDICES ADDITIONAL FEATURES 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 394 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 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. EIS AUDIO PANEL & CNS SAFETAXI Option FLIGHT MANAGEMENT SafeTaxi Range Options HAZARD AVOIDANCE AFCS Figure 8-16 MAP SETUP Menu, Aviation Group, SAFETAXI Range Options ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 395 SYSTEM OVERVIEW Additional Features SafeTaxi Cycle Number and Revision HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS The SafeTaxi database is revised every 56 days. SafeTaxi is always available for use after the expiration date. When turning on the G1000, the Power-up Page indicates whether the databases are current, out of date, or not available. The Power-up Page shows the SafeTaxi database is current when the SafeTaxi Expires date is shown in white. When the SafeTaxi cycle has expired, the SafeTaxi Expires date appears in yellow. The message SafeTaxi: N/A appears in white if no SafeTaxi data is available on the database card. SafeTaxi Database has Expired APPENDICES ADDITIONAL FEATURES AFCS SafeTaxi Database is Current INDEX SafeTaxi Database Not Available Figure 8-17 Power-up Page, SafeTaxi Database 396 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW FLIGHT INSTRUMENTS The SafeTaxi Region, Version, Cycle, Effective date and Expires date of the database cycle can also be found on the AUX - System Status page. 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). SafeTaxi REGION NOT AVAILABLE appears in blue if SafeTaxi data is not available on the database card (Figure 8‑19). Expired SafeTaxi data is never disabled. Press the DBASE Softkey for scrolling through the database information. Scroll through the database with the FMS knob or ENT Key. The SafeTaxi database cycle number shown in the figure, 08S6, is deciphered as follows: EIS 08 – Indicates the year 2008 S – Indicates the data is for SafeTaxi AUDIO PANEL & CNS 6 – Indicates the sixth issue of the SafeTaxi database for the year The SafeTaxi EFFECTIVE date 25–OCT–08 is the beginning date for the current database cycle. SafeTaxi EXPIRES date 20–DEC–08 is the revision date for the next database cycle. FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS SafeTaxi Data ADDITIONAL FEATURES APPENDICES Figure 8-18 AUX – System Status Page, SafeTaxi Current Information The SafeTaxi database is provided by Garmin. Refer to Updating Garmin Databases in Appendix B for instructions on revising the SafeTaxi database. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 397 SYSTEM OVERVIEW Additional Features HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS The other three possible AUX - System Status page conditions are shown here. 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. SafeTaxi Database has Expired APPENDICES ADDITIONAL FEATURES AFCS Current Date is before Effective Date INDEX SafeTaxi Database Not Installed Figure 8-19 AUX – System Status Page, SafeTaxi Expired, SafeTaxi Not Available 398 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW 8.3 ChartView FLIGHT INSTRUMENTS 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 plan view of approach charts and on airport diagrams. Airport Hot Spots are outlined in magenta. The ChartView database subscription is available from Jeppesen, Inc. Available data includes: • Arrivals (STAR) • Airport Diagrams • Departure Procedures (DP) • NOTAMs EIS • Approaches ChartView Softkeys AUDIO PANEL & CNS ChartView functions are displayed on three levels of softkeys. While on the Navigation Map Page, Nearest Airports Page, or Flight Plan Page, pressing 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. FLIGHT MANAGEMENT Pressing the GO BACK Softkey reverts to the top level softkeys and previous page. Pressing 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. HAZARD AVOIDANCE SHW CHRT CHRT INFO DP STAR APR WX NOTAM GO BACK AFCS CHRT OPT Pressing the GO BACK Softkey returns to the top-level softkeys and previous page. HEADER PLAN PROFILE MINIMUMS FIT WDTH FULL SCN ADDITIONAL FEATURES ALL BACK Pressing the BACK Softkey returns to the Chart Selection Softkeys. APPENDICES Figure 8-20 ChartView SHW CHRT, Chart Selection, and Chart Option Softkeys INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 399 SYSTEM OVERVIEW Additional Features Terminal Procedures Charts Selecting Terminal Procedures Charts: FLIGHT INSTRUMENTS While viewing the Navigation Map Page, Nearest Airport Page, or Flight Plan Page, press 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. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 3) Press the ENT Key to display the chart. Navigation Map Page OPTIONS Menu Waypoint Airport Information Page OPTIONS Menu Figure 8-21 Option Menus ADDITIONAL FEATURES AFCS 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. APPENDICES Figure 8-22 Chart Not Available Banner INDEX 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 8-23 Unable To Display Chart Banner 400 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW When a chart is not available by pressing 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. FLIGHT INSTRUMENTS 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, pressing 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. EIS Selecting a chart: 1) While viewing the Navigation Map Page, Flight Plan Page, or Nearest Airports Page, press the SHW CHRT Softkey. The airport diagram or approach chart is displayed on the Airport Information Page. AUDIO PANEL & CNS 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. (Press 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. FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 8) Turn either FMS Knob to scroll through the available charts. 9) Press the ENT Key to complete the chart selection. AFCS Chart Scale Select Desired Approach Chart From Menu ADDITIONAL FEATURES Scroll Through Chart With the Joystick APPENDICES INDEX Figure 8-24 Approach Information Page, Chart Selection 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 401 SYSTEM OVERVIEW Additional Features While the APPROACH Box is selected using the FMS Knob, the G1000 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. FLIGHT INSTRUMENTS 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 8‑28). 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. AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS Pressing 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 Colorado Springs, CO (KCOS) Airport Diagram and the navigation map on the WPT – Airport Information page. INDEX APPENDICES ADDITIONAL FEATURES Press CHRT Softkey to Switch Between ChartView and WPT Airport Information Page Figure 8-25 CHRT Softkey, Airport Information Page 402 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW Pressing the INFO Softkey returns to the airport diagram when the view is on a different chart. If the displayed chart is the airport diagram, the INFO Softkey has no effect. FLIGHT INSTRUMENTS 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 Romeo on the Charlotte, NC (KCLT) airport. EIS 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 Softkey. When the INFO Box is selected using the FMS Knob, the G1000 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.) AUDIO PANEL & CNS FLIGHT MANAGEMENT Aircraft Current Position HAZARD AVOIDANCE AFCS Figure 8-26 Airport Information Page, INFO View, Full Screen Width ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 403 SYSTEM OVERVIEW Additional Features FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS In the example shown in Figure 8-26, the Class B Chart is selected. Pressing the ENT Key displays the Charlotte Class B Airspace Chart (Figure 8-27). HAZARD AVOIDANCE Figure 8-27 Airport Information Page, Class B Chart Selected from INFO View Pressing the DP Softkey displays the Departure Procedure Chart if available. APPENDICES ADDITIONAL FEATURES AFCS Chart Not To Scale INDEX Aircraft Not Shown Icon Figure 8-28 Departure Information Page 404 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW Pressing the STAR Softkey displays the Standard Terminal Arrival Chart if available. FLIGHT INSTRUMENTS Chart Not To Scale EIS Change Range and Scroll Through the Chart With the Joystick AUDIO PANEL & CNS FLIGHT MANAGEMENT Aircraft Not Shown Icon Figure 8-29 Arrival Information Page HAZARD AVOIDANCE Pressing the APR Softkey displays the approach chart for the airport if available. AFCS ADDITIONAL FEATURES APPENDICES 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX Figure 8-30 Approach Information Page 405 SYSTEM OVERVIEW Additional Features EIS FLIGHT INSTRUMENTS Pressing 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 XM Weather subscription is current. FLIGHT MANAGEMENT AUDIO PANEL & CNS WX Info When Available WX Softkey Selected HAZARD AVOIDANCE Figure 8-31 Weather Information Page NOTE: A subdued softkey label indicates the function is disabled. INDEX APPENDICES ADDITIONAL FEATURES AFCS Recent NOTAMS applicable to the current ChartView cycle are included in the ChartView database. Pressing 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 as shown in Figure 8-31. The NOTAM Softkey may appear on the Airport Information Page and all of the chart page selections. 406 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT NOTAM Softkey Appears for Selected Airports Figure 8-32 NOTAM Softkey Highlighted HAZARD AVOIDANCE Local NOTAM on This Airport AFCS ADDITIONAL FEATURES APPENDICES NOTAM Softkey Selected Figure 8-33 Airport Information Page, Local NOTAMs INDEX Pressing the NOTAM Softkey again removes the NOTAMS information. Pressing the GO BACK Softkey reverts to the previous page (Navigation Map Page, Nearest Pages, or Flight Plan Page). 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 407 SYSTEM OVERVIEW Additional Features Chart Options Pressing the CHRT OPT Softkey displays the next level of softkeys, the chart options level (Figure 8-20). AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Pressing the ALL Softkey shows the complete approach chart on the screen. HAZARD AVOIDANCE FLIGHT MANAGEMENT Complete Chart Shown INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 8-34 Approach Information Page, ALL View 408 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW Pressing the HEADER Softkey shows the header view (approach chart briefing strip) on the screen. FLIGHT INSTRUMENTS EIS Approach Chart Briefing Strip AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-35 Approach Information Page, Header View HAZARD AVOIDANCE Pressing the PLAN Softkey shows the approach chart two dimensional plan view. AFCS ADDITIONAL FEATURES Approach Chart Plan View APPENDICES INDEX Figure 8-36 Approach Information Page, Plan View 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 409 SYSTEM OVERVIEW Additional Features EIS FLIGHT INSTRUMENTS Pressing the PROFILE Softkey displays the approach chart descent profile strip. FLIGHT MANAGEMENT AUDIO PANEL & CNS Approach Chart Descent Profile Strip Figure 8-37 Approach Information Page, Profile View, Full Screen Width ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Pressing the MINIMUMS Softkey displays the minimum descent altitude/visibility strip at the bottom of the approach chart. INDEX APPENDICES Minimum Descent Altitude/ Visibility Strip Figure 8-38 Approach Information Page, Minimums View, Full Screen Width 410 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW If the chart scale has been adjusted to view a small area of the chart, pressing the FIT WIDTH Softkey changes the chart size to fit the available screen width. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Press FIT WDTH Softkey to Show Full Chart Width Figure 8-39 Airport Information Page, FIT WDTH Softkey Pressed APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 411 SYSTEM OVERVIEW Additional Features Pressing the FULL SCN Softkey alternates between removing and replacing the data window to the right. Selecting Additional Information: FLIGHT INSTRUMENTS 1) While viewing the Airport Taxi Diagram, press 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). EIS 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. FLIGHT MANAGEMENT AUDIO PANEL & CNS 5) Press the FMS Knob again to deactivate the cursor. AFCS HAZARD AVOIDANCE Available Information APPENDICES ADDITIONAL FEATURES Press FULL SCN Softkey to Switch Between Full Screen and Chart with Info Window Figure 8-40 Airport Information Page, Full Screen and Info Window INDEX Pressing the BACK Softkey, or waiting for 45 seconds reverts to the chart selection softkeys. 412 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW The full screen view can also be selected by using the page menu option. Selecting full screen On or Off: FLIGHT INSTRUMENTS 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. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Chart Setup Option Full Screen On/Off Selection HAZARD AVOIDANCE Figure 8-41 Page Menus AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 413 SYSTEM OVERVIEW Additional Features Day/Night View FLIGHT INSTRUMENTS 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 G1000 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. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key. HAZARD AVOIDANCE Figure 8-42 Waypoint Information Page, OPTIONS Menu 3) Turn the large FMS Knob to move to the COLOR SCHEME Option (Figure 8‑43). 4) Turn the small FMS Knob to choose between Day, Auto, and Night Options. AFCS 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. ADDITIONAL FEATURES 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. INDEX APPENDICES 6) Press the FMS Knob when finished to remove the Chart Setup Menu. 414 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-43 Arrival Information Page, Day View HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 8-44 Arrival Information Page, Night View INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 415 SYSTEM OVERVIEW Additional Features ChartView Cycle Number and Expiration Date FLIGHT INSTRUMENTS The ChartView database is revised every 14 days. Charts are still viewable during a period that extends from the cycle expiration date to the disabled date. ChartView is disabled 70 days after the expiration date and is no longer available for viewing upon reaching the disabled date. When turning on the G1000, the Power-up Page indicates any of nine different possible criteria for ChartView availability. See the table below for the various ChartView Power-up Page displays and the definition of each. AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS Power-up Page Display Definition Blank Line. G1000 system is not configured for ChartView. Contact a Garmin-authorized 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 G1000 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. INDEX APPENDICES ADDITIONAL FEATURES Table 8-1 ChartView Power-up Page Annunciations and Definitions 416 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW FLIGHT INSTRUMENTS Examples of four possible Power-up Page conditions are shown here. ‘ChartView Disables’, plus a date in white, indicates chart data is current. This indication for normal operation shows how long the charts may be viewed. ‘Chart data update available.’ in white, indicates the chart data cycle has expired within the past week and the next chart cycle is available. ‘Chart data is out of date!’ in yellow, indicates charts are still viewable, but approaching the disable date. ‘Chart data is disabled.’ in yellow, indicates the chart cycle has been disabled and is no longer viewable. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Chart Cycle has Expired but is Still Viewable for 70 Days from Expiration Date Chart Cycle is No Longer Viewable AFCS Chart Cycle has Expired, Next Cycle is Available HAZARD AVOIDANCE ChartView Database is Current and Available ADDITIONAL FEATURES APPENDICES INDEX Figure 8-45 Examples of Power-up Page, ChartView Database 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 417 SYSTEM OVERVIEW Additional Features NOTE: A subdued softkey label indicates the function is disabled. FLIGHT INSTRUMENTS 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. EIS Press the DBASE Softkey for scrolling through the database information. Scroll through the database with the FMS knob or ENT Key. The ChartView database cycle number shown in the figure, 0822, is deciphered as follows: AUDIO PANEL & CNS 08 – Indicates the year 2008 22 – Indicates the 22nd issue of the ChartView database for the year The EXPIRES date 15–NOV–08 is the date that this database should be replaced with the next issue. AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT The DISABLES date 24–JAN–09 is the date that this database becomes inoperative. APPENDICES ADDITIONAL FEATURES ChartView Data Figure 8-46 AUX – System Status Page, ChartView Current and Available INDEX The ChartView database is provided directly from Jeppesen. Refer to Updating Jeppesen Databases in Appendix B for instructions on revising the ChartView database. 