Garmin Software Version 0764 09
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™ Cirrus Perspective by Garmin ® www.garmin.com Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. p:503.391.3411 f:503.364.2138 Garmin (Europe) Ltd. Liberty House, 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 Cirrus SR20/SR22/SR22T Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p:913.397.8200 f:913.397.8282 Cirrus SR20/SR22/SR22T Integrated Avionics System Pilot’s Guide SYSTEM OVERVIEW FLIGHT INSTRUMENTS ENGINE INDICATION SYSTEM AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AUTOMATIC FLIGHT CONTROL SYSTEM ADDITIONAL FEATURES APPENDICES INDEX Copyright © 2008-2010 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software 0764.09 or later for the Cirrus Perspective Integrated Avionics System. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Always refer to the FAA approved Airplane Flight Manual for a description of systems, limitations and procedures. For a complete list of Garmin manuals with corresponding part numbers and system software versions, refer to www.garmin.com. 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 For after-hours emergency, aircraft on ground (AOG) technical support for Garmin panel mount and integrated avionics systems, please contact Garmin’s AOG Hotline at 913.397.0836. 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® is a registered trademark of Garmin Ltd. or its subsidiaries. FliteCharts®, SafeTaxi®, and ESP™ are trademarks of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin. Perspective™ is a trademark of Cirrus Design Corporation; Bendix/King® and Honeywell® are registered trademarks of Honeywell International, Inc.; NavData® is a registered trademark of Jeppesen, Inc.; XM® is a registered trademark of XM Satellite Radio, Inc.; Skywatch® and Stormscope® is a registered trademark of L-3 Communications. aopa membership publications, inc. and its related organizations (hereinafter collectively “aopa”) expressly disclaim all warranties, with respect to the aopa information included in this data, express or implied, including, but not limited to, the implied warranties of merchantability and fitness for a particular purpose. The information is provided “as is” and aopa does not warrant or make any representations regarding its accuracy, reliability, or otherwise. under no circumstances including negligence, shall aopa be liable for any incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even if aopa or an aopa authorized representative has been advised of the possibility of such damages. user agrees not to sue aopa and, to the maximum extent allowed by law, to release and hold harmless aopa from any causes of action, claims or losses related to any actual or alleged inaccuracies in the information. some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations or exclusions may not apply to you. November 2010 Printed in the U.S.A. Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Limited Warranty LIMITED WARRANTY Within the warranty period, Garmin will, at its sole discretion, 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/or labor incidental to the direct repair of said product. Garmin may, at its discretion with prior approval, reimburse an authorized Garmin Service Center for associated labor costs incurred for removal and replacement of the panel mount product installed in an aircraft. The customer shall be responsible for any transportation or other cost. This warranty does not apply to: (i) cosmetic damage, such as scratches, nicks and dents; (ii) consumable parts, such as batteries, unless product damage has occurred due to a defect in materials or workmanship; (iii) damage caused by accident, abuse, misuse, water, flood, fire, or other acts of nature or external causes; (iv) damage caused by service performed by anyone who is not an authorized service provider of Garmin; or (v) damage to a product that has been modified or altered without the written permission of Garmin. In addition, Garmin reserves the right to refuse warranty claims against products or services that are obtained and/or used in contravention of the laws of any country. THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES, WHETHER EXPRESS, 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 in every case. Garmin retains the exclusive right to repair or replace (with a new or newly-overhauled replacement product) the product or 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 the nearest Service Center, call Garmin Customer Service at one of the numbers listed below. Products sold through online auctions are not eligible for warranty coverage or rebates or other special offers from Garmin. Online auction confirmations are not accepted for warranty verification. To obtain warranty service, an original or copy of the sales receipt from the original retailer is required. Garmin will not replace missing components from any package purchased through an online auction. Garmin International Inc. 1200 East 151st Street, Olathe, Kansas 66062 Telephone: (913)397-8200 Telephone Toll Free: (888)606-5482 Facsimile: (913)397-8282 Facsimile Toll Free: (800)801-4670 E-mail: orders@garmin.com avionics@garmin.com warranty@garmin.com 190-00820-06 Rev. A Garmin (Europe) Ltd. Liberty House, Bulls Copse Road, Southampton, SO40 9RB, UK Telephone: ++44 (0) 870-8501243 Telephone Toll Free: ++44 (0) 0808 238 0000 (option 5) Facsimile: ++44 (0) 238052004 E-mail: avionics.europe@garmin.com Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 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 the 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 Perspective™ PFD or other pressure altimeters in aircraft. WARNING: Do not use outdated database information. Databases used in the Perspective™ system must be updated regularly in order to ensure that the information remains current. Pilots using any outdated database do so entirely at their own risk. WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness. WARNING: Traffic information shown on system displays is provided as an aid in visually acquiring traffic. Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic. WARNING: Use of the L-3 WX-500 Stormscope® is not intended for hazardous weather penetration (thunderstorm penetration). Stormscope information, as displayed on the Perspective™, 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. ii Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Warnings, Cautions, and Notes WARNING: The Perspective™ 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 Perspective™. It is thus the responsibility of the pilot to detect such an occurrence by means of crosschecking with all redundant or correlated information available in the cockpit. WARNING: For safety reasons, Perspective™ 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 Perspective™ utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the Perspective™ 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 Perspective™ Pilot’s Guide documentation and the Pilot’s Operating Handbook. Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications from the Perspective™ 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 Perspective™ 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 variations in the earth’s magnetic field, operating the system within the following areas could result in loss of reliable attitude and heading indications. North of 72° North latitude at all longitudes. South of 70° South latitude at all longitudes. North of 65° North latitude between longitude 75° W and 120° W. (Northern Canada). North of 70° North latitude between longitude 70° W and 128° W. (Northern Canada). North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia). South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and New Zealand). 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T iii Warnings, Cautions, and Notes WARNING: Do not use GPS to navigate to any active waypoint identified as a ‘NON WGS84 WPT’ by a system message. ‘NON WGS84 WPT’ waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS (known as WGS84) and may be positioned in error as displayed. CAUTION: The PFD and MFD displays use a lens coated with a special anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an eyeglass lens cleaner that is specified as safe for anti-reflective coatings. CAUTION: The Perspective™ 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 Perspective™ panel and displays, are subject to change, and may not reflect the most current Perspective™ 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. For additional information, refer to the website at www.garmin.com/prop65. iv Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Revision Information Record of Revisions Part Number 190-00820-00 Revision A B Date 04/11/08 05/02/08 190-00820-01 C D A 05/12/08 06/04/08 09/29/08 Page Range ALL 408 through 421 v 184 and I-1 i – I-6 190-00820-02 A 11/17/08 i – I-6 190-00820-03 1TP 6/30/09 i – I-6 190-00820-04 A 2/28/10 i – I-6 190-00820-05 A 5/3/10 i – I-6 190-00820-06 A 11/15/10 i-I-6 190-00820-06 Rev. A Description Initial release Made clerical changes Made clerical changes Made update to optional equipment and made clerical changes Added Enhanced Vision System Added changes in page navigation Added new procedures for creating user waypoints Added importing and exporting flight plans Updated Warning, Caution and Advisory Alerts Added other GDU 9.12 parameters Added Flight Into Known Icing (FIKI) Added the SR20 Added other GDU 9.12 parameters Added AOPA Airport Directory Added dual navigation database capability Added database synchronization Added other GDU 10.00 parameters Added the SR22T Updated Warning and Caution Alerts Added other GDU 11.00 parameters Added GTS 33 w/ES transponder option Added GTS 800 traffic option Added other GDU 11.01 parameters Added Profile View Updated Active Flight Plan modification procedures to include the Quick Select Box and Insertion Point Indicator Updated XM Weather product status display Added Electronic Stability and Protection Added Underspeed Protection Added Selected Altitude Intercept Arc Added Hypoxia Recognition System Added integrated fuel quantity gauges Added other GDU 11.11 parameters Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T v Revision Information Blank Page vi Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Table of Contents 1.1 1.2 1.3 1.4 1.5 1.6 1.7 Section 1 System Overview Line Replaceable Units (LRU).................................. 2 System Controls....................................................... 7 PFD/MFD Controls......................................................... 7 PFD/MFD Control Unit. .................................................. 9 Audio Panel Controls................................................... 12 Softkey Function. ........................................................ 14 Secure Digital Cards.............................................. 22 System Power-up.................................................... 23 System Operation................................................... 24 Display Operation. ...................................................... 24 System Annunciations.................................................. 26 System Status............................................................. 27 AHRS Operation.......................................................... 28 GPS Receiver Operation............................................... 29 Accessing System Functionality........................... 34 Menus. ...................................................................... 34 Page Groups............................................................... 35 System Settings. ......................................................... 39 Timers........................................................................ 45 Display Backlighting.............................................. 48 Section 2 Flight Instruments 2.1 Flight Instruments.................................................. 52 Airspeed Indicator....................................................... 52 Attitude Indicator........................................................ 54 Altimeter.................................................................... 55 Vertical Speed Indicator (VSI). ...................................... 58 Vertical Deviation........................................................ 58 Horizontal Situation Indicator (HSI)............................... 59 Course Deviation Indicator (CDI)................................... 64 2.2 Supplemental Flight Data..................................... 71 Temperature Display.................................................... 71 Wind Data.................................................................. 73 Vertical Navigation (VNV) Indications. .......................... 74 2.3 PFD Annunciations and Alerting Functions......... 75 Marker Beacon Annunciations...................................... 75 Traffic Annunciation. ................................................... 75 TAWS Annunciations. .................................................. 76 Altitude Alerting. ........................................................ 77 Low Altitude Annunciation........................................... 77 Minimum Descent Altitude/Decision Height Alerting....... 78 190-00820-06 Rev. A 2.4 Abnormal Operations............................................ 79 Abnormal GPS Conditions............................................ 79 Unusual Attitudes. ...................................................... 80 3.1 3.2 3.3 3.4 4.1 4.2 4.3 4.4 4.5 Section 3 Engine Indication System EIS Display............................................................... 82 Engine Page............................................................ 85 Fuel Calculations......................................................... 89 Ice Protection Systems................................................. 91 Leaning Assist Mode.............................................. 94 EIS Display in Reversionary Mode........................ 95 System Display............................................................ 96 Section 4 Audio Panel and CNS Overview................................................................. 99 MFD/PFD Controls and Frequency Display.................... 100 GMA 347 Audio Panel Controls. ................................. 102 Control Unit.............................................................. 104 COM Operation..................................................... 106 COM Transceiver Selection and Activation. .................. 106 COM Transceiver Manual Tuning................................. 107 Quick-tuning and Activating 121.500 MHz. ................. 108 Auto-tuning the COM Frequency. ............................... 109 Frequency Spacing. ................................................... 113 Automatic Squelch.................................................... 114 Volume. ................................................................... 114 NAV Operation...................................................... 115 NAV Radio Selection and Activation............................ 115 NAV Receiver Manual Tuning. .................................... 116 Auto-tuning a NAV Frequency from the MFD. .............. 117 Auto-tuning NAV Frequencies on Approach Activation.. 121 Marker Beacon Receiver. ........................................... 122 DME Tuning.............................................................. 123 GTX 32/GTX 33 Transponder............................... 124 Transponder Controls. ............................................... 124 Transponder Mode Selection. ..................................... 125 Entering a Transponder Code...................................... 127 IDENT Function......................................................... 129 Additional Audio Panel Functions...................... 130 Power-Up. ................................................................ 130 Mono/Stereo Headsets. ............................................. 130 Speaker.................................................................... 130 Intercom. ................................................................. 130 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T vii Table of Contents Passenger Address (PA) System. ................................. 132 Clearance Recorder and Player................................... 133 Entertainment Inputs................................................. 134 Multifunction Controls............................................... 135 4.6 Audio Panel Preflight Procedure........................ 136 4.7 Abnormal Operation............................................ 137 Audio Panel Fail-safe Operation.................................. 137 Stuck Microphone..................................................... 137 COM Tuning Failure................................................... 137 5.1 5.2 5.3 5.4 5.5 5.6 viii Section 5 Flight Management Introduction ......................................................... 139 Navigation Status Box............................................... 140 Using Map Displays.............................................. 142 Map Orientation. ...................................................... 142 Map Range............................................................... 144 Map Panning............................................................ 146 Measuring Bearing and Distance. ............................... 150 Topography. ............................................................. 151 Map Symbols............................................................ 154 Airways.................................................................... 160 Track Vector.............................................................. 162 Wind Vector.............................................................. 163 Nav Range Ring........................................................ 164 Fuel Range Ring........................................................ 165 Field of View (SVS). ................................................... 166 Selected Altitude Intercept Arc.................................... 167 Destination Airport Information.................................. 168 Waypoints.............................................................. 169 Airports.................................................................... 170 Intersections............................................................. 177 NDBs. ...................................................................... 179 VORs........................................................................ 181 User Waypoints......................................................... 183 Airspaces............................................................... 189 Direct-to-Navigation . ......................................... 193 Flight Planning...................................................... 198 Flight Plan Creation................................................... 199 Adding Waypoints to an Existing Flight Plan................ 204 Adding Airways to a Flight Plan.................................. 207 Adding Procedures to a Stored Flight Plan................... 210 Flight Plan Storage.................................................... 217 Flight Plan Editing..................................................... 219 Along Track Offsets. .................................................. 223 Parallel Track. ........................................................... 225 Activating a Flight Plan Leg........................................ 228 Inverting a Flight Plan. .............................................. 229 Flight Plan Views....................................................... 230 Closest Point of FPL................................................... 232 5.7 Vertical Navigation.............................................. 233 Altitude Constraints. ................................................. 235 5.8 Procedures............................................................ 239 Departures. .............................................................. 239 Arrivals . .................................................................. 242 Approaches . ............................................................ 244 5.9 Trip Planning......................................................... 250 Trip Planning. ........................................................... 250 5.10 RAIM Prediction................................................... 254 5.11 Navigating a Flight Plan...................................... 257 5.12 Abnormal Operation............................................ 285 6.1 6.2 6.3 6.4 6.5 6.6 6.7 Section 6 Hazard Avoidance XM Satellite Weather........................................... 287 Activating Services.................................................... 288 Using XM Satellite Weather Products.......................... 289 Stormscope Lightning.......................................... 317 Setting Up Stormscope on the Navigation Map............ 317 Selecting the Stormscope Page................................... 321 Terrain Proximity.................................................. 323 Displaying Terrain Proximity Data. .............................. 324 Terrain Proximity Page............................................... 326 Terrain-SVS............................................................ 328 Displaying Terrain-SVS Data. ...................................... 329 Terrain-SVS Page....................................................... 332 Terrain-SVS Alerts...................................................... 334 System Status........................................................... 337 TAWS-B.................................................................. 338 Displaying TAWS-B Data. ........................................... 339 TAWS-B Page............................................................ 342 TAWS-B Alerts........................................................... 344 System Status........................................................... 350 Profile View Terrain.............................................. 352 Profile View Display................................................... 352 Garmin GTS 800 Traffic........................................ 354 Theory of operation................................................... 354 TAS Alerts................................................................. 358 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Table of Contents Section 7 Automatic Flight Control System 7.1 GFC 700 (Optional)............................................... 383 GFC 700 Controls...................................................... 384 Flight Director Operation. .......................................... 386 Vertical Modes.......................................................... 389 Lateral Modes........................................................... 404 Autopilot and Yaw Damper Operation......................... 412 Example Flight Plan................................................... 415 AFCS Annunciations and Alerts................................... 429 Overspeed Protection. ............................................... 430 Underspeed Protection. ............................................. 430 7.2 S-TEC Fifty Five X Autopilot (Optional)............. 432 8.4 ChartView.............................................................. 457 ChartView Softkeys. .................................................. 457 Terminal Procedures Charts........................................ 458 Chart Options........................................................... 466 Day/Night View......................................................... 472 ChartView Cycle Number and Expiration Date. ............ 474 8.5 FliteCharts............................................................. 477 FliteCharts Softkeys................................................... 477 Terminal Procedures Charts........................................ 478 Chart Options........................................................... 485 Day/Night View......................................................... 488 FliteCharts Cycle Number and Expiration Date............. 490 8.6 AOPA Airport Directory........................................ 493 AOPA Database Cycle Number and Revision................ 493 8.7 XM Radio Entertainment..................................... 495 Activating XM Satellite Radio Services. ....................... 495 Using XM Radio........................................................ 497 8.8 Scheduler............................................................... 