418 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW The other three possible AUX - System Status page conditions are shown here. 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. REGION and CYCLE NOT AVAILABLE in blue, indicate that no ChartView data is available on the database card or no database card is inserted. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT ChartView Database has Expired, but is not Disabled ChartView Database is Disabled HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES System is Configured for ChartView but Database is not Available APPENDICES ChartView Database is Not Available 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX Figure 8-47 AUX – System Status Page, ChartView Expired, ChartView Disabled, ChartView Not Available 419 SYSTEM OVERVIEW Additional Features 8.4 FliteCharts FLIGHT INSTRUMENTS FliteCharts resemble the paper version of National Aeronautical Charting Office (NACO) terminal procedures charts. The charts are displayed with high-resolution and in color for applicable charts. FliteCharts database subscription is available from Garmin. Available data includes: • Arrivals (STAR) • Approaches • Departure Procedures (DP) • Airport Diagrams EIS FliteCharts Softkeys AUDIO PANEL & CNS FliteCharts functions are displayed on three levels of softkeys. While on the Navigation Map Page, Nearest Airports Page, or Flight Plan Page, pressing 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. Pressing the GO BACK Softkey reverts to the top level softkeys and previous page. FLIGHT MANAGEMENT Pressing 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. HAZARD AVOIDANCE SHW CHRT AFCS CHRT OPT CHRT INFO DP STAR APR WX GO BACK Presssing the GO BACK Softkey returns to the top-level softkeys and previous page. ADDITIONAL FEATURES ALL FIT WDTH FULL SCN BACK Pressing the BACK Softkey returns to the Chart Selection Softkeys. INDEX APPENDICES Figure 8-48 FliteCharts SHW CHRT, Chart Selection, and Chart Option Softkeys 420 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW Terminal Procedures Charts Selecting Terminal Procedures Charts: FLIGHT INSTRUMENTS While viewing the Navigation Map Page, Nearest Airport Page, or Flight Plan Page, press 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. EIS 3) Press the ENT Key to display the chart. AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Navigation Map Page OPTIONS Menu Waypoint Airport Information Page OPTIONS Menu Figure 8-49 Option Menus AFCS 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. ADDITIONAL FEATURES Figure 8-50 Chart Not Available Banner APPENDICES 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. INDEX Figure 8-51 Unable To Display Chart Banner 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 421 SYSTEM OVERVIEW Additional Features When a chart is not available by pressing 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. FLIGHT INSTRUMENTS 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, pressing 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. EIS Selecting a chart: 1) While viewing the Navigation Map Page, Flight Plan Page, or Nearest Airports Page, press the SHW CHRT Softkey. The airport diagram or approach chart is displayed on the Airport Information Page. AUDIO PANEL & CNS 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. (Press the APR Softkey if the Approach Box is not currently shown). FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 8) Turn either FMS Knob to scroll through the available charts. 9) Press the ENT Key to complete the chart selection. AFCS Chart Not To Scale ADDITIONAL FEATURES Select Desired Approach Chart from Menu APPENDICES Scroll Through Chart With the Joystick INDEX Aircraft Not Shown Icon Figure 8-52 Approach Information Page, Chart Selection 422 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW While the APPROACH Box is selected using the FMS Knob, the G1000 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. FLIGHT INSTRUMENTS The aircraft symbol is not shown on FliteCharts. The Chart Scale Box displays a banner NOT TO SCALE, and the Aircraft Not Shown Icon is displayed in the lower right corner of the screen. Pressing the CHRT Softkey alternates 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. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS Press CHRT Softkey to Switch Between FliteCharts and Navigation Map Page ADDITIONAL FEATURES APPENDICES Figure 8-53 CHRT Softkey, Airport Information Page INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 423 SYSTEM OVERVIEW Additional Features Pressing the INFO Softkey returns to the airport diagram when the view is on a different chart. If the displayed chart is the airport diagram, the INFO Softkey has no effect. EIS FLIGHT INSTRUMENTS Another source for additional airport information is from the INFO Box above the chart (Figure 8-53) or to the right of the chart (Figure 8-54) for certain airports. This information source is not related to the INFO Softkey. When the INFO Box is selected using the FMS Knob, the G1000 softkeys are blank. The Charlotte, NC airport has three additional charts offering information; the Airport Diagram, Alternate Minimums, and Take-off Minimums. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS Info Box Selected INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 8-54 Airport Information Page, INFO View with Airport Information 424 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW In the example shown in Figure 8-54, TAKE OFF MINIMUMS is selected. Pressing the ENT Key displays the Take-off Minimums and Departure Procedures Chart (Figure 8-55). FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-55 Airport Information Page, TAKE OFF MINIMUMS Selected from INFO View HAZARD AVOIDANCE Pressing the DP Softkey displays the Departure Procedure Chart if available. AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 8-56 Departure Information Page 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 425 SYSTEM OVERVIEW Additional Features FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Pressing the STAR Softkey displays the Standard Terminal Arrival Chart if available. Figure 8-57 Arrival Information Page APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Pressing the APR Softkey displays the approach chart for the airport if available. INDEX Figure 8-58 Approach Information Page 426 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW Pressing 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 XM Weather subscription is current. FLIGHT INSTRUMENTS Selecting Additional Information: 1) While viewing the Airport Taxi Diagram, press 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. EIS 4) Turn the small FMS Knob to select the INFO Box choices. When the INFO Box is selected the G1000 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. AUDIO PANEL & CNS 5) Press the FMS Knob again to deactivate the cursor. FLIGHT MANAGEMENT Info Available on This Airport HAZARD AVOIDANCE WX Info When Available AFCS Chart Not To Scale Figure 8-59 Weather Information Page, WX Softkey Selected ADDITIONAL FEATURES Softkeys are Blank during Info Box Selection WX Softkey Selected APPENDICES Pressing the GO BACK Softkey reverts to the previous page (Navigation Map Page or Flight Plan Page). INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 427 SYSTEM OVERVIEW Additional Features Chart Options Pressing the CHRT OPT Softkey displays the next level of softkeys, the chart options level (Figure 8-48). EIS FLIGHT INSTRUMENTS Pressing the ALL Softkey shows the complete chart on the screen. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS Complete Chart Shown INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 8-60 Airport Information Page, ALL View Selected 428 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW Pressing 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. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Press FIT WDTH Softkey to Show Full Chart Width Figure 8-61 Approach Information Page, FIT WDTH Softkey Selected APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 429 SYSTEM OVERVIEW Additional Features FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Pressing the FULL SCN Softkey alternates between removing and replacing the data window to the right. AFCS HAZARD AVOIDANCE Press FULL SCN Softkey to Switch Between Chart on Full Screen and Chart with Info Window ADDITIONAL FEATURES Figure 8-62 Airport Information Page, Full Screen and Info Window INDEX APPENDICES Pressing the BACK Softkey, or waiting for 45 seconds reverts to the chart selection softkeys. 430 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW The full screen view can also be selected by using the page menu option. Selecting full screen On or Off: FLIGHT INSTRUMENTS 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. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Chart Setup Option Full Screen On/Off Selection HAZARD AVOIDANCE Figure 8-63 Page Menus AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 431 SYSTEM OVERVIEW Additional Features Day/Night View FLIGHT INSTRUMENTS 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 G1000 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. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key. HAZARD AVOIDANCE Figure 8-64 Waypoint Information Page, OPTIONS Menu 3) Turn the large FMS Knob to move to the COLOR SCHEME Option (Figure 8‑65). 4) Turn the small FMS Knob to choose between Day, Auto, and Night Options. AFCS 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. ADDITIONAL FEATURES 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. INDEX APPENDICES 6) Press the FMS Knob when finished to remove the Chart Setup Menu. 432 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-65 Approach Information Page, Day View HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 8-66 Approach Information Page, Night View INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 433 SYSTEM OVERVIEW Additional Features FliteCharts Cycle Number and Expiration Date FLIGHT INSTRUMENTS FliteCharts data is revised every 28 days. Charts are still viewable during a period that extends from the cycle expiration date to the disabled date. FliteCharts is disabled 180 days after the expiration date and are no longer available for viewing upon reaching the disabled date. When turning on the G1000, the Power-up Page indicates any of five different possible criteria for chart availability. These indications are whether the databases are not configured, not available, current, out of date, or disabled. See the table below for the various FliteCharts Power-up Page displays and the definition of each. AUDIO PANEL & CNS EIS Power-up Page Display Definition Blank Line. G1000 system is not configured for FliteCharts. Contact a Garmin-authorized 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. HAZARD AVOIDANCE FLIGHT MANAGEMENT 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. INDEX APPENDICES ADDITIONAL FEATURES AFCS Table 8-2 FliteCharts Power-up Page Annunciations and Definitions 434 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW Examples of four possible Power-up Page messages are shown here. ‘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. FLIGHT INSTRUMENTS 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. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT FliteCharts Database is Disabled FliteCharts Database is Not Available AFCS FliteCharts Database is Expired but Still Available HAZARD AVOIDANCE FliteCharts Database is Current and Available ADDITIONAL FEATURES APPENDICES INDEX Figure 8-67 FliteCharts Power-up Page Messages 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 435 SYSTEM OVERVIEW Additional Features NOTE: A subdued softkey label indicates the function is disabled. FLIGHT INSTRUMENTS 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. EIS 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. Press the DBASE Softkey for scrolling through the database information. Scroll through the database with the FMS knob or ENT Key. AUDIO PANEL & CNS The FliteCharts database cycle number shown in the figure, 0807, is deciphered as follows: 08 – Indicates the year 2008 07 – Indicates the seventh issue of the FliteCharts database for the year FLIGHT MANAGEMENT The FliteCharts EFFECTIVE date 05–JUL–08 is the first date that this database is current. The FliteCharts EXPIRES date 02–AUG–08 is the last date that this database is current. ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE The DISABLES date 29–JAN–09 is the date that this database becomes inoperative. APPENDICES FliteCharts Data Figure 8-68 AUX – System Status Page, FliteCharts Current and Available INDEX The FliteCharts database is provided from Garmin. Refer to Updating Garmin Databases in Appendix B for instructions on revising the FliteCharts database. 436 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW The other three possible AUX - System Status page conditions are shown here. 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. REGION and CYCLE NOT AVAILABLE in blue, indicate that FliteCharts database is not available on the database card or no database card is inserted. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT FliteCharts Database has Expired, but is not Disabled FliteCharts Database is Disabled HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES System is Configured for FliteCharts but Database is not Installed APPENDICES FliteCharts Database is Not Available 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX Figure 8-69 AUX – System Status Page, FliteCharts Expired, FliteCharts Disabled, FliteCharts Not Available 437 SYSTEM OVERVIEW Additional Features 8.5 XM Radio Entertainment (Optional) FLIGHT INSTRUMENTS Note: Refer to the Hazard Avoidance Section for information about XM Weather products. The optional XM Radio entertainment feature of the GDL 69A Data Link Receiver is available for the pilot’s ® and passengers’ enjoyment. The GDL 69A can receive XM Satellite Radio entertainment services at any altitude throughout the Continental U.S. Entertainment audio is available only on the GDL 69A Data Link Receiver, not the GDL 69. AUDIO PANEL & CNS EIS XM 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. XM Satellite Radio services are subscription-based. For more information on specific service packages, visit www.xmradio.com. Activating XM Satellite Radio Services FLIGHT MANAGEMENT The service is activated by providing XM 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 XM 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. XM 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. HAZARD AVOIDANCE These IDs are located: • On the label on the back of the Data Link Receiver • On the XM Information Page on the MFD (Figure 8-70) • On the XM Satellite Radio Activation Instructions included with the unit (available at www.garmin.com, P/N 190-00355-04) INDEX APPENDICES ADDITIONAL FEATURES AFCS Contact the installer if the Data Radio ID and the Audio Radio ID cannot be located. 438 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW NOTE: The LOCK Softkey on the XM Information Page (Auxiliary Page Group) is used to save GDL 69A FLIGHT INSTRUMENTS activation data when the XM services are initially set up. It is not used during normal XM Radio operation, but there should be no adverse effects if inadvertently pressed during flight. Refer to the GDL 69/69A XM Satellite Radio Activation Instructions (190-00355-04, Rev F or later) for further information. Activating the XM Satellite Radio services: EIS 1) Contact XM Satellite Radio through the email address listed on their website (www.xmradio.com) or by the customer service phone number listed on the website. Follow the instructions provided by XM Satellite Radio services. 2) Select the Auxiliary Page Group. 3) Select the next to last page in the AUX Page Group. AUDIO PANEL & CNS 4) Press the INFO Softkey to display the XM Information Page. 5) Verify that the desired services are activated. 6) Press the LOCK Softkey. FLIGHT MANAGEMENT 7) Turn the large FMS Knob to highlight YES. 8) To complete activation, press the ENT Key. Data Radio ID HAZARD AVOIDANCE Audio Radio ID AFCS Weather Products Window ADDITIONAL FEATURES Figure 8-70 XM Information Page APPENDICES RADIO and INFO Softkeys LOCK Softkey is Used to Save Activation Data During Initial Setup 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX If XM weather services have not been activated, all the weather product boxes are blank 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. 