500 8.9 Electronic Checklists............................................ 502 8.10 Flight Data Logging............................................. 505 8.11 Hypoxia Recognition with Automatic Descent Mode................................................................................ 507 Determining Pilot Alertness........................................ 507 Automatic Descent Mode........................................... 508 8.12 Electronic Stability and Protection (ESP™)........ 509 Operation................................................................. 510 8.13 Abnormal Operation............................................ 512 SVS Troubleshooting.................................................. 512 Reversionary Mode. .................................................. 512 Unusual Attitudes. .................................................... 513 Section 8 Additional Features 8.1 Synthetic Vision System (SVS)............................ 434 SVS Operation. ......................................................... 435 SVS Features............................................................. 437 Field of View............................................................. 446 8.2 Enhanced Vision System (EVS)............................ 448 Image Quality and Interpretation................................ 448 EVS Softkeys............................................................. 448 8.3 SafeTaxi................................................................. 451 SafeTaxi Cycle Number and Revision........................... 454 Appendices Annunciations and Alerts.............................................. 515 Alert Level Definitions. .............................................. 517 Aircraft Alerts. .......................................................... 518 Perspective™ Voice Alerts........................................... 521 GTS 800 Traffic Advisory System Voice Alerts................ 522 System Annunciations................................................ 522 System Message Advisories........................................ 525 GFC 700 AFCS Alerts. ................................................ 535 GFC 700 Speed Condition/Stall Alert........................... 536 System Test............................................................... 359 Operation................................................................. 360 System Status.......................................................... 367 6.8 Avidyne TAS610 Traffic.............................................. 368 TAS Symbology......................................................... 368 Displaying Traffic Data............................................... 368 Altitude Display. ....................................................... 371 Traffic Map Page Display Range.................................. 371 TAS Alerts................................................................. 373 System Status........................................................... 374 6.9 L-3 Skywatch Traffic............................................. 375 TAS Symbology......................................................... 375 Operation................................................................. 376 Displaying Traffic Data............................................... 376 Altitude Display. ....................................................... 379 Traffic Map Page Display Range.................................. 379 TAS Alerts................................................................. 381 System Status........................................................... 381 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T ix Table of Contents Terrain-SVS Alerts...................................................... 536 TAWS-B System Status Annunciations......................... 538 Flight plan Import/Export Messages............................ 539 Database Management................................................. 541 Garmin Databases..................................................... 541 Jeppesen Databases.................................................. 542 Automatic Database Synchronization.......................... 543 Loading Updated Databases. ..................................... 545 Glossary........................................................................... 553 Frequently Asked Questions......................................... 559 Map Symbols.................................................................. 563 Index Index . ...............................................................................I-1 x Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW Section 1 System Overview • GDU 1240A Primary Flight Display (PFD) • GDL 69/69A Satellite Data Link Receiver (optional) • GDU 1040A Multi Function Display (optional) • GRC 10 Remote Control (option with GDL 69A) • GIA 63W Integrated Avionics Unit • GRT 10 XM Radio Remote Transceiver (option with GDL 69A) • GDC 74A Air Data Computer (ADC) • GEA 71 Engine/Airframe Unit • GMU 44 Magnetometer • GMA 347 Audio Panel with Integrated Marker Beacon Receiver • GTX 33 Mode S Transponder (option without TIS-A) • GMC 705 AFCS Control Unit (if GFC 700 is installed) • GTP 59 Outside Air Temperature (OAT) Probe • GSA 80 AFCS Yaw Servo (if GFC 700 is installed) • GSA 81 AFCS Pitch and Roll Servos (if GFC 700 is installed) • GTA 82 Pitch Trim Adapter (if GFC 700 is installed) HAZARD AVOIDANCE • GTX 32 Transponder • GCU 478 PFD/MFD Control Unit FLIGHT MANAGEMENT • GRS 77 Attitude and Heading Reference System (AHRS) AUDIO PANEL & CNS • GDU 1040A Primary Flight Display (optional) EIS • GDU 1240A Multi Function Display (MFD) • GTX 33 Mode S Transponder with Extended Squitter (option without TIS-A) FLIGHT INSTRUMENTS The system is an integrated flight control system that presents flight instrumentation, position, navigation, communication, and identification information to the pilot through large-format displays. The system consists of the following Line Replaceable Units (LRUs): • GSM 85/86 Servo Gearboxes (if GFC 700 is installed) AFCS A top-level system block diagram is shown in Figure 1-1 (it does not include the GSM 85, GTA 82, GRC 10, or GRT 10). NOTE: Refer to the AFCS section for details on the GFC 700 AFCS. ADDITIONAL FEATURES The optional GFC 700 Automated Flight Control System (AFCS) provides the flight director (FD), autopilot (AP), yaw damper (YD - optional), and manual electric trim (MET) functions. APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 1 SYSTEM OVERVIEW System Overview 1.1 Line Replaceable Units (LRU) AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS • GDU 1240A-30/1040A-30 (1) – This unit is configured as a PFD that features a 12 or 10.4-inch LCD with 1024 x 768 resolution. The unit installed on the left/pilot side is designated as PFD. This unit communicates with the GDU 1240A-20/1040A-20 (MFD), and with the on-side GIA 63W Integrated Avionics Unit through a High-Speed Data Bus (HSDB) connection. AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT • GDU 1240A-20/1040A-20 (1) – This unit is configured as a MFD that features a 12 or 10.4-inch LCD with 1024 x 768 resolution. The unit installed on the right/copilot side is designated as MFD. This unit communicates with the GDU 1240A-30/1040A-30 (PFD), and with the on-side GIA 63W Integrated Avionics Unit through a High-Speed Data Bus (HSDB) connection. INDEX APPENDICES ADDITIONAL FEATURES • GIA 63W (2) – The Integrated Avionics Units (IAU) function as the main communication hub, linking all LRUs with the PFD. Each GIA 63W contains a GPS SBAS 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 GIA 63Ws are not paired together and do not communicate with each other directly. 2 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW • GDC 74A (1 or 2) – The Air Data Computer (ADC) processes data from the pitot/static system and outside air temperature (OAT) sensor. This unit provides pressure altitude, airspeed, vertical speed and OAT information to the system, and it communicates with the primary GIA 63W, GDU 1240A and GRS 77, using an ARINC 429 digital interface (it also interfaces directly with the primary GTP 59). FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS • GEA 71 (1) – Receives and processes signals from the engine and airframe sensors. This unit communicates with both GIA 63Ws using an RS-485 digital interface. FLIGHT MANAGEMENT HAZARD AVOIDANCE • GRS 77 (1 or 2) – The Attitude and Heading Reference System (AHRS) provides aircraft attitude and heading information via ARINC 429 to both GDUs and the primary GIA 63W. The GRS 77 contains advanced sensors (including accelerometers and rate sensors) and interfaces with the primary GMU 44 to obtain magnetic field information, with the GDC 74A to obtain air data, and with both GIA 63Ws to obtain GPS information. AHRS modes of operation are discussed later in this document. AFCS ADDITIONAL FEATURES • GMU 44 (1 or 2) – The Magnetometer measures local magnetic field and sends the data to the GRS 77 for processing to determine aircraft magnetic heading. This unit receives power directly from the GRS 77 and communicates with the GRS 77, using an RS-485 digital interface. APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 3 SYSTEM OVERVIEW System Overview FLIGHT INSTRUMENTS • GMA 347 (1) – The Audio Panel integrates NAV/COM digital audio, intercom and marker beacon controls (refer to the Audio Panel & CNS Section). This unit communicates with both GIA 63Ws, using an RS-232 digital interface. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS • GTX 32 (1) or GTX 33 (1) or GTX 33 with Extended Squitter (1) – The GTX 32 solid-state transponder provides Modes A and C capability. The GTX 33 solid-state transponder provides Modes A, B, and S capability. The GTX 33 may also also be additionally be equipped with Extended Squitter (ES) transmit capability. The transponder can be controlled from the PFD. The transponder communicates with the primary GIA 63W through an RS-232 digital interface. ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE • GTS 800 (1) – The optional GTS 800 provides real-time traffic information to the MFD (and, indirectly, to the inset map of the PFD). The GTS 800 communicates with the MFD with an HSDB connection. The GTS 800 also has an analog audio connection to the GMA 347. INDEX APPENDICES • GDL 69/69A (1) – The optional Data Link Satellite Radio Receiver provides real-time weather information to the MFD (and, indirectly, to the inset map of the PFD) as well as digital audio entertainment. The GDL 69/69A communicates with the MFD via an HSDB connection. A subscription to the XM Satellite Radio service is required to enable the GDL 69/69A capability. 4 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW • GCU 478 (1) – Provides the Flight Management System (FMS) controls for the PFD and MFD through an RS-232 digital interface. FLIGHT INSTRUMENTS • GMC 705 (1) – Provides the controls for the GFC 700 AFCS through an RS-232 digital interface allowing communication with the PFD and MFD. EIS AUDIO PANEL & CNS • GTP 59 (1 or 2) – The Temperature Probe provides Outside Air Temperature (OAT) data to the primary GDC 74A. FLIGHT MANAGEMENT HAZARD AVOIDANCE • GSA 80 (1), GSA 81 (2), and GSM 85A/86 (3) – The GSA 80 servo is used for the automatic control of yaw, while the GSA 81 servos are used for the automatic control of pitch and roll. These units interface with each GIA 63W. The GSM 85A/86 servo gearbox is responsible for transferring the output torque of the GSA 80/81 servo actuator to the mechanical flight-control surface linkage. AFCS ADDITIONAL FEATURES • GTA 82 (1) – The Pitch Trim Adapter takes input from the trim switches, GIA 63W and GSA 81 to control the DC motor to drive the aircraft trim system. APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 5 FLIGHT INSTRUMENTS SYSTEM OVERVIEW System Overview GMC 705 EIS GCU 478 GDL 69/69A (optional) GDU 1240A GDU 1040A (MFD) AUDIO PANEL & CNS (PFD) GMA 347 FLIGHT MANAGEMENT GDU 1240A GDU 1040A GTS 800 (optional) GMU 44 #2 (optional) GMU 44 #1 GRS 77 #1 HAZARD AVOIDANCE GRS 77 #2 (optional) AFCS GIA 63W #1 GIA 63W #2 VHF COM VHF NAV/LOC GPS/SBAS G/S GDC 74A #1 AFCS Mode Logic Flight Director Servo Management GTP 59 #1 GSA 82 (Pitch Trim) GSA 81 GDC 74A #2 (optional) GTP 59 #2 (optional) (Pitch & Roll) VHF COM VHF NAV/LOC GPS/SBAS G/S AFCS Mode Logic Flight Director Servo Management GSA 80 ADDITIONAL FEATURES (Yaw) GEA 71 #1 APPENDICES GTX 32/33/ 33 w/ ES INDEX Figure 1-1 Perspective™ System (LRU Configuration) 6 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW 1.2 System Controls FLIGHT INSTRUMENTS NOTE: The Audio Panel (GMA 347) and AFCS controls (GMC 705) are described in the Audio Panel & CNS and AFCS sections respectively. The system controls are located on the PFD and MFD bezels, PFD/MFD Control Unit, AFCS Control Unit and audio panel. The controls for the PFD and MFD are discussed within the following pages of this section. PFD/MFD Controls EIS PFD 1 2 AUDIO PANEL & CNS FLIGHT MANAGEMENT 3 HAZARD AVOIDANCE 4 13 MFD 15 16 6 11 7 10 8 ADDITIONAL FEATURES 14 12 AFCS 5 APPENDICES 9 13 Figure 1-2 PFD & MFD Controls INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 7 SYSTEM OVERVIEW System Overview 1 COM Frequency Transfer Key – Toggles the standby and active COM frequencies. Press and hold this key for two seconds to tune the emergency frequency (121.5 MHz) automatically into the active frequency field. 2 COM VOL/SQ Knob – Controls COM audio volume level. Volume level is shown in the COM frequency field as a percentage. Press to turn the COM automatic squelch ON and OFF. 3 Dual COM Knob – Tunes the standby frequencies for the COM transceiver (large knob for MHz; small knob for kHz). Press to switch the light blue tuning arrow between COM1 and COM2. 4 BARO Knob – Sets the altimeter barometric pressure. Press to enter standard pressure (29.92). 5 Joystick – Changes the map range when rotated. Activates the map pointer when pressed. 6 MENU Key – Displays a context-sensitive list of options. This list allows the user to access additional features or make setting changes that relate to particular pages. 7 PROC Key – Gives access to IFR departure procedures (DPs), arrival procedures (STARs) and approach procedures (IAPs) for a flight plan. If a flight plan is used, available procedures for the departure and/or arrival airport are automatically suggested. These procedures can then be loaded into the active flight plan. If a flight plan is not used, both the desired airport and the desired procedure may be selected. 8 ENT Key – Validates or confirms a menu selection or data entry. 9 Dual FMS Knob – Flight Management System Knob. Press the FMS Knob to turn the selection cursor ON and OFF. When the cursor is ON, data may be entered in the applicable window by turning the small and large knobs. The large knob moves the cursor on the page, while the small knob selects individual characters for the highlighted cursor location. 10 CLR Key – Erases information, cancels entries, or removes page menus. 11 FPL Key – Displays the active Flight Plan Page for creating and editing the active flight plan. 12 Direct-to Key ( ) – Allows the user to enter a destination waypoint and establish a direct course to the selected destination (the destination is either specified by the identifier, chosen from the active route, or taken from the map pointer position). 13 Bezel Keys – Used to select the appropriate softkey to access additional functionality. 14 Dual NAV Knob – Tunes the standby frequencies for the NAV receiver (large knob for MHz; small knob for kHz). Press to switch the light blue tuning arrow between NAV1 and NAV2. 15 NAV VOL/ID Knob – Controls NAV audio volume level. Press to toggle the Morse code identifier audio ON and OFF. Volume level is shown in the NAV frequency field as a percentage. 16 NAV Frequency Transfer Key – Toggles the standby and active NAV frequencies. INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS The following list provides an overview of the controls located on the PFD and MFD bezel (see Figure 1-2). 8 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW PFD/MFD Control Unit The additional controls for the PFD and MFD are located on the PFD/MFD Control Unit (GCU 478). The following list provides an overview of the controls located on the PFD/MFD Control Unit: 2 3 4 5 6 7 8 9 10 FLIGHT INSTRUMENTS 1 11 21 12 EIS 13 20 AUDIO PANEL & CNS 14 19 17 16 FLIGHT MANAGEMENT 18 15 Figure 1-3 PFD/MFD Control Unit (GCU 478) Direct-to Key ( ) – Allows the user to enter a destination waypoint and establish a direct course to the selected destination (the destination is either specified by the identifier, chosen from the active route, or taken from the map pointer position). 4 MENU Key – Displays a context-sensitive list of options. This list allows the user to access additional features or make setting changes that relate to particular pages. 5 PROC Key – Gives access to IFR departure procedures (DPs), arrival procedures (STARs) and approach procedures (IAPs) for a flight plan. If a flight plan is used, available procedures for the departure and/or arrival airport are automatically suggested. Theses procedures can then be loaded into the active flight plan. If a flight plan is not used, both the desired airport and the desired procedure may be selected. 6 ENT Key – Validates or confirms a menu selection or data entry. 7 FMS/XPDR/COM/NAV Key – Acts as the FMS Knob for the MFD. Sets the transponder code when in XPDR mode. Acts as the COM Knob when in COM tuning mode. Acts as the NAV Knob when in NAV tuning mode. 8 FMS Key – Selects/deselects FMS mode. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX 3 APPENDICES FPL Key – Displays the active Flight Plan Page for creating and editing the active flight plan, or for accessing stored flight plans. ADDITIONAL FEATURES 2 AFCS CLR Key – Erases information, cancels entries, or removes page menus. Pressing and holding this key displays the Navigation Map Page automatically. HAZARD AVOIDANCE 1 9 9 COM Key – Selects/deselects COM tuning mode. 10 XPDR Key – Selects/deselects XPDR mode. 11 NAV Key – Selects/deselects NAV tuning mode. 12 Joystick – Changes the map range when rotated. Activates the map pointer when pressed. Moves the Quick Select Box or cursor on the Active Flight Plan Page on the MFD when joystick is moved left, right, up, or down. 13 Frequency Transfer Key (EMERG) – Transfers between active and standby COM or NAV tuning frequencies. Selects/deselects NAV tuning mode. Press and hold 2 seconds to tune the emergency frequency (121.5 MHz) automatically into the active frequency field. 14 Alphanumeric Keys – Allow the user to enter data quickly, without having to select individual characters with the FMS Knob. When the Quick Select Box is shown on the Active Flight Plan Page on the MFD, alphanumeric keys can be used to enter data into the Quick Select Box area. 15 Plus (+) Minus (-) Key – Toggles a (+) or (-) character. 16 Decimal Key – Enters a decimal point. 17 BKSP Key – Moves the cursor back one character space. 18 SPC Key – Adds a space character. 19 ALT SEL Knob – Sets the selected altitude in the Selected Altitude Box. Pressing this knob synchronizes the selected altitude to the current altitude. In addition to providing the standard altitude alerter function, selected altitude provides an altitude setting for the Altitude Capture/Hold mode of the AFCS. The Selected Altitude Range Arc (when enabled), which appears on navigation maps during climbs or descents, is also based on the selected altitude setting. 20 CRS Knob – Sets the selected course on the HSI when the VOR1, VOR2, or OBS/SUSP mode is selected. Pressing this knob centers the CDI on the currently selected VOR. The selected course provides course reference to the flight director when operating in Navigation and Approach modes. 21 HDG Knob – Sets the selected heading on the HSI. Pressing this knob synchronizes the heading bug to the current heading. When operating in Heading Select mode, this knob provides the heading reference to the flight director. ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW System Overview APPENDICES AFCS Controls 2 3 4 12 11 10 5 6 7 9 8 INDEX 1 Figure 1-4 GMC 705 AFCS Control Unit 10 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW NOTE: If a key is selected, its respective annunciator is illuminated. HDG Key – Selects/deselects Heading Select Mode. 2 NAV Key – Selects/deselects Navigation Mode. 3 AP Key – Engages/disengages the autopilot. 4 LVL Key – Engages the autopilot (if the autopilot is disengaged and the aircraft is within the autopilot engagement limitations) in level vertical and lateral modes. EIS 1 FLIGHT INSTRUMENTS The GFC 700 AFCS is mainly controlled through the GMC 705 AFCS Control Unit. The AFCS Control Unit consists of the following controls: IAS Key – Selects/deselects Indicated Airspeed Mode. 7 ALT Key – Selects/deselects Altitude Hold Mode. 8 VNV Key – Selects/deselects Vertical Navigation mode. 9 VS Key – Selects/deselects Vertical Speed Mode. 10 YD Key (optional) – Engages/disengages the yaw damper. 11 FD Key – Activates/deactivates the flight director in the default pitch and roll modes. If the autopilot is engaged, the FD Key is disabled. 12 APR Key – Selects/deselects Approach Mode. AFCS 6 HAZARD AVOIDANCE NOSE UP/DN Wheel – Controls the active mode reference for the Pitch, Vertical Speed, and Indicated Airspeed modes. FLIGHT MANAGEMENT 5 AUDIO PANEL & CNS NOTE: The LVL Key will not engage the autopilot when Automatic Descent Mode (ADM) is active. Additional AFCS Controls ADDITIONAL FEATURES The AP DISC (Autopilot Disconnect) Switch, GA (Go Around) Button, and MET (Manual Electric Trim) Switch are additional AFCS controls and are located in the cockpit, separately from the AFCS Control Unit. These are discussed in detail in the AFCS section. APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 11 SYSTEM OVERVIEW System Overview Audio Panel Controls 2 3 4 5 6 16 17 18 19 7 8 10 9 EIS FLIGHT INSTRUMENTS 1 11 AUDIO PANEL & CNS 12 13 14 15 20 21 22 23 24 25 Figure 1-5 GMA 347 Audio Panel Controls 1 Marker Beacon Annunciators – Each annunciator lights independently when flying over the associated marker beacon station. 2 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 and allows music mute option. 3 COM1 – When selected, audio from the #1 COM receiver can be heard. 4 COM2 – When selected, audio from the #2 COM receiver can be heard. 5 COM3 – Reserved for optional COM radio. 6 NAV1 – When selected, audio from the #1 NAV receiver can be heard. 7 NAV2 – When selected, audio from the #2 NAV receiver can be heard. 8 DME – Turns optional DME audio on or off. 9 ADF – Turns optional ADF receiver audio on or off. 10 PLAY – Press once to play the last recorded COM audio. Press again while audio is playing and the previous block of recorded audio will be played. Each subsequent press plays each previously recorded block. Pressing the MKR/MUTE Key during play of a memory block stops play. 11 PILOT Squelch – Turn to adjust Pilot’s squelch. The Pilots volume knob must be pressed to allow manual squelch adjustment. INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT NOTE: When a key is selected, an annunciator in the key is illuminated. 12 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview 16 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. 17 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. 18 COM3 MIC – Reserved for optional COM radio. 19 COM 1/2 – Split COM operation key. When selected, the pilot uses the COM 1 transceiver and the copilot uses COM 2. 20 SPKR – Selects and deselects the cabin speaker. COM and NAV receiver audio can be heard on the speaker. Press and hold for 2 seconds for Passenger Address (PA). The SPKR key flashes during PA. 21 TEL – Not used. 22 COPLT – Selects and deselects the copilot intercom isolation. 23 PILOT – Selects and deselects the pilot intercom isolation. 24 COPILOT/PASS Volume – Turn to adjust Copilot/Passenger intercom volume or squelch. Pulling the right volume knob controls passenger volume, pushing in controls Copilot volume. 