439 SYSTEM OVERVIEW Additional Features Using XM Radio FLIGHT INSTRUMENTS The XM Radio Page provides information and control of the audio entertainment features of the XM Satellite Radio. Selecting the XM Radio Page: 1) Turn the large FMS Knob to select the Auxiliary Page Group. 2) Turn the small FMS Knob to select the displayed AUX - XM Information Page. EIS 3) Press the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled. FLIGHT MANAGEMENT AUDIO PANEL & CNS Active Channel HAZARD AVOIDANCE Channel List Volume Field AFCS Categories Field Figure 8-71 XM Radio Page ADDITIONAL FEATURES Active Channel and Channel List The Active Channel Box on the XM Radio Page displays the currently selected channel that the XM Radio is using. APPENDICES 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, press the CHNL Softkey. INDEX 2) Press the CH + Softkey to go up through the list in the Channel Box, or move down the list with the CH – Softkey. 440 Or: Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW 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. Selecting a channel directly: FLIGHT INSTRUMENTS 1) While on the XM Radio Page, press the CHNL Softkey. 2) Press the DIR CH Softkey. The channel number in the Active Channel Box is highlighted. 3) Press the numbered softkeys located on the bottom of the display to directly select the desired channel number. EIS 4) Press the ENT Key to activate the selected channel. Category AUDIO PANEL & CNS 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: FLIGHT MANAGEMENT 1) Press the CATGRY Softkey on the XM Radio Page. 2) Press the CAT + and CAT - Softkeys to cycle through the categories. Or: HAZARD AVOIDANCE 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. AFCS ADDITIONAL FEATURES APPENDICES Figure 8-72 Categories List INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 441 SYSTEM OVERVIEW Additional Features Presets FLIGHT INSTRUMENTS Up to 15 channels from any category can be assigned a preset number. The preset channels are selected by pressing the PRESETS and MORE Softkeys. Then the preset channel can be selected directly and added to the channel list for the Presets category. Setting a preset channel number: 1) On the XM Radio Page, while listening to an Active Channel that is wanted for a preset, press the PRESETS Softkey to access the first five preset channels (PS1 - PS5). EIS 2) Press the MORE Softkey to access the next five channels (PS6 – PS10), and again to access the last five channels (PS11 – PS15). Pressing the MORE Softkey repeatedly cycles through the preset channels. 3) Press any one of the (PS1 - PS15) softkeys to assign a number to the active channel. AUDIO PANEL & CNS 4) Press the SET Softkey on the desired channel number to save the channel as a preset. FLIGHT MANAGEMENT Press PRESETS to Access the Preset Channels Softkeys Press MORE to Cycle Through the Preset Channels HAZARD AVOIDANCE Press SET to Save Each Preset Channel Figure 8-73 Accessing and Selecting XM Preset Channels Pressing the BACK Softkey, or waiting during 45 seconds of softkey inactivity, returns the system to the top level softkeys. AFCS Volume Radio volume is shown as a percentage of full volume. Volume level is controlled by pressing the VOL Softkey, which brings up the MUTE Softkey and the volume increase and decrease softkeys. ADDITIONAL FEATURES Adjusting the volume: 1) With the XM Radio Page displayed, press the VOL Softkey. APPENDICES 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.) INDEX 3) Press the MUTE Softkey to mute the audio. Press the MUTE Softkey again to unmute the audio. Figure 8-74 Volume Control 442 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW 8.6 Scheduler FLIGHT INSTRUMENTS The Scheduler feature can be used to enter and display reminder messages (e.g., Change oil, Switch fuel tanks, or Altimeter-Transponder Check) in the Alerts 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. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-75 Scheduler (Utility Page) HAZARD AVOIDANCE 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. AFCS 4) Use the FMS Knob to enter the message text to be displayed in the Alerts 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: ADDITIONAL FEATURES • 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 APPENDICES 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. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 443 SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 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. EIS 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. AUDIO PANEL & CNS 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. ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT Scheduler messages appear in the Messages Window on the PFD. When a scheduler message is waiting, the ALERTS Softkey label changes to ADVISORY. Pressing the ADVISORY Softkey opens the Messages Window and acknowledges the scheduler message. The softkey label reverts to ALERTS when pressed. Pressing the ALERTS Softkey again removes the Messages Window from the display, and the scheduler message is deleted from the message queue. INDEX APPENDICES Figure 8-76 PFD Messages Window 444 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW 8.7 Electronic Checklists FLIGHT INSTRUMENTS NOTE: The checklists presented here are for example only and may not reflect checklists actually available for the Diamond DA42NG. This material is not intended to replace the checklist information presented in the AFM or the Pilot Safety and Warning Supplements document. NOTE: Garmin is not responsible for the content of checklists. User-defined checklists are created by the EIS 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. MAP DCLTR SYSTEM DONE AUDIO PANEL & CNS (Optional) SYSTEM SHW CHRT CHKLIST EXIT EMERGCY FLIGHT MANAGEMENT The DONE Softkey label changes to UNDO when the checklist item is already checked. Figure 8-77 Checklist Softkeys HAZARD AVOIDANCE The MFD is able to display optional electronic checklists which allow a pilot to quickly find the proper procedure on the ground and during each phase of flight. The G1000 accesses the checklists from an SD card inserted into the bezel slot. If the SD card contains an invalid checklist file or no checklist, the Power-up Page messages display Invalid Checklist File or Checklist File Not Present and the CHKLIST Softkey is not available. AFCS Accessing and navigating checklists: 1) From any page on the MFD, press the CHKLIST Softkey. 2) Turn the large FMS Knob to select the GROUP field. ADDITIONAL FEATURES 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 FMS Knob to select the desired checklist and press the ENT Key. The following colors are used for checklist items: • Blue - Items has not been highlighted • Green - Item has been checked • White - Item is highlighted for checking • Yellow - Warning notes APPENDICES 6) Turn the FMS Knob to scroll through the checklist and highlight the desired checklist item. A hollow white box is used for the checkmark. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 445 SYSTEM OVERVIEW Additional Features 7) Press the ENT Key or DONE Softkey to check the highlighted 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. Press the CLR Key to remove a check mark from an item. FLIGHT INSTRUMENTS 8) Once the last item in a checklist is checked, the next highlighted item is, Go to the next checklist? Press the ENT Key to advance to the next checklist displayed. APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 9) Press the EXIT Softkey or hold down the CLR Key momentarily to exit the Checklist Page and return to the page last viewed. INDEX Figure 8-78 Sample Checklist 446 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW Immediately accessing emergency procedures: 1) From any page, press the CHKLIST Softkey. 2) Press the EMERGCY Softkey. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Figure 8-79 Emergency Checklist Page Example APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 447 SYSTEM OVERVIEW Additional Features 8.8 Abnormal Operation FLIGHT INSTRUMENTS SVS Troubleshooting SVS is intended to be used with traditional attitude, heading, obstacle, terrain, and traffic inputs. SVS is disabled when valid attitude or heading data is not available for the display. In case of invalid SVS data, the PFD display reverts to the standard blue-over-brown attitude display. SVS becomes disabled without the following data resources: EIS • Attitude data • Heading data • GPS position data AUDIO PANEL & CNS • 9 Arc-second Terrain data • Obstacle data • Terrain function is not available, in test mode, or failed FLIGHT MANAGEMENT • The position of the aircraft exceeds the range of the terrain database. Reversionary Mode INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE SVS can be displayed on the Multifunction Display (MFD) in Reversionary Mode. If it is enabled when switching to Reversionary Mode, SVS will take up to 30 seconds to be displayed. The standard, non-SVS PFD display will be shown in the interim. Figure 8-80 SVS Reversionary Mode 448 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW Unusual Attitudes FLIGHT INSTRUMENTS 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. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-81 Unusual Attitude Display The blue colored bar is also displayed when terrain gradient is great enough to completely fill the display. HAZARD AVOIDANCE Blue Band AFCS Terrain Completely Fills Display ADDITIONAL FEATURES Figure 8-82 Blue Sky Bar with Full Display Terrain APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 449 SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS • Ensure the owner/operator of the aircraft in which the Data Link Receiver is installed has subscribed to XM • Ensure the XM subscription has been activated • Perform a quick check of the circuit breakers to ensure that power is applied to the Data Link Receiver EIS 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: AUDIO PANEL & CNS 1) Turn the large FMS Knob to select the AUX Page Group. APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT 2) Turn the small FMS Knob to select the System Status Page (the last page in the AUX Page Group). INDEX Figure 8-83 LRU Information Window on System Status Page 450 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Additional Features SYSTEM OVERVIEW If a failure still exists, the following messages may provide insight as to the possible problem: NO SIGNAL LOADING OFF AIR --- Message Location XM Radio Page - active channel field XM Radio Page - active channel field XM Radio Page - active channel field Weather Datalink Page - center of page XM Radio Page - active channel field XM Radio Page - active channel field XM Radio Page - active channel field Description Data Link Receiver antenna error; service required Data Link Receiver updating encryption code FLIGHT INSTRUMENTS Message CHECK ANTENNA UPDATING Loss of signal; signal strength too low for receiver EIS Acquiring channel audio or information Channel not in service Missing channel information No communication from Data Link Receiver WEATHER DATA LINK FAILURE Weather Datalink Page - center of page within last five minutes ACTIVATION REQUIRED Weather Datalink Page - center of page XM subscription is not activated AUDIO PANEL & CNS Table 8-3 GDL 69/69A Data Link Receiver Error Messages FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 451 INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Additional Features Blank Page 452 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Appendix A SYSTEM OVERVIEW Annunciations and Alerts Note: The Aircraft Flight Manual (AFM) supersedes information found in this document. FLIGHT INSTRUMENTS The G1000 Alerting System conveys alerts using the following: EIS • Annunciation Window: The Annunciation Window displays abbreviated annunciation text. Text color is based on alert levels described in the following section. The Annunciation Window is located to the right of the Altimeter and Vertical Speed Indicator. All aircraft annunciations can be displayed simultaneously in the Annunciation Window. A white horizontal line separates annunciations that are acknowledged from annunciations that are not yet acknowledged. Higher priority annunciations are displayed towards the top of the window. AUDIO PANEL & CNS • Alerts Window: The Alerts Window displays text messages for up to 64 prioritized alert messages. Pressing the ALERTS Softkey displays the Alerts Window. Pressing the ALERTS Softkey a second time removes the Alerts Window from the display. When the Alerts Window is displayed, the FMS Knob can be used to scroll through the alert message list. FLIGHT MANAGEMENT • Softkey Annunciation: During certain alerts, the ALERTS Softkey may appear as a flashing annunciation to accompany an alert. The ALERTS Softkey assumes a new label consistent with the alert level (WARNING, CAUTION, or ADVISORY). By selecting the softkey when flashing an annunciation, the alert is acknowledged. The softkey label then returns to ALERTS. If alerts are still present, the ALERTS label is displayed in white with black text. Selecting the ALERTS Softkey a second time views the alert text messages. • System Annunciations: Typically, a large red ‘X’ appears over instruments whose information is supplied by a failed Line Replaceable Unit (LRU). See the G1000 System Annunciations Section for more information. HAZARD AVOIDANCE AFCS System Annunciation Red ‘X’ ADDITIONAL FEATURES Annunciation Window Alerts Window APPENDICES Softkey Annunciation 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX Figure A-1 G1000 Alerting System 453 SYSTEM OVERVIEW Appendix A • Audio Alerting System: The G1000 System issues audio alert tones when specific system conditions are met. See the Alert Level Definitions Section for more information. The annunciation tone may be tested from the AUX - System Status Page. FLIGHT INSTRUMENTS Testing the system annunciation tone: 1) Use the FMS Knob to select the AUX - System Status Page. 2) Select the ANN TEST Softkey. Or: EIS a) Press the MENU Key. AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS b) Highlight ‘Enable Annunciator Test Mode’ and press the ENT Key. Press to Test Annunciation Tone INDEX APPENDICES ADDITIONAL FEATURES Figure A-2 Annunciation Tone Testing (AUX-System Status Page) 454 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Appendix A SYSTEM OVERVIEW Alert Level Definitions The G1000 Alerting System uses three alert levels. • WARNING: This level of alert requires immediate attention. FLIGHT INSTRUMENTS Warning alert text is shown in red in the Annunciation Window and is accompanied by a continuous chime and a flashing ‘WARNING’ Softkey annunciation. Pressing the WARNING Softkey acknowledges the presence of the warning alert and stops the aural chime. • CAUTION: This level of alert indicates the existence of abnormal conditions on the aircraft that may require intervention. EIS Caution alert text is shown in yellow in the Annunciation Window and is accompanied by a single chime and a flashing ‘CAUTION’ Softkey annunciation. Pressing the CAUTION Softkey acknowledges the presence of the caution alert. AUDIO PANEL & CNS • ANNUNCIATION OR MESSAGE ADVISORY: This level of alert provides general information. Annunciation alert text is shown in white in the Annunciation Window; no aural tone is generated. An annunciation alert is accompanied by a flashing ADVISORY Softkey annunciation. Pressing the ADVISORY Softkey acknowledges the presence of the annunciation alert. FLIGHT MANAGEMENT Message advisory alerts do not issue annunciations in the Annunciation Window. Instead, message advisory alerts only issue a flashing ‘ADVISORY’ Softkey annunciation. Selecting the ADVISORY Softkey acknowledges the presence of the message advisory alert and displays the alert text message in the Alerts Window. HAZARD AVOIDANCE AFCS Figure A-3 Softkey Annunciation (ALERTS Softkey Labels) ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 455 SYSTEM OVERVIEW Appendix A Aircraft Alerts FLIGHT INSTRUMENTS The following alerts are configured specifically for the Diamond DA42NG. Red annunciation window text signifies warnings and yellow, cautions. See the Aircraft Flight Manual Supplement (AFMS) for recommended pilot actions. EIS Annunciation Window Text L ENG TEMP R ENG TEMP L OIL TEMP Left engine oil temp is greater than 145 deg C. R OIL TEMP Right engine oil temp is greater than 145 deg C. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS L OIL PRES R OIL PRES L ENG FIRE R ENG FIRE L GBOX TEMP R GBOX TEMP L ALTN AMPS R ALTN AMPS L STARTER R STARTER L FUEL TEMP R FUEL TEMP L FUEL PRESS R FUEL PRESS DOOR OPEN Left engine oil pressure is less than 1.5 bar. Right engine oil pressure is less than 1.5 bar. Left engine fire detected. Right engine fire detected. Left engine gearbox temp is >120 deg C. Right engine gearbox temp is >120 deg C. Left engine alternator output is >60 amps. Right engine alternator output is >60 amps. Left engine starter is engaged. Right engine starter is engaged. Left fuel temp is greater than 75 deg C. Right fuel temp is greater than 75 deg C. Left engine fuel pressure is low. Right engine fuel pressure is low. Front, rear, or baggage door is not closed. Table A-1 Warning Alerts Audio Alert Continuous Aural Tone INDEX APPENDICES ADDITIONAL FEATURES AFCS Alerts Window Message Left engine coolant temp is >105 deg C. Right engine coolant temp is >105 deg C. 456 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Appendix A Audio Alert FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS Single Aural Tone FLIGHT MANAGEMENT HAZARD AVOIDANCE Alerts Window Message Landing gear is not down and locked Left engine ECU A has failed. Right engine ECU A has failed. Left engine ECU B has failed. Right engine ECU B has failed. Left engine main tank fuel quantity is low. Right engine main tank fuel quantity is low. Left engine alternator has failed. Right engine alternator has failed. Left bus voltage is less than 25 volts. Right bus voltage is less than 25 volts. Left engine coolant level is low. Right engine coolant level is low. Left auxiliary fuel tank is empty. Right auxiliary fuel tank is empty. Pitot heat has failed. Pitot heat is off. Stall warning heat has failed. Stall warning heat is off. De-icing fluid level is low. De-icing pressure is high. De-icing pressure is low. Stick limiting system has failed. SYSTEM OVERVIEW AFCS Annunciation Window Text CHECK GEAR L ECU A FAIL R ECU A FAIL L ECU B FAIL R ECU B FAIL L FUEL LOW R FUEL LOW L ALTN FAIL R ALTN FAIL L VOLTS LOW R VOLTS LOW L COOL LVL R COOL LVL L AUX FUEL E R AUX FUEL E PITOT FAIL PITOT HT OFF STAL HT FAIL STAL HT OFF DEICE LVL LO DEIC PRES HI DEIC PRES LO STICK LIMIT Optional Table A-2 Caution Alerts Audio Alert No Tone APPENDICES Alerts Window Message Left engine glow plug active. Right engine glow plug active. Left fuel transfer from aux to main in progress. Right fuel transfer from aux to main in progress. ADDITIONAL FEATURES Annunciation Window Text L GLOW ON R GLOW ON L AUXPUMP ON R AUXPUMP ON Optional Table A-3 Advisory Alerts INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 457 SYSTEM OVERVIEW Appendix A FLIGHT INSTRUMENTS Alerts Window Message PFD FAN FAIL – The cooling fan for the PFD is inoperative. MFD FAN FAIL – The cooling fan for the MFD is inoperative. GIA FAN FAIL – The cooling fan for the GIAs is inoperative. Table A-4 Message Advisory Alerts Audio Alert No Tone Voice Alerts EIS The following audio alerts are announced by the system using a voice of male or female gender. AUDIO PANEL & CNS Voice Alert “Minimums, Minimums” “Vertical Track” “Traffic” “Traffic Not Available” Alert Trigger Issued when the aircraft transitions through the minimum descent altitude/decision height (MDA/DH) Aircraft is one minute from Top of Descent - issued only when vertical navigation is enabled TIS voice alert - issued when a Traffic Advisory (TA) is issued TIS voice alert - issued when the traffic system fails or cannot communicate FLIGHT MANAGEMENT Selecting the audio alert voice: 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 voice in the Audio Alert Box. APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE 4) Turn the small FMS Knob to select the desired voice, press the ENT Key. INDEX Figure A-4 Audio Alert (AUX - System Status Page) 458 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Appendix A SYSTEM OVERVIEW G1000 System Annunciations NOTE: Upon power-up, certain windows remain invalid as G1000 equipment begins to initialize. All windows FLIGHT INSTRUMENTS should be operational within one minute of power-up. If any window continues to remain flagged, the G1000 System should be serviced by a Garmin-authorized repair facility. When an LRU or an LRU function fails, a large red ‘X’ is typically displayed on windows associated with the failed data (refer to Figure B-1 for all possible flags and the responsible LRUs). Refer to the Aircraft Flight Manual (AFM) for additional information regarding pilot responses to these annunciations. EIS GIA 63/63W AUDIO PANEL & CNS GRS 77, GMU 44 or GIA 63/63W GDC 74A FLIGHT MANAGEMENT Database Mismatch in PFD and MFD GEA 71, GIA 63/63W, or ECU HAZARD AVOIDANCE GIA 63/63W or DME/ADF Source GIA 63/63W GDC 74A GIA 63/63W GTX 33 or GIA 63/63W AFCS Figure A-5 G1000 System Failure Annunciations ADDITIONAL FEATURES The status of detected LRUs can be checked on the AUX - System Status Page (Figure A-2). Active LRUs are indicated by green check marks; failed, by red ‘X’s. Failed LRUs should be noted and a service center or Garmin-authorized dealer informed. Viewing LRU information: 1) Use the FMS Knob to select the AUX - System Status Page. APPENDICES 2) To place the cursor in the ‘LRU Info’ Box, a) Select the LRU Softkey. Or: a) Press the MENU Key. INDEX b) With ‘Select LRU Window’ highlighted, press the ENT Key. 3) Use the FMS Knob to scroll through the box to view LRU status information. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 459 SYSTEM OVERVIEW Appendix A System Annunciation Comment System Annunciation FLIGHT INSTRUMENTS Attitude and Heading Reference System is aligning. Display system is not receiving airspeed input from air data computer. AUDIO PANEL & CNS EIS Display system is not receiving attitude information from the AHRS. Display system is not receiving vertical speed input from the air data computer. FLIGHT MANAGEMENT AHRS calibration incomplete or configuration module failure. Different versions of GDU software are installed in the PFD and MFD. This can also indicate different versions of the navigation database installed in the PFD and MFD. In some circumstances, a cross-talk error between the PFD and MFD can cause this annunciation. APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE This annunciation is seen only when the autopilot is engaged. The annunciation indicates an AHRS monitor has detected an abnormal flight parameter, possibly caused by strong turbulence. In this case, the situation should correct itself within a few seconds. If there is an actual failure, a red “X” soon appears over the Attitude Indicator. 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). Display system is not receiving valid heading input from AHRS. INDEX Display system is not receiving valid true airspeed information from air data computer. 460 Comment Display system is not receiving altitude input from the air data computer. Other Various Red X Indications Display system is not receiving valid OAT information from air data computer. Display system is not receiving valid transponder information. A red ‘X’ through any other display field (such as engine instrumentation fields) indicates that the field is not receiving valid data. Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Appendix A SYSTEM OVERVIEW G1000 System Message Advisories NOTE: This section provides information regarding G1000 message advisories that may be displayed by the FLIGHT INSTRUMENTS system. Knowledge of the aircraft, systems, flight conditions, and other existing operational priorities must be considered when responding to a message. This section describes various G1000 System message advisories. Certain messages are issued due to an LRU or LRU function failure. Such messages are normally accompanied by a corresponding red ‘X’ annunciation as shown previously in the G1000 System Annunciations section. The PFD and/or MFD self-test has detected a problem. The G1000 system should be serviced. FLIGHT MANAGEMENT The PFD and/or MFD has incorrect software installed. The G1000 system should be serviced. HAZARD AVOIDANCE The PFD configuration settings do not match backup configuration memory. The G1000 system should be serviced. The MFD configuration settings do not match backup configuration memory. The G1000 system should be serviced. The MFD and PFD have different software versions installed. The G1000 system should be serviced. AFCS The PFD and/or MFD is overheating and is reducing power consumption by dimming the display. If problem persists, the G1000 system should be serviced. ADDITIONAL FEATURES A key is stuck on the PFD and/or MFD bezel. Attempt to free the stuck key by pressing it several times. The G1000 system should be serviced if the problem persists. APPENDICES The PFD1 configuration module backup memory has failed. The G1000 system should be serviced. The PFD1 voltage is low. The G1000 system should be serviced. INDEX 190-00962-00 Rev. B Comments The pilot profile data was lost. System reverts to default pilot profile and settings. The pilot may reconfigure the MFD & PFD with preferred settings, if desired. The MFD and PFD are not communicating with each other. The G1000 system should be serviced. AUDIO PANEL & CNS Message Advisory 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. MFD1 SERVICE – MFD1 needs service. Return unit for repair. MANIFEST – PFD1 software mismatch, communication halted. MANIFEST – MFD1 software mismatch, communication halted. PFD1 CONFIG – PFD1 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. MFD1 COOLING – MFD1 has poor cooling. Reducing power usage. PFD1 KEYSTK – PFD1 [key name] is stuck. MFD1 KEYSTK – MFD1 [key name] is stuck. CNFG MODULE – PFD1 configuration module is inoperative. PFD1 VOLTAGE – PFD1 has low voltage. Reducing power usage MFD1 VOLTAGE – MFD1 has low voltage. Reducing power usage EIS Primary Flight Display & Multi Function Display The MFD voltage is low. The G1000 system should be serviced. Garmin G1000 Pilot’s Guide for the Diamond DA42NG 461 SYSTEM OVERVIEW Appendix A Databases INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Message Advisory MFD1 DB ERR – MFD1 aviation database error exists. PFD1 DB ERR – PFD1 aviation database error exists. MFD1 DB ERR – MFD1 basemap database error exists. PFD1 DB ERR – PFD1 basemap database error exists. MFD1 DB ERR – MFD1 terrain database error exists. PFD1 DB ERR – PFD1 terrain database error exists. MFD1 DB ERR – MFD1 terrain database missing. PFD1 DB ERR – PFD1 terrain database missing. MFD1 DB ERR – MFD1 obstacle database error exists. PFD1 DB ERR – PFD1 obstacle database error exists. MFD1 DB ERR – MFD1 obstacle database missing. PFD1 DB ERR – PFD1 obstacle database missing. MFD1 DB ERR – MFD1 airport terrain database error exists. PFD1 DB ERR – PFD1 airport terrain database error exists. MFD1 DB ERR – MFD1 airport terrain database missing. PFD1 DB ERR – PFD1 airport terrain database missing. MFD1 DB ERR – MFD1 Safe Taxi database error exists. PFD1 DB ERR – PFD1 Safe Taxi database error exists. MFD1 DB ERR – MFD1 Chartview database error exists. MFD1 DB ERR – MFD1 FliteCharts database error exists. 462 Comments The MFD and/or PFD detected a failure in the aviation database. Attempt to reload the aviation database. If problem persists, the G1000 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 terrain database. Ensure that the terrain card is properly inserted in display. Replace terrain card. If problem persists, the G1000 system should be serviced. The terrain database is present on another LRU, but is missing on the specified LRU. The MFD and/or PFD detected a failure in the obstacle database. Ensure that the data card is properly inserted. Replace data card. If problem persists, the G1000 system should be serviced. 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 G1000 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 G1000 system should be serviced. The MFD and/or PFD detected a failure in the ChartView database (optional feature). Ensure that the data card is properly inserted. Replace data card. If problem persists, the G1000 system should be serviced. The MFD and/or PFD detected a failure in the FliteCharts database (optional feature). Ensure that the data card is properly inserted. Replace data card. If problem persists, the G1000 system should be serviced. Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Appendix A SYSTEM OVERVIEW Comments The PFD and MFD have different aviation database versions installed. Crossfill is off. Install correct aviation database version in both displays. The PFD and MFD have different aviation database types installed (Americas, European, etc.). Crossfill is off. Install correct aviation database type in both displays. The PFD and MFD have different terrain database versions installed. Install correct terrain database version in both displays. The PFD and MFD have different terrain database types installed. Install correct terrain database type in both displays. The PFD and MFD have different obstacle database versions installed. Install correct obstacle database version in both displays. The PFD and MFD have different airport terrain databases installed. Install correct airport terrain database in both displays. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS Message Advisory DB MISMATCH – Aviation database version mismatch. Xtalk is off. DB MISMATCH – Aviation database type mismatch. Xtalk is off. DB MISMATCH – Terrain database version mismatch. DB MISMATCH – Terrain database type mismatch. DB MISMATCH – Obstacle database version mismatch. DB MISMATCH – Airport Terrain database mismatch. GIA 63W Integrated Avionics Unit The GIA1 and/or GIA2 configuration settings do not match backup configuration memory. The G1000 system should be serviced. The GIA1 and/or GIA2 have an error in the audio configuration. The G1000 system should be serviced. HAZARD AVOIDANCE The GIA1 and/or GIA2 temperature is too low to operate correctly. Allow units to warm up to operating temperature. AFCS The GIA1 and/or GIA2 temperature is too high. If problem persists, the G1000 system should be serviced. ADDITIONAL FEATURES The GIA1 and/or GIA2 self-test has detected a problem in the unit. The G1000 system should be serviced. APPENDICES A GIA mismatch has been detected, where only one is WAAS capable. Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX 190-00962-00 Rev. B Comments FLIGHT MANAGEMENT Message Advisory 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. 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. 463 SYSTEM OVERVIEW Appendix A INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Message Advisory 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. 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. 464 Comments The GIA1 and/or GIA 2 has incorrect software installed. The G1000 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 operates at reduced power. If the problem persists, the G1000 system should be serviced. The system has detected a failure in COM1 and/or COM2. COM1 and/or COM2 may still be usable. The G1000 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 G1000 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 G1000 system should be serviced. GPS integrity is insufficient for the current phase of flight. 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. Use LNAV minima when approach is downgraded. Displayed after passing the first waypoint of a true north approach when the nav angle is set to ‘MAGNETIC’. A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver may still be available. The G1000 system should be serviced. Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Appendix A A failure has been detected in the NAV1 and/or NAV2 receiver. The receiver may still be available. The G1000 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 G1000 system should be serviced. A failure has been detected in glideslope receiver 1 and/or receiver 2. The G1000 system should be serviced. EIS A failure has been detected in glideslope receiver 1 and/or receiver 2. The receiver may still be available. The G1000 system should be serviced when possible. AUDIO PANEL & CNS G/S1 SERVICE – G/S1 needs service. Return unit for repair. G/S2 SERVICE – G/S2 needs service. Return unit for repair. Comments FLIGHT INSTRUMENTS G/S2 FAIL – G/S2 is inoperative. SYSTEM OVERVIEW Message Advisory 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. FLIGHT MANAGEMENT GRS 77 Attitude and Heading Reference System Message Advisory AHRS1 TAS – AHRS1 not receiving airspeed. HAZARD AVOIDANCE 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 G1000 system should be serviced. AHRS1 GPS – AHRS1 using backup The #1 AHRS is using the backup GPS path. Primary GPS path has failed. The G1000 GPS source. system should be serviced when possible. AHRS1 GPS – AHRS1 not receiving The #1 AHRS is not receiving any or any useful GPS information. Check AFMS any GPS information. limitations. The G1000 system should be serviced. AHRS1 GPS – AHRS1 not receiving The #1 AHRS is not receiving backup GPS information. The G1000 system should be backup GPS information. serviced. AHRS1 GPS – AHRS1 operating The #1 AHRS is operating exclusively in no-GPS mode. The G1000 system should be exclusively in no-GPS mode. serviced. AHRS1 SRVC – AHRS1 Magnetic-field The #1 AHRS earth magnetic field model is out of date. Update magnetic field model model needs update. when practical. GEO LIMITS – AHRS1 too far North/ The aircraft is outside geographical limits for approved AHRS operation. Heading is South, no magnetic compass. flagged as invalid. MANIFEST – GRS1 software The #1 AHRS has incorrect software installed. The G1000 system should be serviced. mismatch, communication halted. AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 465 SYSTEM OVERVIEW Appendix A GDL 69/69A Satellite Datalink Receiver FLIGHT INSTRUMENTS Message Advisory GDL69 CONFIG – GDL 69 config error. Config service req’d. GDL69 FAIL – GDL 69 has failed. Comments GDL 69 configuration settings do not match those of backup configuration memory. The G1000 system should be serviced. A failure has been detected in the GDL 69. The receiver is unavailable. The G1000 system should be serviced. MANIFEST – GDL software mismatch, The GDL 69 has incorrect software installed. The G1000 system should be serviced. communication halted. EIS GTX 33 Transponder FLIGHT MANAGEMENT AUDIO PANEL & CNS Message Advisory XPDR1 CONFIG – XPDR1 config error. Config service req’d. MANIFEST – GTX1 software mismatch, communication halted. XPDR1 SRVC – XPDR1 needs service. Return unit for repair. XPDR1 FAIL – XPDR1 is inoperative. Comments The transponder configuration settings do not match those of backup configuration memory. The G1000 system should be serviced. The transponder has incorrect software installed. The G1000 system should be serviced. The #1 transponder should be serviced when possible. There is no communication with the #1 transponder. GDC 74A Air Data Computer AFCS HAZARD AVOIDANCE Message Advisory MANIFEST – GDC1 software mismatch, communication halted. ADC1 ALT EC – ADC1 altitude error correction is unavailable. ADC1 AS EC – ADC1 airspeed error correction is unavailable. Comments The GDC 74A has incorrect software installed. The G1000 system should be serviced. GDC1 is reporting that the altitude error correction is unavailable. GDC1 is reporting that the airspeed error correction is unavailable. GEA 71 Engine/Airframe Unit ADDITIONAL FEATURES Message Advisory GEA1 CONFIG – GEA1 config error. Config service req’d. MANIFEST – GEA1 software mismatch, communication halted. Comments The GEA1 configuration settings do not match those of backup configuration memory. The G1000 system should be serviced. The #1 GEA 71 has incorrect software installed. The G1000 system should be serviced. APPENDICES GMU 44 Magnetometer INDEX Message Advisory HDG FAULT – AHRS1 magnetometer fault has occurred. MANIFEST – GMU1 software mismatch, communication halted. 466 Comments A fault has occurred in the #1 GMU 44. Heading is flagged as invalid. The AHRS uses GPS for backup mode operation. The G1000 system should be serviced. The GMU 44 has incorrect software installed. The G1000 system should be serviced. Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Appendix A SYSTEM OVERVIEW GMA 1347 Audio Panel Message Advisory GMA1 FAIL – GMA1 is inoperative. FLIGHT INSTRUMENTS The audio panel has incorrect software installed. The G1000 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 G1000 system should be serviced when possible. EIS GMA1 CONFIG – GMA1 config error. Config service req’d. MANIFEST – GMA1 software mismatch, communication halted. GMA1 SERVICE – GMA1 needs service. Return unit for repair. Comments The audio panel self-test has detected a failure. The audio panel is unavailable. The G1000 system should be serviced. The audio panel configuration settings do not match backup configuration memory. The G1000 system should be serviced. Miscellaneous AUDIO PANEL & CNS AFCS ADDITIONAL FEATURES APPENDICES INDEX Garmin G1000 Pilot’s Guide for the Diamond DA42NG HAZARD AVOIDANCE 190-00962-00 Rev. B FLIGHT MANAGEMENT Message Advisory Comments FPL WPT LOCK – Flight plan waypoint Upon power-up, the G1000 system detects that a stored flight plan waypoint is is locked. locked. This occurs when an aviation 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. FPL WPT MOVE – Flight plan The system has detected that a waypoint coordinate has changed due to a new waypoint moved. aviation database update. Verify that stored flight plans contain correct waypoint locations. TIMER EXPIRD – Timer has expired. The system notifies the pilot that the timer has expired. DB CHANGE – Database changed. This occurs when a stored flight plan contains procedures that have been manually Verify user modified procedures. edited. This alert is issued only after an aviation database update. Verify that the user-modified procedures in stored flight plans are correct and up to date. DB CHANGE – Database changed. This occurs when a stored flight plan contains an airway that is no longer consistent Verify stored airways. with the aviation database. This alert is issued only after an aviation database update. Verify use of airways in stored flight plans and reload airways as needed. FPL TRUNC – Flight plan has been This occurs when a newly installed aviation database eliminates an obsolete approach truncated. 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. LOCKED FPL – Cannot navigate This occurs when the pilot attempts to activate a stored flight plan that contains locked flight plan. locked waypoint. Remove locked waypoint from flight plan. Update flight plan with current waypoint. WPT ARRIVAL – Arriving at waypoint Arriving at waypoint [xxxx], where [xxxx] is the waypoint name. -[xxxx] STEEP TURN – Steep turn ahead. A steep turn is 15 seconds ahead. Prepare to turn. INSIDE ARSPC – Inside airspace. The aircraft is inside the airspace. ARSPC AHEAD – Airspace ahead less Special use airspace is ahead of aircraft. The aircraft will penetrate the airspace within than 10 minutes. 10 minutes. ARSPC NEAR – Airspace near and Special use airspace is near and ahead of the aircraft position. ahead. 467 SYSTEM OVERVIEW Appendix A INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Message Advisory Comments ARSPC NEAR – Airspace near – less Special use airspace is within 2 nm of the aircraft position. than 2 nm. APR INACTV – Approach is not active. The system notifies the pilot that the loaded approach is not active. Activate approach when required. SLCT FREQ – Select appropriate The system notifies the pilot to load the approach frequency for the appropriate NAV frequency for approach. receiver. Select the correct frequency for the approach. SLCT NAV – Select NAV on CDI for The system notifies the pilot to set the CDI to the correct NAV receiver. Set the CDI to approach. the correct NAV receiver. PTK FAIL – Parallel track unavailable: Bad parallel track geometry. bad geometry. PTK FAIL – Parallel track unavailable: Invalid leg type for parallel offset. invalid leg type. PTK FAIL – Parallel track unavailable: IAF waypoint for parallel offset has been passed. past IAF. UNABLE V WPT – Can’t reach current The current vertical waypoint can not be reached within the maximum flight path vertical waypoint. angle and vertical speed constraints. The system automatically transitions to the next vertical waypoint. VNV – Unavailable. Unsupported leg The lateral flight plan contains a procedure turn, vector, or other unsupported leg type in flight plan. type prior to the active vertical waypoint. This prevents vertical guidance to the active vertical waypoint. VNV – Unavailable. Excessive The current crosstrack exceeds the limit, causing vertical deviation to go invalid. crosstrack error. VNV – Unavailable. Excessive track The current track angle error exceeds the limit, causing the vertical deviation to go angle error. invalid. VNV – Unavailable. Parallel course A parallel course has been selected, causing the vertical deviation to go invalid. selected. NO WGS84 WPT – Non WGS 84 The selected waypoint [xxxx] does not use the WGS 84 datum. Cross-check position waypoint for navigation -[xxxx] with alternate navigation sources. TRAFFIC FAIL – Traffic device has The G1000 is no longer receiving data from the traffic system. The traffic device failed. should be serviced. STRMSCP FAIL – Stormscope has Stormscope has failed. The G1000 System should be serviced. failed. FAILED PATH – A data path has A data path connected to the GDU or the GIA 63/63W has failed. failed. MAG VAR WARN – Large magnetic The GDU’s internal model cannot determine the exact magnetic variance for variance. Verify all course angles. geographic locations near the magnetic poles. Displayed magnetic course angles may differ from the actual magnetic heading by more than 2°. SCHEDULER [#] – . Message criteria entered by the user. SVS – SVS DISABLED: Out of available Synthetic Vision is disabled because the aircraft is not within the boundaries of the terrain region. installed terrain database. SVS – SVS DISABLED: Terrain DB Synthetic Vision is disabled because a terrain database of sufficient resolution (9 arcresolution too low. second or better) is not currently installed. 468 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Appendix A SYSTEM OVERVIEW AFCS Status Annunciations FLIGHT INSTRUMENTS The following annunciations (listed in order of increasing priority) can appear on the PFD above the Airspeed and Attitude indicators. Only one annunciation may occur at a time, and messages are prioritized by criticality. AFCS Status Annunciation EIS AUDIO PANEL & CNS Figure A-6 AFCS Status Annunciation Rudder Mistrim Right Rudder Mistrim Left Aileron Mistrim Right Elevator Mistrim Down Elevator Mistrim Up (or Stuck AP TRIM Switch) Roll servo providing sustained force in indicated direction Pitch servo providing sustained force in the indicated direction If AP engaged, take control of the aircraft and disengage AP If AP disengaged, move AP TRIM switches separately to unstick YD control failure Roll Failure Roll axis control failure; AP inoperative Pitch Failure Pitch axis control failure; AP inoperative Preflight Test AP and MET are unavailable; FD may still be available APPENDICES System Failure ADDITIONAL FEATURES Yaw Damper Failure Yaw servo providing sustained force in the indicated direction AFCS Pitch Trim Failure Description HAZARD AVOIDANCE Aileron Mistrim Left Annunciation FLIGHT MANAGEMENT Alert Condition INDEX Performing preflight system test; aural alert sounds at completion Do not press the AP DISC Switch during servo power-up and preflight system tests as this may cause the preflight system test to fail or never to start (if servos fail their power-up tests). Power must be cycled to the servos to remedy the situation. Preflight system test failed; aural alert sounds at failure 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 469 SYSTEM OVERVIEW Appendix A SVS Terrain Alerts FLIGHT INSTRUMENTS Annunciations appear on the PFD and MFD. Pop-up alerts appear only on the MFD. For more information on SVS Terrain, refer to the Hazard Avoidance Section. PFD/MFD TERRAIN-SVS Page Annunciation Alert Type Pop-Up Alert (MFD Navigation Map Page) HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 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) Aural Message “Warning; Terrain, Terrain” “Warning; Terrain, Terrain” “Warning; Obstacle, Obstacle” “Warning; Obstacle, Obstacle” “Caution; Terrain, Terrain” “Caution; Terrain, Terrain” “Caution; Obstacle, Obstacle” “Caution; Obstacle, Obstacle” AFCS SVS Terrain Status Annunciations PFD/MFD TERRAIN-SVS Page Annunciation Alert Type “Terrain System Failure” ADDITIONAL FEATURES System Test Fail Terrain Alerting is disabled None No GPS position or excessively degraded GPS signal “Terrain System Not Available” None APPENDICES System Test in progress None None “Terrain System Test OK” “Terrain System Available” INDEX System Test pass GPS signal is re-established Aural Message 470 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Appendix B SYSTEM OVERVIEW SD Card Use and Databases FLIGHT INSTRUMENTS The G1000 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 aviation and ChartView database updates. CAUTION: Do not load Jeppesen navigation data (except ChartView) onto Garmin Supplemental Data Cards. EIS NOTE: Loading a database in the system prior to it’s 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. AUDIO PANEL & CNS Jeppesen Databases The Jeppesen aviation database is updated on a 28-day cycle. The optional ChartView database is updated on a 14-day cycle. If the ChartView database is not updated within 70 days of the disable date, ChartView no longer functions. FLIGHT MANAGEMENT Both of these databases are provided directly from Jeppesen. The ChartView database should be copied to the Garmin supplied Supplemental Data Card which resides in the bottom card slot on the MFD. The aviation database must be installed from the Jeppesen or user supplied SD data card. Contact Jeppesen (www.jeppesen. com) for subscription and update information. HAZARD AVOIDANCE NOTE: After the aviation database is installed, the card may be removed. Updating the Jeppesen aviation database: 1) With the G1000 System OFF, insert the SD card containing the aviation database update into the top card slot of the PFD to be updated (label of SD card should face left). AFCS 2) Turn the G1000 System ON. A prompt similar to the following is displayed in the upper left corner of the PFD: ADDITIONAL FEATURES Figure B-1 Database Update Prompt APPENDICES 3) Press the ENT Key to start the database update. A prompt similar to the following is displayed: INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 471 FLIGHT INSTRUMENTS SYSTEM OVERVIEW Appendix B EIS Figure B-2 Database Update Confirmation 4) After the update completes, the PFD continues to power-up normally. AUDIO PANEL & CNS 5) Turn the G1000 System OFF and remove the SD card. 6) Repeat steps 1 through 4 for the MFD. The MFD and PFD databases are now updated. Remove the SD card when finished. FLIGHT MANAGEMENT 7) Verify the correct update cycle is loaded during MFD power-up. Garmin Databases NOTE: The data contained in the terrain and obstacle databases comes from government agencies. Garmin HAZARD AVOIDANCE accurately processes and cross-validates the data, but cannot guarantee the accuracy and completeness of the data. The following G1000 databases are stored on Supplemental Data Cards provided by Garmin: • Expanded basemap –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. AFCS • Terrain – The terrain database contains terrain mapping data. It is updated periodically and has no expiration date. ADDITIONAL FEATURES • Airport terrain – The airport terrain database contains increased resolution terrain data around airports. It is updated periodically and has no expiration date. APPENDICES • Obstacle – 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. • SafeTaxi – 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. INDEX • FliteCharts – 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 disable date, FliteCharts no longer functions. 472 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Appendix B SYSTEM OVERVIEW PFD FLIGHT INSTRUMENTS Since these databases are not stored internally in the PFD or MFD, a Supplemental Data Card containing identical database versions must be kept in each display unit. After subscribing to the desired databases product, these database products will be downloaded to two Supplemental Data Cards (with the exception of FliteCharts, which is loaded on only one card). Insert each Supplemental Data Card into the correct location shown in Figure B-3. If one of the Supplemental Data Cards contains the ChartView database, or the FliteCharts database, this card must be inserted into the bottom card slot on the MFD. These cards must not be removed except to update the databases stored on each card. MFD EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure B-3 Correct Database Locations AFCS ADDITIONAL FEATURES The Garmin database updates can be obtained by following the instructions detailed in the ‘Aviation Databases’ section of the Garmin website (www.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 the existing Supplemental Data Cards. The following equipment is required to perform the update: • Windows-compatible PC computer (Windows 2000 or XP recommended) • SanDisk SD Card Reader, P/Ns SDDR-93 or SDDR-99 or equivalent card reader APPENDICES • Updated database obtained from the Garmin website • Existing 010-00330-42 Supplemental Database SD Cards from both PFD and MFD 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. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 473 SYSTEM OVERVIEW Appendix B Updating Garmin databases: 1) Copy the data to the appropriate data cards. FLIGHT INSTRUMENTS 2) Insert one SD card in the bottom card slot of the MFD and one in the bottom card slot of each PFD. The SD card containing the ChartView or FliteCharts database must be inserted into the bottom slot on the MFD. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 3) Apply power to the G1000 System. View the MFD power-up screen. Check that the databases are initialized and displayed on the power-up screen. When updating the terrain and FliteCharts databases, an ‘in progress’ message may be seen. If this message is present, wait for the system to finish loading before verifying the correct databases are initialized, then proceed to step 4. HAZARD AVOIDANCE Figure B-4 Database Information on the Power-up Screen 4) Acknowledge the Power-up screen agreement by pressing the ENT Key or the right most softkey. 5) Use the FMS Knob to select the AUX - System Setup Page. AFCS 6) Select the DBASE Softkey to place the cursor in the ‘Database’ box. 7) Turn the FMS Knob to scroll through the list and check that all databases are current and there are no errors. INDEX APPENDICES ADDITIONAL FEATURES 8) Power down the G1000. 474 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Appendix C SYSTEM OVERVIEW Glossary ADDITIONAL FEATURES APPENDICES INDEX Garmin G1000 Pilot’s Guide for the Diamond DA42NG AFCS 190-00962-00 Rev. B barometric altitude barometric setting battery backcourse HAZARD AVOIDANCE B ALT BARO BATT BC FLIGHT MANAGEMENT ATK AUTOSEQ AUX AWOS The compass direction from the present position to a destination waypoint BFO beat frequency oscillator BKSP backspace 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 AUDIO PANEL & CNS ATC ATCRBS ATIS Bearing EIS AIM AIRMET ALRT ALT ALT, ALTN AMPS ANNUNC ANT AP AP DISC APR APT ARINC ARSPC ARTCC ARV AS ASB ASOS accuracy active, activate air data computer Automatic Direction Finder Attitude Direction Indicator Arc to fix Automatic Flight Control System Airplane Flight Manual Airplane Flight Manual Supplement airframe Above Ground Level Attitude and Heading Reference System Airman’s Information Manual Airman’s Meteorological Information alert altitude alternator amperes annunciation antenna autopilot autopilot disconnect approach airport, aerodrome Aeronautical Radio Incorporated airspace Air Route Traffic Control Center arrival airspeed Aviation Support Branch Automated Surface Observing System Air Traffic Control ATC Radar Beacon System Automatic Terminal Information Service along-track automatic sequence auxiliary Automated Weather Observing System FLIGHT INSTRUMENTS ACC ACT, ACTV ADC ADF ADI AF AFCS AFM AFMS AFRM AGL AHRS 475 SYSTEM OVERVIEW Appendix C FLIGHT INSTRUMENTS Cumulative CVR CVRG CWS CYL The total of all legs in a flight plan. Cockpit Voice Recorder coverage control wheel steering cylinder density altitude database decibels ‘Z’ (radar return) declutter decrease fuel degree de-icing departure 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 ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS D ALT DB, DBASE dBZ DCLTR, DECLTR DEC FUEL deg DEIC, DEICE DEP Desired Track APPENDICES E ECU Efficiency INDEX EGT EIS ELEV ELEV EMERGCY EMI ENDUR 476 empty, east Engine Control Unit A measure of fuel consumption, expressed in distance per unit of fuel Exhaust Gas Temperature Engine Indication System elevation elevator emergency Electromagnetic Interference endurance Endurance Flight endurance, or total possible flight time based on available fuel on board ENG engine ENGD engaged ENR enroute 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 FA FAA FADEC FAF FAIL FC FCC FCST FD FD FDE FFLOW FIS-B FISDL FL FLC FM degrees Fahrenheit Course From Fix to Altitude Federal Aviation Administration Full Authority Digital Engine Control Final Approach Fix failure Course From Fix to Distance Federal Communication Commission forecast Course From Fix to DME Distance flight director Fault Detection and Exclusion fuel flow Flight Information ServicesBroadcast Flight Information Service Data Link flight level Flight Level Change Course From Fix to Manual Termination Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Appendix C ADDITIONAL FEATURES APPENDICES key stuck kilogram Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX 190-00962-00 Rev. B AFCS KEYSTK kg HAZARD AVOIDANCE Hold Terminating at Altitude heading Groundspeed FLIGHT MANAGEMENT HA HDG GMA GMT GMU GND gph GPS Grid MORA AUDIO PANEL & CNS Ground Track GRS GS GTX glideslope go-around gallon(s) gearbox Garmin Air Data Computer Garmin Satellite Data Link Garmin Display Unit Garmin Engine/Airframe Unit geographic Garmin Flight Control Garmin Integrated Avionics Unit Global Navigation Satellite Landing System Garmin Audio Panel System Greenwich Mean Time Garmin Magnetometer Unit ground gallons per hour Global Positioning System 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 The velocity that the aircraft is travelling relative to a ground position see Track Garmin Reference System Ground speed Garmin Transponder 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 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 IAU Integrated Avionics Unit 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 EIS G/S, GS GA gal, gl GBOX GDC GDL GDU GEA GEO GFC GIA GLS Heading FLIGHT INSTRUMENTS Fuel On Board Flight Management System Fuel On Board flight plan feet per minute frequency freezing Flight Service Station foot/feet The fuel flow rate, expressed in units of fuel per hour The total amount of usable fuel on board the aircraft SYSTEM OVERVIEW FMS FOB FPL fpm FREQ FRZ FSS ft Fuel Flow 477 SYSTEM OVERVIEW Appendix C kHz km kt kilohertz kilometer knot AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 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 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 directto, 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 APPENDICES ADDITIONAL FEATURES M m MAG MAG VAR MAHP MAN IN MAN SQ MAP MASQ MAX MAXSPD MDA INDEX MET METAR 478 Middle Marker meter Magnetic Magnetic Variation Missed Approach Hold Point manifold pressure (inches Hg) Manual Squelch Missed Approach Point Master Avionics Squelch maximum maximum speed (overspeed) barometric minimum descent altitude manual electric trim 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 MSG message MSL Mean Sea Level MT meter mV millivolt(s) MVFR Marginal Visual Flight Rules N NAV NAVAID NDB NEXRAD nm NPT NRST north navigation NAVigation AID Non-directional Beacon Next Generation Radar nautical mile(s) O OAT OBS OFST OXY Outer Marker Outside Air Temperature Omni Bearing Selector offset oxygen P ALT PA PA PASS PC PFD PI PIT, PTCH POSN PPM P. POS PRES, PRESS PROC psi PT pressure altitude Passenger Address Proximity Advisory passenger(s) personal computer Primary Flight Display Procedure Turn to Course Intercept pitch position parts per million Present Position pressure procedure(s), procedure turn pounds per square inch Procedure Turn nearest Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Appendix C RAM REF REM REQ RES REV RF RMI RMT RNG RNWY ROL ROM rpm RST FUEL RSV RT RVRSNRY RX SID SIGMET 190-00962-00 Rev. B TRG TRK TRSA TRUNC Garmin G1000 Pilot’s Guide for the Diamond DA42NG INDEX Sim SLP/SKD Track Angle Error APPENDICES SD sec SEL, SLCT SFC SIAP TCA TCAS TEL TEMP TERM TF TFR T HDG TIS TIT TKE TMA TMR/REF Topo Track ADDITIONAL FEATURES SCIT south Selective Availability Static Air Temperature Satellite-Based Augmentation System Storm Cell Identification and Tracking Secure Digital second(s) select surface Standard Instrument Approach Procedures Standard Instrument Departure Significant Meteorological Information simulator slip/skid true Traffic Advisory Tactical Air Navigation System Terminal Aerodrome Forecast True Airspeed Traffic Advisory System Total Air Temperature Terrain Awareness and Warning System Terminal Control Area Traffic Collision Avoidance System telephone temperature terminal Track Between Two Fixes Temporary Flight Restriction True Heading Traffic Information System Turbine Inlet Temperature Track Angle Error Terminal Maneuvering Area Timer/Reference topographic Direction of aircraft movement relative to a ground position; also ‘Ground Track’ The angle difference between the desired track and the current track target track Terminal Radar Service Area truncated AFCS S SA SAT SBAS T TA TACAN TAF TAS TAS TAT TAWS HAZARD AVOIDANCE right, right runway radial Receiver Autonomous Integrity Monitoring random access memory reference remaining (fuel remaining) required reserve (fuel reserve entered by pilot) reverse, revision, revise Constant Radius Turn to Fix Radio Magnetic Indicator remote range runway roll read only memory revolutions per minute reset fuel reserve (fuel reserve entered by pilot) right reversionary receive FLIGHT MANAGEMENT R RAD RAIM AUDIO PANEL & CNS quantity symbol speed Special Position Identification speaker squelch service stall Standard Terminal Arrival Route statistics standby standard Stormscope Special Use Airspace suspend Synthetic Vision System software system EIS QTY SMBL SPD SPI SPKR SQ SRVC, SVC STAL STAR STATS STBY STD STRMSCP SUA SUSP SVS SW SYS FLIGHT INSTRUMENTS parallel track Push-to-Talk power SYSTEM OVERVIEW PTK PTT PWR 479 FLIGHT INSTRUMENTS SYSTEM OVERVIEW Appendix C TTL TURN TX total procedure turn transmit UNAVAIL USR UTC UTM/UPS unavailable user Coordinated Universal Time Universal Transverse Mercator/ Universal Polar Stereographic Grid VPL VPROF VPTH VR VS VSI VSR VTF Heading Vector to Manual Termination Visual Meteorological Conditions vertical navigation volume VHF Omni-directional Range very high frequency omnidirectional range station and tactical air navigation Vertical Protection Level VNV profile, vertical profile VNV path, vertical path Heading Vector to Radial vertical speed Vertical Speed Indicator Vertical Speed Required vector to final W WAAS WGS-84 WPT WW WX watt(s), west Wide Area Augmentation System World Geodetic System - 1984 waypoint(s) world wide weather XFER, XFR XPDR XTALK XTK transfer transponder cross-talk cross-track VMC VNAV, VNV VOL VOR VORTAC INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 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 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 480 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Appendix D SYSTEM OVERVIEW Frequently Asked Questions FLIGHT INSTRUMENTS If a particular aspect of G1000 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 WAAS? EIS The Wide Area Augmentation System (WAAS) 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 one of two geostationary satellites. This correction information can then be received by any WAAS-enabled GPS receiver. AUDIO PANEL & CNS WAAS is designed to provide the additional accuracy, availability, and integrity necessary to enable users to rely on GPS for all phases of flight. WAAS is currently available in the United States, including Alaska and Hawaii. How does WAAS affect approach operations? FLIGHT MANAGEMENT Both LNAV/VNAV and LPV approaches use the accuracy of WAAS 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. HAZARD AVOIDANCE 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 WAAS. 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. If WAAS is not available for the final approach course, the approach downgrades, as indicated by the “Approach downgraded. Use LNAV minima.” message. AFCS What is RAIM and how does it affect approach operations? When WAAS is unavailable, the GPS receivers use Receiver Autonomous Integrity Monitoring (RAIM) to perform the following functions: ADDITIONAL FEATURES • Monitor and verify integrity and geometry of tracked GPS satellites • Notify pilot when satellite conditions do not provide necessary coverage to support a certain phase of flight • Predict satellite coverage of a destination area to determine whether the number of available satellites is sufficient to satisfy requirements (refer to the System Overview Section for instructions on RAIM prediction) APPENDICES • Detect and exclude bad satellites from the navigation solution (Fault Detection and Exclusion, FDE) RAIM ensures that satellite geometry allows for a navigation solution calculation within a specified protection limit (4.0 nm for oceanic, 2.0 nm for enroute, 1.0 nm for terminal, and 0.3 nm for non-precision approaches). Without WAAS or RAIM, GPS position accuracy integrity cannot be monitored. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 481 SYSTEM OVERVIEW Appendix D Why might there be no approaches available for a flight plan? FLIGHT INSTRUMENTS 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 G1000 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? EIS 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 enroute 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 MANAGEMENT AUDIO PANEL & CNS 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 G1000 uses the waypoint information from the current database to define the waypoints. If the database is changed or updated, the G1000 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 G1000? HAZARD AVOIDANCE “/G” may be filed for a flight plan. GPS approaches are not to be flown with an expired database. See the approved Airplane Flight Manual (AFM) as well as the Aeronautical Information Manual (AIM) for more information. What does the OBS Softkey do? 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 INDEX APPENDICES ADDITIONAL FEATURES AFCS 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 G1000 automatically activates the next waypoint in the flight plan once the aircraft has crossed the present active waypoint. 482 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Appendix D SYSTEM OVERVIEW When OBS mode is active, the G1000 allows the pilot to set a desired course to/from a waypoint using the CRS/BARO Knob and HSI (much like a VOR). FLIGHT INSTRUMENTS The most common application for using the OBS Softkey is the missed approach. The G1000 suspends automatic waypoint sequencing (indicated by a ‘SUSP’ annunciation placed on the HSI) when the missed approach point (MAP) is crossed. This prevents the G1000 from automatically sequencing to the missed approach holding point (MAHP). During this time, the OBS Softkey designation changes to SUSP. Selecting the SUSP Softkey reactivates automatic waypoint sequencing. The OBS Softkey then resumes its normal functionality. Why might the G1000 not automatically sequence to the next waypoint? EIS AUDIO PANEL & CNS The G1000 only sequences flight plan waypoints when automatic sequencing is enabled (i.e., no ‘OBS’ or ‘SUSP’ annunciation on the HSI). 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? FLIGHT MANAGEMENT The G1000 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? HAZARD AVOIDANCE The G1000 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. AFCS • 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. ADDITIONAL FEATURES • The To/From indicator on the HSI flips momentarily to indicate that the midpoint of the turn has been crossed. When does the CDI scale change? APPENDICES Once a departure is activated, the G1000 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. INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 483 SYSTEM OVERVIEW Appendix D Why does the HSI not respond like a VOR when OBS mode is active? FLIGHT INSTRUMENTS 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? EIS To comply with TSO specifications, the G1000 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. All published missed approach procedures must be followed, as indicated on the approach plate. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 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 G1000 directs the pilot back to the transition waypoint and does not take into consideration any missed approach procedures, if the current approach is reactivated. HAZARD AVOIDANCE 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 G1000 provides navigation along the desired course to the waypoint and rejoins the approach in sequence from that point. AFCS 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. INDEX APPENDICES ADDITIONAL FEATURES 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. 