25 COPILOT/PASS Squelch – Copilot and passenger share the squelch knob. ADDITIONAL FEATURES HI SENS Annunciator – Indicates marker beacon receiver sensitivity, high sensitivity when illuminated, low sensitivity when extinguished. AFCS 15 HAZARD AVOIDANCE SENS – Press to increase marker beacon receiver sensitivity as indicated by illumination of the HI SENS annunciator. Press again to return to low sensitivity and extinguish the HI SENS annunciator. FLIGHT MANAGEMENT 14 AUDIO PANEL & CNS MAN SQ – Manual Squelch annunciator. When lit, pilot and copilot squelch knobs control manual squelch. EIS 13 FLIGHT INSTRUMENTS PILOT Volume – Turn the left (Pilot) volume knob to control pilot’s intercom volume and the ON and OFF function. (Full CCW detent is OFF) Press to switch between manual and automatic squelch control as indicated by illumination of the MAN SQ annunciator. SYSTEM OVERVIEW 12 APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 13 SYSTEM OVERVIEW System Overview Softkey Function FLIGHT INSTRUMENTS 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). Softkeys revert to the previous level after 45 seconds of inactivity. Softkey On EIS Bezel-Mounted Softkeys (Press) Softkey Names (Displayed) AUDIO PANEL & CNS Figure 1-6 Softkeys (Second-Level PFD Configuration) In the following descriptions, top level softkeys are denoted with bullets. FLIGHT MANAGEMENT PFD Softkeys 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. HAZARD AVOIDANCE The PFD softkeys provide control over flight management functions, including GPS, NAV, terrain, traffic, and weather data (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). (optional) INSET SENSOR PFD OBS CDI DME XPDR IDENT TMR/REF NRST ALERTS BACK ALERTS AFCS Press the CDI Softkey to cycle through navigation sources: - GPS - NAV1 (VOR/LOC) - NAV2 (VOR/LOC) ADDITIONAL FEATURES Figure 1-7 Top Level PFD Softkeys APPENDICES INSET (optional) (optional) (optional) (optional) INDEX OFF DCLTR TRAFFIC DCLTR-1 TRFC-1 DCLTR-2 TRFC-2 TOPO TERRAIN STRMSCP NEXRAD XM LTNG METAR Press the OFF or BACK Softkey to return to the top-level softkeys. DCLTR-3 14 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW 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 DCLTR-1: Removes land data DCLTR-2: Removes land and SUA data DCLTR-3: Removes everything except active flight plan Inset Map TRAFFIC (2) Displays/removes traffic information on (optional) INSET SENSOR PFD OBS CDI DME XPDR IDENT TMR/REF NRST ALERTS TRFC-1: Displays traffic on Inset Map. TRFC-2: Removes everything except traffic. Press the (e.g., CDI Softkey to cycle terrain, through rivers, lakes) on Inset Map Displays/removes topographical data coastlines, TOPO navigation sources: - GPSon Inset Map Displays/removes terrain information TERRAIN - NAV1 (VOR/LOC) Displays/removes Stormscope lightning information on Inset Map (optional) STRMSCP - NAV2 (VOR/LOC) Displays/removes NEXRAD weather and coverage information on Inset Map (optional) NEXRAD Displays/removes XM lightning information on Inset Map (optional) XM LTNG Displays/removes METAR weather information on Inset Map (optional) METAR • INSET OFF DCLTR (3) FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT INSET HAZARD AVOIDANCE (optional) (optional) (optional) (optional) OFF TRAFFIC DCLTR-1 TRFC-1 DCLTR-2 TRFC-2 TOPO TERRAIN STRMSCP NEXRAD XM LTNG METAR BACK ALERTS Press the OFF or BACK Softkey to return to the top-level softkeys. AFCS DCLTR DCLTR-3 ADDITIONAL FEATURES Figure 1-8 INSET Softkeys APPENDICES SENSOR ADC2 AHRS1 AHRS2 BACK INDEX ADC1 ALERTS Press the BACK Softkey to return to the top-level softkeys. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 15 OFF TRAFFIC DCLTR TRFC-1 DCLTR-2 TRFC-2 SYSTEM OVERVIEW System OverviewDCLTR-1 TERRAIN STRMSCP NEXRAD XM LTNG METAR BACK ALERTS Press the OFF or BACK Softkey to return to the top-level softkeys. Displays second-level softkeys for ADC and AHRS sensors Selects ADC1 Selects ADC2 (optional) • SENSOR ADC1 ADC2 FLIGHT INSTRUMENTS TOPO DCLTR-3 Selects AHRS1 Selects AHRS2 (optional) AHRS1 AHRS2 EIS SENSOR AUDIO PANEL & CNS ADC1 ADC2 AHRS1 AHRS2 BACK ALERTS Press the BACK Softkey to return to the top-level softkeys. FLIGHT MANAGEMENT Figure 1-9 SENSOR Softkeys HAZARD AVOIDANCE • PFD SYN VIS PATHWAY AFCS SYN TERR HRZN HDG APTSIGNS APPENDICES ADDITIONAL FEATURES DFLTS WIND OPTN1 OPTN2 OFF DME BRG INDEX HSI FMT 360 HSI ARC HSI 16 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 Enables synthetic terrain depiction Displays compass heading along the Zero-Pitch line Displays position markers for airports within approximately 15 nm of the current aircraft position. Airport identifiers are displayed when the airport is within approximately 9nm. Resets PFD to default settings, including changing units to standard Displays softkeys to select and configure wind data Displays wind direction arrow with true numeric direction and speed Displays headwind/tailwind and crosswind arrows with numeric speed components Removes wind information from display Displays/removes DME Information Window (optional) Displays the Bearing Information Window and cycles through: NAV1: Waypoint frequency/identifier and DME information NAV2: Waypoint frequency/identifier and DME information GPS: Waypoint identifier and GPS distance information Off: Removes window Displays softkeys to select the HSI format Displays HSI as a 360° compass rose Displays HSI as a 140° viewable arc (Bearing Information window unavailable) Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview EIS • DME Displays softkeys for changing the Altimeter barometric setting and altitude displays to metric units Displays the current and Selected altitudes in meters in addition to feet, when selected Displays the Altimeter barometric setting in inches of mercury (in Hg) Displays the Altimeter barometric setting in hectopascals (hPa) Sets barometric pressure to 29.92 in Hg (1013 hPa if metric display is selected) Selects OBS Mode on the CDI when navigating by GPS (only available with active leg) Cycles CDI through GPS, NAV1 (VOR/LOC), and NAV2 (VOR/LOC) navigation sources Displays/removes the DME Radio Tuning Window (optional) FLIGHT INSTRUMENTS METERS IN HPA STD BARO • OBS • CDI SYSTEM OVERVIEW ALT UNIT (optional) (optional) DFLTS WIND DME BRG ALT UNIT STD BARO HSI FMT Press the BRGsoftkeys to display/remove the Bearing Information window and cycle through bearing sources: - NAV1/NAV2 - GPS - ADF (optional) Press the STD BARO or BACK Softkey to return to the top-level softkeys. OFF OPTN2 METERS IN HPA ALERTS BACK ALERTS BACK ALERTS BACK ALERTS ADDITIONAL FEATURES ARC HSI BACK AFCS PATHWAY SYN TERR HRZN HDG APTSIGNS 360 HSI ALERTS HAZARD AVOIDANCE OPTN1 BACK FLIGHT MANAGEMENT SYN VIS AUDIO PANEL & CNS PFD APPENDICES Figure 1-10 PFD Softkeys INDEX XPDR 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T STBY ON ALT GND VFR CODE IDENT BACK ALERTS 17 PFD System Overview SYSTEM OVERVIEW (optional) DFLTS FLIGHT INSTRUMENTS • XPDR STBY ON ALT GND AUDIO PANEL & CNS EIS VFR CODE 0—7 BKSP • IDENT FLIGHT MANAGEMENT • TMR/REF • NRST • ALERTS WIND DME BRG ALT UNIT STD BARO HSI FMT BACK ALERTS BACK ALERTS Displays transponder mode selection softkeys: Selects standby mode (Transponder does not reply to any interrogations) Press the BRGsoftkeys Press the STD BARO or BACK to display/remove Selects Mode A (Transponder replies to interrogations) Softkey to return to the top-level the Bearing Information softkeys. Selects Mode C – altitude reporting mode window and(Transponder cycle through replies to identification and altitude bearing sources: interrogations) - NAV1/NAV2 Manually selects Ground Mode (Transponder does not allow Mode A and Mode C - GPS ADF (optional) replies, but does permit acquisition squitter and replies to discretely addressed Mode S interrogations) BACK ALERTS OFF OPTN1 OPTN2 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 IN HPA BACK ALERTS Activates the Special Position Identification (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 STBY ON ALT GND VFR CODE IDENT AFCS Press the BACK Softkey to return to the top-level softkeys. 1 2 3 4 5 6 7 ADDITIONAL FEATURES 0 IDENT BKSP BACK ALERTS Press the IDENT or BACK Softkey to return to the toplevel softkeys. INDEX APPENDICES Figure 1-11 XPDR Softkeys 18 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW MFD Softkeys MFD softkeys vary depending on the page selected. EIS and Navigation Map Page (default MFD page) DCLTR SHW CHRT CHKLIST ENGINE softkeys are described MAP here. FLIGHT INSTRUMENTS NOTE: The ice protection system (optional) must be operated in accordance with the approved flight manual DCLTR-1 limitations. This option is only available on SR22 models. DCLTR-2 DCLTR-3 EIS Displays full Engine Page and second-level engine softkeys; press again to return to the Engine Strip and top-level softkeys (see the EIS Section for more information) Displays Anti-Ice softkeys (TKS FIKI is optional. See Operational Note above) ANTI-ICE ENGINE Selects manual mode and opens the left tank valve and closes the right tank valve LEFT Selects auto tank mode AUTO (Optional) Selects manual mode and opens the right tank valve and closes the left tank valve RIGHT FUEL CO RST ASSIST ENGINE DCLTR Removes bars and temperature readouts from the Engine Temperature Box DCLTR Identifies temperature peaks ASSIST Press the ENGINE Softkey to return to the top-level softkeys. Resets the CO Guardian CO RST UNDO ENTER TABS FULL Accesses the Initial Usable Fuel Page FUEL Resets fuel totalizer to full (usable fuel) FULL Press the UNDO or ENTER Softkey to return to the second-level softkeys. Resets fuel totalizer to tabs (usable fuel) TABS Resets to the initial usable fuel amount shown on the Initial Usable Fuel Page UNDO Saves the usable fuel amount as displayed on the Initial Usable Fuel Page ENTER • ENGINE AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE ENGINE The ANTI-ICE Softkey and its secondlevel softkeys are only available with the TKS FIKI system installed. ANTI-ICE ASSIST DCLTR AFCS (Optional) ENGINE FUEL CO RST Press the ENGINE Softkey to return to the top-level softkeys. ADDITIONAL FEATURES (Optional) (Optional) (Optional) LEFT AUTO RIGHT FULL TABS BACK UNDO ENTER APPENDICES Press the UNDO or ENTER Softkey to return to the second-level softkeys. Figure 1-12 MFD Softkeys (EIS) INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 19 SYSTEM OVERVIEW System Overview Enables second-level Navigation Map Page softkeys Displays/removes traffic information on Navigation Map Page Displays/removes profile view 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 lightning information on the Navigation 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) Displays/removes METAR weather information on Navigation Map Page (optional) METAR Displays/removes XM weather product legend on Navigation Map Page. Softkey available LEGEND when one or more XM weather products are enabled for display (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 (optional) • 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 PROFILE TOPO 20 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW (optional) ENGINE MAP DCLTR SHW CHRT CHKLIST DCLTR-1 FLIGHT INSTRUMENTS DCLTR-2 DCLTR-3 TRAFFIC PROFILE TOPO (optional) (optional) (optional) (optional) TERRAIN AIRWAYS STRMSCP NEXRAD XM LTNG METAR LEGEND BACK EIS Press the BACK softkey to return to the top-level softkeys. AIRWY ON AIRWY LO AIRWY HI DONE EXIT AUDIO PANEL & CNS ENGINE EMERGCY The DONE Softkey label changes to UNDO when the checklist item is already checked. Figure 1-13 MFD Softkeys (Navigation Map and Checklist) FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 21 SYSTEM OVERVIEW System Overview 1.3 Secure Digital Cards FLIGHT INSTRUMENTS NOTE: Refer to the Appendices for instructions on updating the aviation databases. NOTE: Ensure that the system is powered off before inserting the SD card. EIS The PFD and MFD data card slots use Secure Digital (SD) cards and are located on the top right portion of the display bezels. Each display bezel is equipped with two SD card slots. SD cards are used for aviation database and system software updates as well as terrain database storage. Install an SD card: AUDIO PANEL & CNS Insert the SD card in the SD card slot, pushing the card in until the spring latch engages. The front of the card should remain flush with the face of the display bezel. Remove an SD card: FLIGHT MANAGEMENT Gently press on the SD card to release the spring latch and eject the card. MFD AFCS HAZARD AVOIDANCE PFD APPENDICES ADDITIONAL FEATURES SD Card Slots INDEX Figure 1-14 Display Bezel SD Card Slots 22 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW 1.4 System Power-up NOTE: Refer to the Appendices for AHRS initialization bank angle limitations. FLIGHT INSTRUMENTS NOTE: See the Appendices for additional information regarding system-specific annunciations and alerts. NOTE: See the Pilot’s Operating Handbook (POH) for specific procedures concerning avionics power application and emergency power supply operation. EIS The Perspective™ 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 1-15. All system annunciations should disappear typically within one minute of power-up. Upon power-up, key annunciator lights also become momentarily illuminated on the audio panels, the control units and the display bezels. 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 one minute of power-up. The AHRS can align itself both while taxiing and during level flight. HAZARD AVOIDANCE When the MFD powers up (Figure 1-16), the MFD Power-up Page displays the following information: • System version • Obstacle database name and version • Copyright • Navigation database name, version, and effective dates • Land database name and version • Airport Directory name, version and effective dates • Safe Taxi database information • FliteCharts/ChartView database information • Terrain database name and version AFCS Current database information includes the valid operating dates, cycle number and database type. When this information has been reviewed for currency (to ensure that no databases have expired), the pilot is prompted to continue. Pressing the ENT Key acknowledges this information and the Navigation Map Page is displayed upon pressing the key a second time. 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. ADDITIONAL FEATURES APPENDICES INDEX Figure 1-15 PFD Initialization 190-00820-06 Rev. A Figure 1-16 MFD Power-up Page Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 23 SYSTEM OVERVIEW System Overview 1.5 System Operation FLIGHT INSTRUMENTS The displays are connected together via a single Ethernet bus, thus allowing for high-speed communication. As shown in Figure 1-1, each IAU is connected to the PFD. This section discusses the normal and reversionary modes of operation as well as the various AHRS modes of the system. Display Operation NOTE: In normal operating mode, backlighting can only be adjusted from the PFD, or from any display EIS operating in reversionary mode. APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS 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). The PFD offers control for COM frequency selection and the MFD offers control for NAV frequency selection. The PFD/MFD Control Unit offers control for both COM and NAV frequency selection. INDEX Figure 1-17 Normal Operation 24 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW FLIGHT INSTRUMENTS In the event of a display failure, the system automatically switches to reversionary (backup) mode. In Reversionary Mode, all essential flight information from the PFD is combined with the EIS and presented on the display operating in Reversionary Mode. 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. EIS 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. If the system fails to detect a display problem, Reversionary Mode may be manually activated by pressing the red DISPLAY BACKUP Button. Pressing this button again deactivates Reversionary Mode. AUDIO PANEL & CNS DISPLAY BACKUP Button Manually Activates/Deactivates Reversionary Mode on Both Displays NAV1 and COM1 (provided by the failed PFD) Flagged Invalid FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Figure 1-18 Reversionary Mode (Failed PFD) APPENDICES NOTE: The system alerts the pilot when backup paths are utilized by the LRUs. Refer to the Appendices for further information regarding system-specific alerts. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 25 SYSTEM OVERVIEW System Overview System Annunciations FLIGHT INSTRUMENTS When an LRU or an LRU function fails, a large red ‘X’ is typically displayed over the instrument experiencing failed data (Figure 1-19 displays all possible flags and responsible LRUs). The system alerts the pilot when backup paths are utilized by the LRUs. Upon 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 system should be serviced by a Garmin-authorized repair facility. NOTE: For a detailed description of all annunciations and alerts, refer to Appendix A. Refer to the Pilot’s EIS Operating Handbook (POH) for additional information regarding pilot responses to these annunciations. AUDIO PANEL & CNS GIA 63W Integrated Avionics Units FLIGHT MANAGEMENT GDC 74A Air Data Computer Navigation Database Mismatch in PFD and MFD GRS 77 AHRS OR GMU 44 Magnetometer HAZARD AVOIDANCE GEA 71 Engine Airframe Unit OR GIA 63W Integrated Avionics Unit GIA 63W Integrated Avionics Units AFCS GDC 74A Air Data Computer GTX 32/33/33 ES Transponder OR GIA 63W Integrated Avionics Units INDEX APPENDICES ADDITIONAL FEATURES Figure 1-19 System Failure Annunciations 26 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW System Status FLIGHT INSTRUMENTS The System Status Page displays the status and software version numbers for all detected system LRUs. Pertinent information on all system databases is also displayed. Active LRUs are indicated by green check marks and failed LRUs are indicated by red “X”s. Failed LRUs should be noted and a Cirrus service center or Garmin dealer informed. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS Figure 1-20 Example AUX - System Status Page The LRU and ARFRM softkeys on the System Status Page select the applicable list (LRU INFO or AIRFRAME window) through which the FMS Knob can be used to scroll information within the selected window. ADDITIONAL FEATURES Pressing the MFD1 DB Softkey (label background changes to grey indicting the softkey is selected) places the cursor in the DATABASE window. Use the FMS Knob to scroll through database information for the MFD. Pressing the softkey again will change the softkey label to PFD1 DB. PFD 1 database information is now displayed in the DATABASE window. APPENDICES The ANN TEST Softkey, when pressed, causes an annunciation test tone to be played. Pressing the SYNC DBS Softkey (label background changes to grey indicting the softkey is selected) activates the Automatic Database Synchronization feature. When this feature is active, databases are updated automatically in the MFD and PFD from one SD card. For a detailed discussion on database synchronization, see the SD Card Use section in the Appendices. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 27 SYSTEM OVERVIEW AHRS Operation FLIGHT INSTRUMENTS System Overview The Attitude and Heading Reference System (AHRS) performs attitude, heading, and vertical acceleration calculations for the 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. Note: Aggressive maneuvering in reversionary mode can degrade AHRS accuracy. unavailable available available unavailable FLIGHT MANAGEMENT le ab Attitude/Heading Invalid HAZARD AVOIDANCE AHRS no-GPS Mode ail av AHRS no- AHRS no-Mag/ Mag Mode no-Air Mode Heading Invalid Air Data un available Air Data AHRS Normal Operation Magnetometer Data available unavailable available AUDIO PANEL & CNS Magnetometer Data unavailable EIS GPS Data AFCS Figure 1-21 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’. 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. 28 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW GPS Receiver Operation Each GIA 63W Integrated Avionics Unit (IAU) contains a GPS receiver. 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. FLIGHT INSTRUMENTS Internal system checking is performed to ensure both GPS receivers are providing accurate data to the PFD. In some circumstances, both GPS receivers may be providing accurate data, but one receiver may be providing a better GPS solution than the other receiver. In this case the GPS receiver producing the better solution is automatically coupled to the PFD. “BOTH ON GPS 1” or “BOTH ON GPS 2” are then displayed in the Reversionary Sensor Window (see Appendix A) indicating which GPS receiver is being used. Both GPS receivers are still functioning properly, but one receiver is performing better than the other at that particular time. EIS AUDIO PANEL & CNS These GPS sensor annunciations are most often seen after system power-up when one GPS receiver has acquired satellites before the other, or one of the GPS receivers has not yet acquired an SBAS (Satellite Based Augmentation System) signal. While the aircraft is on the ground, the SBAS signal may be blocked by obstructions causing one GPS receiver to have difficulty acquiring a good signal. Also, while airborne, turning the aircraft may result in one of the GPS receivers temporarily losing the SBAS signal. FLIGHT MANAGEMENT If the sensor annunciation persists, check for a system failure message in the Messages Window on the PFD. If no failure message exists, check the GPS Status Page and compare the information for GPS1 and GPS2. Discrepancies may indicate a problem. Viewing GPS receiver status information: 1) Turn the large FMS Knob on the MFD to select the Auxiliary Page Group (see Section 1.6 for information on navigating MFD page groups). HAZARD AVOIDANCE 2) Turn the small FMS Knob to select AUX - GPS Status Page. 3) To change the selected GPS receiver: Press the desired GPS Softkey. Or: AFCS a) Press the MENU Key. b) Use the FMS Knob to highlight the receiver which is not selected and press the ENT Key. ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 29 SYSTEM OVERVIEW System Overview Satellite Signal Information GPS Receiver Status FLIGHT INSTRUMENTS Satellite Constellation Diagram AUDIO PANEL & CNS EIS RAIM Availability Prediction HAZARD AVOIDANCE FLIGHT MANAGEMENT Satellite Signal Strength Bars AFCS Figure 1-22 GPS Status Page The GPS Status Page provides the following information: ADDITIONAL FEATURES • Satellite constellation diagram Satellites currently in view are shown at their respective positions on a sky view diagram. The sky view is always in a north-up orientation, with the outer circle representing the horizon, the inner circle representing 45° above the horizon, and the center point showing the position directly overhead. APPENDICES Each satellite is represented by an oval containing the Pseudo-random noise (PRN) number (i.e., satellite identification number). Satellites whose signals are currently being used are represented by solid ovals. • Satellite signal information status INDEX The accuracy of the aircraft’s GPS fix is calculated using Estimated Position Uncertainty (EPU), Dilution of Precision (DOP), and horizontal and vertical figures of merit (HFOM and VFOM). EPU is the radius of a circle centered on an estimated horizontal position in which actual position has 95% probability of laying. EPU is a statistical error indication and not an actual error measurement. 30 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW DOP measures satellite geometry quality (i.e., number of satellites received and where they are relative to each other) on a range from 0.0 to 9.9, with lower numbers denoting better accuracy. HFOM and VFOM, measures of horizontal and vertical position uncertainty, are the current 95% confidence horizontal and vertical accuracy values reported by the GPS receiver. FLIGHT INSTRUMENTS The current calculated GPS position, time, altitude, ground speed, and track for the aircraft are displayed below the satellite signal accuracy measurements. • GPS receiver status EIS 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. AUDIO PANEL & CNS FLIGHT MANAGEMENT When the receiver is in the process of acquiring a 3D differential GPS solution, 3D NAV is indicated as the solution until the 3D differential fix has finished acquisition. SBAS (Satellite-Based Augmentation System) indicates INACTIVE. When acquisition is complete, the solution status indicates 3D DIFF NAV and SBAS indicates ACTIVE. • RAIM (Receiver Autonomous Integrity Monitoring) Prediction (RAIM Softkey is pressed) In most cases performing a RAIM prediction is not necessary. However, in some cases, the selected approach may be outside the SBAS coverage area and it may be necessary to perform a RAIM prediction for the intended approach. HAZARD AVOIDANCE 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. AFCS 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. ADDITIONAL FEATURES Because of the tighter protection limit on approaches, there may be times when RAIM is not available. The system automatically monitors RAIM and warns with an alert message when it is not available. If RAIM is not predicted to be available for the final approach course, the approach does not become active, as indicated by the messages “Approach is not active” and “RAIM not available from FAF to MAP”. If RAIM is not available when crossing the FAF, the missed approach procedure must be flown. APPENDICES Predicting RAIM availability 1) Select the GPS Status Page. 2) If necessary, press the RAIM Softkey. 