484 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Appendix E SYSTEM OVERVIEW General TIS Information Introduction FLIGHT INSTRUMENTS NOTE: Aircraft without an operating transponder are invisible to TIS. EIS 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 G1000 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 G1000 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. AUDIO PANEL & CNS TIS VS. TAS/TCAS FLIGHT MANAGEMENT The Traffic Information System (TIS) requires contact with a ground station through a data link 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. HAZARD AVOIDANCE 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 should not be used for avoidance maneuvers during instrument meteorological conditions (IMC) or when there is no visual contact with the intruder aircraft. AFCS Note: Refer to the TIS Limitations section of the Aeronautical Information Manual (AIM) for a more comprehensive explanation of limitations and anomalies associated with TIS. ADDITIONAL FEATURES APPENDICES 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 meteorological 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. INDEX • 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. 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 485 SYSTEM OVERVIEW Appendix E WARNING: Garmin is not responsible for Mode S geographical coverage. Operation of the ground stations FLIGHT INSTRUMENTS 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. AUDIO PANEL & CNS EIS 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: FLIGHT MANAGEMENT • 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. HAZARD AVOIDANCE These are rare occurrences and are typically resolved within a few radar sweeps once the client/intruder aircraft course stabilizes. AFCS 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 INDEX APPENDICES ADDITIONAL FEATURES • 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). 486 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Appendix F SYSTEM OVERVIEW Map Symbols Airports Basemap Item Symbol Unknown Airport Interstate Highway Non-towered, Non-serviced Airport State Highway FLIGHT INSTRUMENTS Item Symbol EIS US Highway Towered, Non-serviced Airport National Highway Non-towered, Serviced Airport AUDIO PANEL & CNS City Towered, Serviced Airport State/Province Border Restricted (Private) Airport Heliport FLIGHT MANAGEMENT International Border Road Railroad NAVAIDS Symbol HAZARD AVOIDANCE Item Latitude/Longitude Intersection LOM (compass locator at outer marker) Airspace Boundaries Mode C Tower Area VOR/ILS VORTAC 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 APPENDICES TACAN ADDITIONAL FEATURES VOR/DME Symbol AFCS VOR Item ICAO Control Area Class B Airspace NDB (non-directional radio beacon) Military Operations Area (MOA) INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 487 SYSTEM OVERVIEW Appendix F Hazard Avoidance Features FLIGHT INSTRUMENTS Feature Symbol Item Terrain Proximity/TAWS display enabled Non-threat Traffic Traffic display enabled Proximity Advisory NEXRAD display enabled Traffic Advisory, Out of Range Cloud Top display enabled EIS Traffic Symbol Traffic Advisory AUDIO PANEL & CNS Echo Top display enabled Miscellaneous XM Lightning display enabled Item Cell Movement display enabled FLIGHT MANAGEMENT SIGMETs/AIRMETs display enabled METARs display enabled HAZARD AVOIDANCE Surface Analysis display enabled Map Pointer (when panning) Measuring Pointer Wind Vector Freezing Levels display enabled AFCS ARTCC Frequency or FSS Frequency Elevation Pointer (on Topography Scale when panning) City Forecast display enabled ADDITIONAL FEATURES Symbol Winds Aloft display enabled Overzoom Indicator County Warnings display enabled User Waypoint Cyclone Warnings display enabled Vertical Navigation Along Track Waypoint Loss of hazard avoidance feature (loss of GPS position) Parallel Track Waypoint APPENDICES Unanchored Flight Path Waypoint Top of Descent (TOD) INDEX Bottom of Descent (BOD) Navigating using Dead Reckoning 488 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Appendix F SYSTEM OVERVIEW Terrain And Obstacle Colors and Symbols Terrain Above Aircraft Altitude FLIGHT INSTRUMENTS Red terrain is above or within 100 ft below the aircraft altitude Aircraft Altitude 100 ft Threshold 1000 ft Yellow terrain is between 100 ft and 1000 ft below the aircraft altitude EIS Black terrain is more than 1000 ft below the aircraft altitude Unlighted Obstacle Lighted Obstacle < 1000’ AGL > 1000’ AGL < 1000’ AGL > 1000’ AGL AUDIO PANEL & CNS Figure F-1 Terrain Proximity Color Chart Obstacle Location FLIGHT MANAGEMENT Red obstacle is above or within 100 ft below the aircraft altitude HAZARD AVOIDANCE Yellow obstacle is between 100 ft and 1000 ft below the aircraft altitude Gray obstacle is more than 1000 ft below aircraft altitude Table F-1 Obstacle Colors AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00962-00 Rev. B Garmin G1000 Pilot’s Guide for the Diamond DA42NG 489 INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Appendix F Blank Page 490 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Index A Activate a Flight Plan---------------------------------------202 Active channel-----------------------------------------------440 Active frequency--------------------------------------- 92, 101 ADF---------------------------------------------------------110 ADF ADF mode------------------------------------------ 110, 112 ANT mode-------------------------------------------------112 Volume-----------------------------------------------------110 ADF audio----------------------------------------------------102 ADF/BFO-----------------------------------------------------112 ADF/DME tuning--------------------------------------------113 ADF frequency tuning--------------------------------------111 ADF volume--------------------------------------------------112 AHRS--------------------------------------------------- 465, 466 Aircraft range------------------------------------------------- 84 Air Data Computer (ADC)------------------------------------ 3 Airport Information-----------------------------------------------164 Airspace Alerts--------------------------------- 178, 179, 269 Airspeed indicator---------------------------------------46, 48 Airspeed Reference-----------------------------------------344 Airways Collapsed--------------------------------------------------215 Expanded--------------------------------------------------215 Alerting system----------------------------------------------453 Alert levels---------------------------------------------------455 Alerts---------------------------------------------------------453 Aircraft-----------------------------------------------------456 Audio voice-----------------------------------------------458 Alerts window------------------------------------------------ 71 Along Track Offset----------------------------------- 206, 207 ALT------------------------------------------------------------265 Altimeter--------------------------------------------------46, 51 Altitude Constraints----------------------------------------- 218, 252 Altitude alerting---------------------------------------------- 73 Altitude capture-------------------------------------- 341, 349 Altitude Hold Mode (ALT)----------------------------------342 Altitude Reference----------------------------- 341, 342, 349 Ammeter------------------------------------------------------ 82 Annunciations AFCS Status-----------------------------------------------469 G1000 System-------------------------------- 10, 459–460 Test tone---------------------------------------------- 12, 454 Annunciation window--------------------------------------- 47 Annunciator lights------------------------------------------121 ANT/BFO-----------------------------------------------------112 Approach-----------------------------------------------------482 Activating-------------------------------------------------231 ILS----------------------------------------------------------371 Loading--------------------------------------- 199, 228, 230 190-00962-00 Rev. B Missed-----------------------------------------------------374 Removing--------------------------------------------------231 Approach box-----------------------------------------------423 Approach Mode, AFCS------------------------ 359, 371, 372 APR softkey------------------------------------------- 230, 236 Arrival procedure-185, 197, 225, 227, 228, 230, 250, 252, 261 Attitude and Heading Reference System (AHRS)----- 3, 8, 13–14 Attitude indicator----------------------------------------46, 50 Audio alerting system--------------------------------------454 Audio Panel------------------------------------------------ 2, 10 Audio Panel fail-safe operation---------------------------127 Automatic Flight Control System (AFCS)------ 1, 333–378 Controls-------------------------------------------- 334–335 Example procedures------------------------------ 364–371 Status Annunciations------------------------------------376 Status Bar-------------------------------------------------362 Status Box-------------------------------------------------337 Automatic squelch------------------------------------------100 Autopilot----------------------------------------333, 361–362 Disconnect----------------------------------- 335, 353, 363 Auto-tuning--------------------------------------------------108 Auto-tuning, COM------------------------------------------- 95 Auto-tuning, NAV-------------------------------------------104 Auto Zoom---------------------------------------------------134 Auxiliary Pages (AUX)--------------------------------------- 31 AUX - system status page-397, 398, 418, 419, 436, 437 Aviation Symbols------------------------------------- 146, 185 B Backlighting-------------------------------------------------- 43 Barometric altimeter setting---------------------------46, 52 Bearing/distance, measuring------------------------------141 Bearing information-------------------------------------47, 59 Bearing pointer----------------------------------------------- 58 Bearing source----------------------------------------------- 59 Bus voltage--------------------------------------------------- 82 C Calibrated Airspeed-----------------------------------------233 CDI------------------------------60, 227, 241, 252, 260, 267 CELL MOV Softkey------------------------------------------287 Chart Not Available---------------------------------- 400, 421 Chart options----------------------------------------- 408, 428 Chart setup box-------------------------------------- 414, 432 ChartView--------------------------------------- 379, 399, 418 ChartView database--------------------------------- 416, 419 ChartView plan view---------------------------------------409 ChartView profile view-------------------------------------410 ChartView subscription------------------------------------418 Checklists------------------------------------41–42, 445–446 Garmin G1000 Pilot’s Guide for the Diamond DA42NG I-1 Index Checklist softkeys-------------------------------------------445 CLD TOP Softkey--------------------------------------------285 Closest Point-------------------------------------------------215 COM channel spacing--------------------------------------- 99 COM frequency box-------------------------------------89, 92 Command Bars, flight director----------------------------338 Communication (COM) frequency box------------------- 46 COM tuning failure-----------------------------------------127 Controls AFCS------------------------------------------------ 334–335 PFD/MFD------------------------------------------18–19, 28 Softkeys------------------------------------------------ 20–23 Control Wheel Steering (CWS)--------------------- 335, 362 Coolant temperature------------------------------------80, 82 Copy a Flight Plan------------------------------------------202 Course Deviation Indicator (CDI) Changing scale-------------------------------------------483 Course To Altitude------------------------------------------232 D Databases-----------------------------------------7, 8, 12, 471 Data entry------------------------------------------------ 27–28 Data Link Receiver--------------------------------------------- 4 Datalink receiver troubleshooting------------------------450 Date and time------------------------------------------------ 34 Day/Night views-------------------------------------- 414, 432 Day view----------------------------------414, 415, 432, 433 Dead reckoning---------------------------------------------- 75 DEC FUEL softkey-------------------------------------------- 85 Decision height (DH)---------------------------------------- 74 Declutter, display--------------------------------------------- 76 Declutter maps-------------------------------------------21, 26 Deice fluid----------------------------------------------------- 82 Delete Flight Plans------------------------------------------203 Deleting An entire airway----------------------------------- 204, 205 An entire procedure------------------------------ 204, 205 An individual waypoint--------------------------- 204, 205 Flight Plan Items-----------------------------------------204 Density Altitude---------------------------------------------235 Departure Procedure------------------------------195, 210, 222, 224 Select------------------------------------222, 225, 228, 231 Time--------------------------------------------------------233 Timer-------------------------------------------------------- 40 Departure procedure chart------------------------- 404, 425 Dilution of Precision (DOP)--------------------------------- 17 Direct-to-- 158, 180, 181, 182, 183, 184, 216, 217, 250, 252, 267 Display backup-------------------------------------------10, 91 Display controls----------------------------------------- 18–25 DME I-2 HOLD mode-----------------------------------------------113 NAV1 mode-----------------------------------------------113 NAV2 mode-----------------------------------------------113 Tuning mode--------------------------------------- 110, 113 DME audio---------------------------------------------------102 DME information-----------------------------------------58, 59 DR mode------------------------------------------------------ 75 E ECHO TOP Softkey------------------------------------------284 Electronic checklists----------------- 41–42, 379, 445, 446 Emergency checklist----------------------------------------447 Emergency frequency---------------------------------------127 Endurance----------------------------------------------------- 84 Engine Airframe Unit------------------------------------------ 3 Engine Indication System (EIS)------------------------ 77–86 Engine load------------------------------------------ 80, 82, 84 Engine Page-------------------------------------------------- 80 ENGINE softkey---------------------------------------------- 77 Entertainment inputs---------------------------------------125 Estimated Position Error (EPE)----------------------------- 17 F Field of View (SVS)------------------------------------------157 Flight director-----------------------------------333, 336–337 Pitch modes---------------------------------------- 339–345 Roll modes------------------------------------------------354 Flight ID----------------------------------------------- 114, 120 Flight instruments----------------------------------------45, 48 Flight Level Change Mode (FLC)------------------ 344, 368 Flight plan Closest point to reference------------------------------215 Storing-----------------------------------------------------482 Flight Plan Pages (FPL)-------------------------------------- 32 Flight timer---------------------------------------------------- 39 FliteCharts--------------------------------379, 420, 434, 472 FliteCharts database-------------------------------- 420, 436 FliteCharts functions---------------------------------------420 FliteCharts softkeys-----------------------------------------420 FPA----------------------------------------------------- 218, 257 Frequency Nearest----------------------------------------------------176 Frequency spacing------------------------------------------- 99 Frequently asked questions--------------------------------481 Fuel Calculations------------------------------------------------ 85 Efficiency--------------------------------------------------235 Endurance-------------------------------------------------235 Flow--------------------------------------------------------- 80 Flow totalizer---------------------------------------------- 85 Quantity------------------------------------------------80, 84 Remaining-------------------------------------------- 84, 235 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Index Required---------------------------------------------------235 Statistics---------------------------------------------------235 Temperature-------------------------------------------80, 84 Used--------------------------------------------------------- 84 Fuel on Board-----------------------------------------------235 Fuel Page------------------------------------------------------ 84 FUEL softkey-------------------------------------------------- 84 G GDL 69/69A-------------------------------------------------271 Gearbox