3) Press the FMS Knob. The ‘WAYPOINT’ field is highlighted. INDEX 4) Turn the small FMS Knob to display the Waypoint Information Window. 5) Enter the desired waypoint: 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 31 SYSTEM OVERVIEW System Overview a) Use the FMS Knob to enter the desired waypoint by identifier, facility, or city name and press the ENT Key. Refer to Section 1.6 for instructions on entering alphanumeric data into the system. Or: FLIGHT INSTRUMENTS a) Use the large FMS Knob to scroll to the Most Recent Waypoints List. b) Use the small FMS Knob to highlight the desired waypoint in the list and press the ENT Key. The system automatically fills in the identifier, facility, and city fields with the information for the selected waypoint. c) Press the ENT Key to accept the waypoint entry. 6) Use the FMS Knob to enter an arrival time and press the ENT Key. EIS 7) Use the FMS Knob to enter an arrival date and press the ENT Key. FLIGHT MANAGEMENT AUDIO PANEL & CNS 8) With the cursor highlighting ‘COMPUTE RAIM?’, press the ENT Key. Once RAIM availability is computed, one of the following is displayed: • ‘COMPUTE RAIM?’—RAIM has not been computed for the current waypoint, time, and date combination • ‘COMPUTING AVAILABILITY’—RAIM calculation in progress • ‘RAIM AVAILABLE’—RAIM is predicted to be available for the specified waypoint, time, and date • ‘RAIM NOT AVAILABLE’—RAIM is predicted to be unavailable for the specified waypoint, time, and date Predicting RAIM availability at present position 1) Select the GPS Status Page. HAZARD AVOIDANCE 2) If necessary, press the RAIM Softkey. 3) Press the FMS Knob. The ‘WAYPOINT’ field is highlighted. 4) Press the MENU Key. 5) With ‘Set WPT to Present Position’ highlighted, press the ENT Key. AFCS 6) Press the ENT Key to accept the waypoint entry. 7) Use the FMS Knob to enter an arrival time and press the ENT Key. 8) Use the FMS Knob to enter an arrival date and press the ENT Key. APPENDICES ADDITIONAL FEATURES 9) With the cursor highlighting ‘COMPUTE RAIM?’, press the ENT Key. Once RAIM availability is computed, one of the following is displayed: • ‘COMPUTE RAIM?’—RAIM has not been computed for the current waypoint, time, and date combination • ‘COMPUTING AVAILABILITY’—RAIM calculation in progress • ‘RAIM AVAILABLE’—RAIM is predicted to be available for the specified waypoint, time, and date • ‘RAIM NOT AVAILABLE’—RAIM is predicted to be unavailable for the specified waypoint, time, and date INDEX • SBAS Selection (SBAS Softkey is pressed) (WAAS, EGNOS, or MSAS capable systems only) In certain situations, such as when the aircraft is outside or on the fringe of the WAAS, EGNOS, or MSAS coverage area, it may be desirable to disable the reception of the applicable SBAS signal (although it is not recommended). When disabled, the SBAS field in the GPS Status box indicates DISABLED. There may be a small delay for the GPS Status box to be updated upon WAAS, EGNOS, and MSAS enabling/disabling. 32 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW Disabling WAAS, EGNOS or MSAS 1) Select the GPS Status Page. 2) If necessary, press the SBAS Softkey. FLIGHT INSTRUMENTS 3) Press the FMS Knob, and turn the large FMS Knob to highlight the desired SBAS system. 4) Press the ENT Key to uncheck the box. 5) Press the FMS Knob to remove the cursor. EIS AUDIO PANEL & CNS Figure 1-23 Enable/Disable SBAS FLIGHT MANAGEMENT HAZARD AVOIDANCE • GPS Satellite Signal Strengths The GPS Status Page can be helpful in troubleshooting weak (or missing) signal levels due to poor satellite coverage or installation problems. As the GPS receiver locks onto satellites, a signal strength bar is displayed for each satellite in view, with the appropriate satellite PRN number (01-32 or 120-138 for WAAS) below each bar. The progress of satellite acquisition is shown in three stages, as indicated by signal bar appearance: AFCS - No bar—Receiver is looking for the indicated satellite - Hollow bar—Receiver has found the satellite and is collecting data - Light blue bar—Receiver has collected the necessary data and the satellite signal can be used - Green bar—Satellite is being used for the GPS solution - Checkered bar—Receiver has excluded the satellite (Fault Detection and Exclusion) - “D” indication—Denotes the satellite is being used as part of the differential computations ADDITIONAL FEATURES Each satellite has a 30-second data transmission that must be collected (signal strength bar is hollow) before the satellite may be used for navigation (signal strength bar becomes solid). APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 33 SYSTEM OVERVIEW System Overview 1.6 Accessing System Functionality FLIGHT INSTRUMENTS Menus The system 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 settings changes which specifically relate to the currently displayed window/page. There is no all-encompassing menu. Some menus provide access to additional submenus that are used to view, edit, select, and review options. Menus display ‘No Options’ when there are no 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. FLIGHT MANAGEMENT Options for FPL Window ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE No Options for NRST Window INDEX APPENDICES Figure 1-24 Page Menu Examples 34 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW Page Groups Note: Refer to other supporting sections in this Pilot’s Guide for details on specific pages. 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 page group tabs are displayed along the bottom. The titles of pages available in the group are displayed in a list above the page groups. The current page group and current page within the group are shown in cyan. For some of these pages (Airport/Procedures/Weather Information, XM, Procedure Loading), the active title of the page changes while the page name in the list remains the same. Active Page Title AUDIO PANEL & CNS FLIGHT MANAGEMENT Pages in Current Group HAZARD AVOIDANCE Page Groups Figure 1-25 Page Title and Page Groups AFCS The main page groups are navigated using the FMS Knob; specific pages within each group can vary depending on the configuration of optional equipment. Selecting a page using the FMS Knob: ADDITIONAL FEATURES 1) Turn the large FMS Knob to display the list of page groups; continue turning the large FMS Knob until the desired page group is selected 2) Turn the small FMS Knob to display the desired page within a specific page group. 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 35 SYSTEM OVERVIEW System Overview Map Pages (MAP) Navigation Map FLIGHT INSTRUMENTS Traffic Map Stormscope (optional) XM Weather Data Link (service optional) AUDIO PANEL & CNS EIS Terrain Proximity/ TERRAIN-SVS (optional)/ TAWS-B (optional) FLIGHT MANAGEMENT Figure 1-26 Map Pages Waypoint Pages (WPT) HAZARD AVOIDANCE Airport/Procedures/Weather Information Pages - Airport Information (INFO-1 Softkey) - Airport Directory (INFO-2 Softkey) AFCS - Departure Information (DP Softkey) ADDITIONAL FEATURES - Approach Information (APR Softkey) APPENDICES - Arrival Information (STAR Softkey) Intersection Information - Weather Information (optional) (WX Softkey) Airport/Procedures/ Weather Information Pages NDB Information VOR Information Figure 1-27 Waypoint Pages INDEX User Waypoint Information 36 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW Auxiliary Pages (AUX) Trip Planning FLIGHT INSTRUMENTS Utility GPS Status System Setup Pages XM Satellite pages (optional) EIS - XM Radio (RADIO Softkey) - XM Information (INFO Softkey) AUDIO PANEL & CNS XM Satellite Pages System Status Video FLIGHT MANAGEMENT Figure 1-28 Auxiliary Pages HAZARD AVOIDANCE Nearest Pages (NRST) Nearest Airports Nearest Intersections AFCS Nearest NDB Nearest VOR Nearest User Waypoints ADDITIONAL FEATURES Nearest Frequencies Nearest Airspaces APPENDICES Figure 1-29 Nearest Pages INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 37 SYSTEM OVERVIEW System Overview FLIGHT INSTRUMENTS In addition to the main page groups accessed exclusively using the FMS Knobs, the Flight Plan Pages can also be accessed using the FPL Key on the PFD/MFD Control Unit. Main pages within this group are then selected by pressing the FMS Key and turning the FMS Knobs. In some instances, softkeys may be used to access the Procedure Pages. Flight Plan Pages (FPL) Active Flight Plan - Wide View, Narrow View (VIEW Softkey) EIS Flight Plan Catalog or FLIGHT MANAGEMENT AUDIO PANEL & CNS Stored Flight Plan (NEW Softkey) Narrow and Wide View HAZARD AVOIDANCE Figure 1-30 Flight Plan Pages AFCS The Procedure pages may be accessed at any time on the PFD/MFD Control Unit 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. Turning the FMS Knob does not scroll through the Procedure pages. Procedure Pages (PROC) ADDITIONAL FEATURES Departure Loading Arrival Loading APPENDICES Approach Loading INDEX Figure 1-31 Procedure Pages 38 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW System Settings 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) FLIGHT INSTRUMENTS • 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) • Page Navigation EIS • Electronic Stability & Protection enable/disable (see AFCS Section) • Audio Alerts AUDIO PANEL & CNS • MFD Navigation Status Box fields (see Flight Management Section) Restoring system setup defaults: 1) Use the FMS Knob to select the AUX - System Setup Page. FLIGHT MANAGEMENT 2) Press the DFLTS Softkey. Or: a) Press the MENU Key. HAZARD AVOIDANCE b) Highlight ‘Restore Defaults’ and press the ENT Key. AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 1-32 AUX - System Setup Page 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 39 SYSTEM OVERVIEW System Overview Date/Time FLIGHT INSTRUMENTS The system obtains the current Coordinated Universal Time (UTC) date and time directly from the GPS satellite signals (shown on the AUX - GPS Status Page, Figure 1-22). 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 1-33 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. INDEX 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. Figure 1-34 Date/Time Settings (AUX - System Setup Page) 40 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW Display Units Units in which various quantities are displayed on the system 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 1-35 Display Unit Settings (AUX - System Setup Page) Altitude and Vertical Speed Feet Meters All altitudes on MFD All elevations on MFD Temperature Celsius Fahrenheit Gallons Liters Pounds Kilograms HDDD°MM.MM’ HDDD°MM’SS.S” All temperatures on PFD Total Air Temperature (Trip Planning Page) Fuel parameters (Trip Planning Page) Altimeter Vertical Speed Indicator VNV altitudes (Active Flight Plan) Engine Indication System (EIS) ADDITIONAL FEATURES APPENDICES Engine Indication System (EIS) N/A N/A All positions N/A INDEX Position Airspeed Indicator True Airspeed (PFD) Wind speed vector Map range (Traffic Page, Terrain Proximity/TAWS-B Page) CDI scaling (System Setup) Fuel range calculation (EIS) AFCS Fuel and Fuel Flow Weight HAZARD AVOIDANCE 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) All speeds on MFD Table 1-1 Display Units Settings (AUX - System Setup Page) 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 41 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 1-16). The system can store up to 25 profiles; the currently active profile, the number of profiles used, and the number of profiles 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 1-36 Pilot Profiles (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. 3) Turn the large FMS Knob to highlight ‘CREATE’ in the Pilot Profile Box. ADDITIONAL FEATURES 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. 