temperature--------------------------------------- 82 GFC 700 AFCS--------------------------------------- 333–378 Glidepath-----------------------------------------------------265 Glidepath indicator------------------------------------------ 54 Glidepath Mode (GP)-------------------------- 350, 359, 372 Glideslope----------------------------------------------------265 Glideslope indicator----------------------------------------- 54 Glideslope Mode (GS)------------------------------- 352, 371 Global Positioning System (GPS) Navigation----------------------------------------- 180–270 Go Around Mode (GA)----------------- 335, 353, 374–375 GTX 33 Transponder----------------------------------------114 H Heading------------------------------------------------------- 46 Heading bug-------------------------------------------------- 46 Heading Select Mode (HDG)----------------------- 356, 365 HI SENS-------------------------------------------------------109 Horizontal situation indicator--------------------------46, 55 HSI double green arrow------------------------------------101 HSI magenta arrow-----------------------------------------101 HSI single green arrow-------------------------------------101 I IDENT function--------------------------------------- 116, 120 ID indicator--------------------------------------------------103 ILS approach-------------------------------------------------371 Indicated airspeed------------------------------------------- 48 Indicated Altitude-------------------------------------------233 Info box-------------------------------------------------------424 Inset map----------------------------------------------------- 47 Intersection Information---------------------------------------- 165–166 Inverting a flight plan--------------------------------------202 IOI-------------------------------------------------------------313 J Jeppesen aviation database-------------------------------471 L Land Symbols------------------------------------------------145 Line Replaceable Units (LRU)------------------------ 2–5, 11 190-00962-00 Rev. B LNAV----------------------------------------------------------241 LO SENS------------------------------------------------------109 LPV----------------------------------------------------- 241, 267 LPV approach------------------------------------------------364 M Manual Electric Trim (MET)------------------------- 333, 361 Map Panning----------------------------------------------------136 Map Pages (MAP)------------------------------------------- 30 Map symbols------------------------------------------------487 Marker beacon----------------------------------------------109 Marker beacon annunciations----------------------------- 72 MASQ processing-------------------------------------------- 87 Measurement units, changing displayed----------------- 35 Menus--------------------------------------------------------- 27 Message advisories--------- 455, 461, 462, 465, 466, 467 Minimum descent altitude (MDA)------------------------- 74 Missed Approach----------- 185, 232, 237, 241, 267, 374 Mode S------------------------------------------------ 114, 115 Mode selection softkeys-----------------------------------115 Morse code identifier---------------------------------------103 Multi Function Display (MFD)-------------------------------- 2 Controls----------------------------------------------- 18–19 Softkeys----------------------------------------------------- 25 N National Weather Service----------------------------------294 NAV1 audio--------------------------------------------------102 NAV2 audio--------------------------------------------------102 NAV frequency box------------------------------------------ 89 Navigation Database------------------------------------------- 218, 219 Map--------------------------------------------------------182 Navigation Mode, AFCS---------------- 357–358, 366–367 Navigation mode selection--------------------------------101 Navigation (NAV) frequency box-------------------------- 46 Navigation source-------------------------------------- 60–61 Navigation status box--------------------------------------- 46 Nav radio selection-----------------------------------------101 Nearest Airport-------------- 161, 162, 163, 164, 176–179, 230 Airport Minimum Runway Length---------------------164 Airports Page-------------------------------- 162, 163, 164 Airport Surface Matching-------------------------------164 VOR------------------------------------------------- 176–177 Nearest airports, frequency tuning------------------------ 95 Nearest Pages (NRST)--------------------------------------- 31 NEXRAD Softkey--------------------------------------------280 Night view--------------------------------414, 415, 432, 433 Non-path descent------------------------------348, 370–371 Normal display operation------------------------------------- 9 NOTAMs------------------------------------------------------406 Garmin G1000 Pilot’s Guide for the Diamond DA42NG I-3 Index O OBS mode----------------------------------------------------- 65 Obstacles-----------------------------------------------------463 Oil Pressure------------------------------------------------80, 82 Temperature-------------------------------------------80, 82 Omni Bearing Selector (OBS)----------------------- 482–483 Other Statistics--------------------------------------- 233, 235 Outside air temperature--------------------------------46, 67 Overspeed protection, autopilot--------------------------378 P Page groups--------------------------------------------- 29–32 Page menus--------------------------------------------------- 27 Parallel Track------------------------------------------ 208, 210 Passenger address------------------------------------------124 PA system----------------------------------------------------124 Pilot profiles--------------------------------------------- 36–37 Pitch Hold Mode (PIT)--------------------------------------340 Pitch modes, flight director------------------------- 339–345 Pitch Reference----------------------------------------------340 Power-up page--------------------------------- 417, 435, 445 Power up settings-------------------------------------------121 Power-up, system---------------------------------------------- 8 Primary Flight Display (PFD)---------------------------------- 2 Controls----------------------------------------------- 18–19 Softkeys------------------------------------------------ 20–22 Procedure examples, AFCS------------------------- 364–376 Procedure Pages (PROC)------------------------------------ 32 Q Quick tuning 121.500 MHz-------------------------------- 94 R RAIM--------------------- 16, 227, 237, 238, 239, 240, 481 Range---------------------------------------------------------155 Range, aircraft------------------------------------------------ 84 Receiver Autonomous Integrity Monitoring (RAIM)-1 6 – 1 7 , 237 Required Vertical Speed--------------------------------------------258 Vertical Speed Indicator---------------------------------258 Reversionary mode-----------------------------------------127 Reversionary Mode--------------------------------------- 9–10 ROC-----------------------------------------------------------313 Roll Hold Mode (ROL)--------------------------------------355 Roll modes, flight director-------------------------- 354–357 Roll Reference-----------------------------------------------355 RVSI---------------------------------------------------- 258, 259 RX indicator--------------------------------------------------- 93 S SafeTaxi------------------------------------379, 393, 396, 472 I-4 SafeTaxi database-------------------------------------------397 SBAS--------------------------------------------- 237, 239, 240 Scheduler----------------------------------------379–380, 443 Secure Digital (SD) card----------------------7, 41, 445, 471 Selected Altitude------------------ 341, 343, 345, 349, 364 Selected Altitude Capture Mode (ALTS)-341, 342, 343, 345 Selected Course----------------------------- 47, 56, 358, 360 Selected Heading--------------------------------- 47, 56, 356 Selecting a COM radio-------------------------------------- 92 Sequencing, automatic-------------------------------------483 Servos---------------------------------------------------------361 SIGMET-------------------------------------------------------288 Slip/Skid indicator----------------------------------------46, 50 Softkeys------------------------------------------------------- 46 LTNG-------------------------------------------------------286 MFD--------------------------------------------------------- 25 PFD----------------------------------------------------- 20–22 Sort Flight Plans---------------------------------------------202 Speaker-------------------------------------------------------121 Split COM Operation---------------------------------------125 Standby frequency-------------------------------- 92, 95, 101 ADF---------------------------------------------------------110 Standby frequency field------------------------------------- 92 Stereo headsets---------------------------------------------121 Stuck microphone-------------------------------------------127 Sunrise--------------------------------------------------------234 Sunset--------------------------------------------------------234 SVS troubleshooting----------------------------------------448 Symbols, map------------------------------------------------487 Synthetic vision (SVS)------------------------------- 379, 380 System annunciations--------------------------------- 10, 453 System Page (EIS)-------------------------------------------- 82 System power-up---------------------------------------------- 8 SYSTEM softkey---------------------------------------------- 82 System time--------------------------------------------------- 46 T Tachometer------------------------------------------ 80, 82, 84 TAF------------------------------------------------------------289 TAS------------------------------------------------------------465 TAWS---------------------------------------------------------311 Terminal procedures charts------------------------- 400, 421 Terrain--------------------------------------------------------463 Color indications-----------------------------------------489 Terrain-SVS---------------------------------------------------306 Timer Departure--------------------------------------------------- 40 Flight-------------------------------------------------------- 39 Timer, PFD generic------------------------------------------- 38 TOD---------------------------------------------- 257, 258, 264 TOPO DATA------------------------------------- 142, 143, 152 Top of Descent--------------------------------------- 257, 258 TOPO SCALE-------------------------------------------------144 Total flight hours--------------------------------------------- 84 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Index Track indicator------------------------------------------------ 55 Traffic Annunciation---------------------------------------------- 47 Traffic annunciation----------------------------------------- 72 Traffic Information Service (TIS)-------------------- 485–486 Voice alerts------------------------------------------------- 72 Transponder----------------------------------------------------- 3 Transponder code entry------------------------------------118 Transponder data box-----------------------------------87, 89 Transponder ground mode--------------------------------115 Transponder standby mode-------------------------------116 Transponder status box------------------------------------- 46 Trim adapter-------------------------------------------------361 Trim, Manual Electric-------------------------------- 333, 335 Trip Planning------------------------------------ 233, 234, 235 Trip statistics------------------------------------------ 234, 235 True Airspeed-------------------------------------- 46, 48, 235 Turn anticipation--------------------------------------------483 Turn rate indicator------------------------------------------- 58 TX indicator--------------------------------------------------- 93 U Unable to display chart----------------------------- 400, 421 Updating Garmin databases----------------------- 397, 436 Updating Jeppesen databases----------------------------418 V VDI----------------------------------------------------- 258, 259 Vertical deviation-------------------------------------------347 Vertical deviation guidance-------------------------------219 Vertical Deviation Indicator-------------------------------258 Vertical navigation------------------------------------------218 Direct-to---------------------------------------------------217 Vertical Navigation (VNV) Flight control--------------------------------------- 345–349 Vertical Path Tracking Mode (VPTH)--------345–346, 369 Vertical speed guidance-----------------------------------219 Vertical speed indicator---------------------------------46, 53 Vertical Speed Mode (VS)----------------------------------343 Vertical Speed Reference----------------------------------343 VFR code-----------------------------------------------------119 VNAV---------------------------------------------------------184 VNV---------------------------------------------------- 257, 480 VNV guidance Disabling--------------------------------------------------216 Enabling---------------------------------------------------216 VNV indications---------------------------------------------- 70 VNV Target Altitude--------------------------------- 345–348 VNV Target Altitude Capture Mode (ALTV)-------------349 Voice alerts, TIS----------------------------------------------- 72 Voice alerts, TIS Traffic------------------------------- 321, 458 Voltmeter------------------------------------------------------ 82 Volume level 190-00962-00 Rev. B ADF-------------------------------------------------- 110, 112 VOR Nearest--------------------------------------------- 176–177 VOR selection------------------------------------------------101 VSI-------------------------------------------------------------259 VS TGT------------------------------------------------- 218, 257 W WAAS-------------------------------------------- 241, 364, 463 Waypoint Automatic sequencing--------------------------- 482, 483 Skipping---------------------------------------------------483 Waypoint Pages (WPT)-------------------------------------- 30 Waypoint Selection Submenu--- 181, 187, 188, 190, 237 Wind--------------------------------------------------- 132, 154 WIND Softkey------------------------------------------------293 X XM radio--------------------------------------------------------271 Radio-------------------------------------------------------438 Receiver troubleshooting-------------------------------450 XM channel list----------------------------------------------440 XM radio entertainment-----------------------------------125 XM radio volume--------------------------------------------442 XM satellite radio------------------------------ 438, 440, 442 XM Satellite Radio--------------------------------------------- 4 XM Satellite Weather AIRMETs---------------------------------------------------288 SIGMETs---------------------------------------------------288 XM service class---------------------------------------------439 Z Zoom Auto--------------------------------------------------------134 Garmin G1000 Pilot’s Guide for the Diamond DA42NG I-5 Index Blank Page I-6 Garmin G1000 Pilot’s Guide for the Diamond DA42NG 190-00962-00 Rev. B Untitled-1 1 11/13/2007 9:15:37 AM G1000 ® Integrated Flight Deck Pilot’s Guide ® G1000 Pilot’s Guide Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p:913.397.8200 f:913.397.8282 Garmin (Europe) Ltd. Liberty House, Bulls Copse Road Houndsdown Business Park Southampton, SO40 9RB, U.K. p:44/0870.8501241 f:44/0870.8501251 Garmin Corporation No. 68, Jangshu 2nd Road Shijr, Taipei County, Taiwan p:886/02.2642.9199 f:886/02.2642.9099 www.garmin.com Diamond DA42NG Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. p:503.391.3411 f:503.364.2138 190-00962-00 Revision B Diamond DA42NG System Software 0670.02 or later
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Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches, Inches Manifest Reference Instance ID : uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:acde12c4-d8d5-11dc-a458-80fbd976a52f, uuid:acde12c4-d8d5-11dc-a458-80fbd976a52f, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:BC279A0327F2DD118C31EF1AC16E911C, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:6320FA0527F2DD118C31EF1AC16E911C, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:127CE3B97786DD11ACC09CE0FA9688DB, uuid:7CC6B2727055DD11B22F90F22C99F3D5, uuid:03FB5CCF7686DD11ACC09CE0FA9688DB, 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