7) Press the ENT Key. INDEX 8) With ‘CREATE’ highlighted, press the ENT Key to create the profile Or: Use the large FMS Knob to select ‘CREATE and ACTIVATE’ and press the ENT Key to activate the new profile. 9) To cancel the process, select ‘CANCEL’ with the large FMS Knob and press the ENT Key. 42 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 3) Turn the large FMS Knob to highlight the active profile field in the Pilot Profile Box. 4) Turn the small FMS Knob to display the pilot profile list and highlight the desired profile. 5) Press the ENT Key. The system loads and displays the system settings for the selected profile. Renaming a profile: EIS 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. AUDIO PANEL & CNS 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. 6) Press the ENT Key. FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 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. 3) Turn the large FMS Knob to highlight ‘DELETE’ in the Pilot Profile Box. AFCS 4) Press the ENT Key. 5) In the ‘Delete Profile’ window, turn the FMS Knob to select the profile to delete. 6) Press the ENT Key. ADDITIONAL FEATURES 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. APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 43 SYSTEM OVERVIEW System Overview Page Navigation FLIGHT INSTRUMENTS The large FMS Knob displays the Page Group Tabs and navigates through the tabs. The small FMS Knob navigates through the pages within a specific group. The number of clicks it takes to display the Page Group Tabs and change to the next tab can be controlled from the Page Navigation box on the AUX - System Setup Page. OFF – Displays the Page Group Tabs with one click of the large FMS Knob. ON – Displays the Page Group Tabs and navigates to the next tab with one click of the large FMS Knob. EIS The pilot can select, from the AUX - System Setup Page, the amount of time the Page Group Tabs are displayed (in the lower right corner of the MFD). The timeout can range from two to ten seconds. Selecting page navigation settings: AUDIO PANEL & CNS 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the ‘Change On 1st Click’ field in the Page Navigation Box. FLIGHT MANAGEMENT 4) Turn the small FMS Knob to select ‘OFF’ or ‘ON’. 5) Turn the large FMS Knob to highlight the ‘Timeout Seconds’ field in the Page navigation Box. 6) Turn the small FMS Knob to select the desired number of seconds APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE 7) Press the FMS Knob momentarily to remove the flashing cursor. INDEX Figure 1-37 Page Navigation Settings (AUX - System Setup Page) 44 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW Timers The system 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). 3) Use the FMS Knob to enter the desired time and press the ENT Key. FLIGHT MANAGEMENT 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. PFD AFCS ADDITIONAL FEATURES APPENDICES Figure 1-38 Generic Timer (Timer/References Window) INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 45 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. FLIGHT INSTRUMENTS Setting the generic timer (MFD AUX - Utility Page): 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?’. AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT 7) To reset the timer, press the ENT Key with ‘RESET?’ highlighted. The field changes back to ‘START?’ and the digits are reset. ADDITIONAL FEATURES Figure 1-39 Timers (AUX - Utility Page) 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: INDEX 1) Use the FMS Knob to select the AUX - Utility Page. 2) Press the MENU Key. 3) With ‘Reset Flight Timer’ highlighted, press the ENT Key. 46 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A System Overview SYSTEM OVERVIEW The system records the time at which departure occurs, depending on whether the pilot prefers the time to be recorded from system power-up or from aircraft lift off. The displayed departure time can also be reset to display the current time at the point of reset. The format in which the time is displayed is controlled from the System Setup Page. FLIGHT INSTRUMENTS 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. 3) Use the FMS Knob to highlight ‘Reset Departure Time’ and press the ENT Key. FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 47 SYSTEM OVERVIEW System Overview 1.7 Display Backlighting EIS FLIGHT INSTRUMENTS The dimming bus is the primary source for backlighting adjustments of the PFD and MFD displays, bezel, Audio Panel keys, AFCS Control Unit keys, and PFD/MFD Control Unit keys. The automatic backlighting adjustment for the AFCS Control Unit annunciators and PFD/MFD Control Unit annunciators 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 dimming 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: AUDIO PANEL & CNS 2) Turn the small FMS Knob to select ‘MANUAL’. FLIGHT MANAGEMENT 1) Press the PFD MENU Key to display the PFD Setup Menu. ‘AUTO’ is now highlighted next to ‘PFD DSPL’. 5) Turn the large FMS Knob to highlight ‘AUTO’ next to ‘MFD DSPL’ and repeat steps 2-4. 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. 6) To remove the menu, press the CLR or MENU Key. Adjusting key backlighting: HAZARD AVOIDANCE 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’. 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’. AFCS 5) Turn the small FMS Knob to select ‘MANUAL’. 6) Press the ENT Key. The intensity value is now highlighted. 7) Use the FMS Knob to enter the desired backlighting and press the ENT Key. ADDITIONAL FEATURES 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. 10) To remove the menu, press the CLR or MENU Key. INDEX APPENDICES PFD Figure 1-40 PFD Setup Menu 48 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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. Note: The Automatic Flight Control System (AFCS) provides additional readouts and bugs on selected flight instruments. Refer to the AFCS Section for details on these bugs and readouts, as they appear on the display during certain AFCS flight director modes. EIS AUDIO PANEL & CNS 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. • Vertical Speed Indicator (VSI) – Turn Rate Indicator – Reference flags • Vertical Navigation indications – Airspeed awareness ranges • Outside Air Temperature (OAT) – Bearing pointer and information window • Attitude Indicator with slip/skid indication • DME Tuning Window – DME Information Window • Wind data – Navigation source • Altimeter, showing • System time – Course Deviation Indicator (CDI) – Barometric setting • Inset Map HAZARD AVOIDANCE – True Airspeed FLIGHT MANAGEMENT The following flight instruments and supplemental flight data are displayed on the PFD: • Airspeed Indicator, showing • Vertical Deviation, Glideslope, • Horizontal Situation Indicator, and Glidepath Indicators showing – Indicated Airspeed AFCS – Selected Altitude The PFD also displays various alerts and annunciations. ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 49 SYSTEM OVERVIEW Flight Instruments FLIGHT INSTRUMENTS 22 21 20 19 18 1 17 16 2 EIS 15 AUDIO PANEL & CNS 14 3 13 4 12 5 11 FLIGHT MANAGEMENT 6 10 9 7 APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE 8 1 Percent Power Box 12 Turn Rate Indicator 2 Airspeed Indicator 13 Barometric Altimeter Setting 3 True Airspeed 14 Vertical Speed Indicator (VSI) 4 Current Heading 15 Selected Altitude Bug 5 Horizontal Situation Indicator (HSI) 16 Altimeter 6 Course Deviation Indicator (CDI) 17 Selected Altitude 7 Outside Air Temperature (OAT) 18 COM Frequency Box 8 Softkeys 19 Navigation Status Box 9 System Time 20 AFCS Status Box 10 Transponder Status Box 21 Slip/Skid Indicator 11 Selected Heading Bug 22 Attitude Indicator INDEX Figure 2-1 Primary Flight Display (Default) 50 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Instruments SYSTEM OVERVIEW 16 15 14 FLIGHT INSTRUMENTS 1 13 12 EIS 11 AUDIO PANEL & CNS 10 2 3 9 4 7 1 Traffic Annunciation 9 Flight Plan Window 2 Selected Heading 10 Annunciation Window 3 Wind Data 11 Current Vertical Speed 4 Inset Map 12 Required Vertical Speed Indicator 5 DME Information Window 13 Vertical Deviation Indicator (VDI) 6 Bearing Information Window 14 VNV Target Altitude 7 Selected Course 15 Terrain Annunciation 8 Barometric Minimums Box 16 AFCS Status Annunciation FLIGHT MANAGEMENT 6 5 8 HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Figure 2-2 Primary Flight Display (Additional Information) APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 51 SYSTEM OVERVIEW Flight Instruments 2.1 Flight Instruments FLIGHT INSTRUMENTS Airspeed Indicator Note: Refer to the Pilot’s Operating Handbook (POH) for speed 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 shown at intervals of 10 knots. The minor tick marks on the moving tape are shown at intervals of five knots. Speed indication starts at 20 knots, with 56 knots of airspeed viewable at any time. The indicated airspeed is displayed inside the black pointer. The pointer remains black until reaching the never-exceed speed (VNE), at which point it turns red. Operating Ranges FLIGHT MANAGEMENT Airspeed Trend Vector Low Speed Range Red and White Barber Pole at VNE Vspeed References Indicated Airspeed HAZARD AVOIDANCE Speed Ranges True Airspeed AFCS 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. A red low speed awareness band extends up to the low speed awareness velocity, VLSA. APPENDICES NOTE: The ice protection system (optional) must be operated in accordance with the approved flight manual INDEX limitations. This option is only available in SR22 models. 52 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Instruments SYSTEM OVERVIEW FLIGHT INSTRUMENTS 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. If the trend vector crosses VNE, the indicated airspeed number changes to yellow. The trend vector is absent if the speed remains constant or if any data needed to calculate airspeed is not available due to a system failure. EIS Vspeeds (Glide, VR, VX, and VY) flags can be turned on/off from the Timer/References Window. VR is categorized as a takeoff Vspeed. When active (on), the Vspeeds are displayed at their respective locations to the right of the airspeed scale. By default, all Vspeed flags changes are retained when power is cycled. Note: VX and VY can only be modified on the SR22. AUDIO PANEL & CNS Changing Vspeeds and turning Vspeed flags on/off: 1) Press the TMR/REF Softkey. 2) Turn the large FMS Knob to highlight the ON/OFF field. FLIGHT MANAGEMENT 3) Turn the small FMS Knob clockwise to ON or counterclockwise to OFF. 4) To remove the window, press the CLR Key or the TMR/REF Softkey. HAZARD AVOIDANCE AFCS Figure 2-4 Timer/References Window and Menus Vspeed flags can be turned on or off all at once or by category (takeoff). ADDITIONAL FEATURES Turning all Vspeed flags on/off: 1) Press the TMR/REF Softkey. 2) Press the MENU Key. APPENDICES 3) To activate all Vspeed flags, press the ENT Key with All References On highlighted. 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. INDEX 2) Press the MENU Key. 3) Turn the FMS Knob to highlight Restore Defaults and press the ENT Key. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 53 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˚. When the Synthetic Vision System (SVS) is activated, the pitch scale is reduced to 10˚ up and 7.5˚ down; refer to the Additional Features section for more information about SVS. AFCS 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. When the optional Electronic Stability and Protection (ESP) system is available, double ticks marks also appear on the roll scale; refer to the Additional Features section for more information about ESP indications. Angle of bank is shown by the position of the pointer on the roll scale. INDEX APPENDICES ADDITIONAL FEATURES The Slip/Skid Indicator is the bar beneath the roll pointer. The indicator moves with the roll pointer and moves laterally away from the pointer to indicate lateral acceleration. Slip/skid is indicated by the location of the bar relative to the pointer. One bar displacement is equal to one ball displacement on a traditional Slip/Skid Indicator. Figure 2-6 Slip/Skid Indication 54 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 When a Selected Altitude is set, a light blue Selected Altitude Intercept Arc (if enabled) is displayed on the navigation maps when the aircraft is climbing or descending. This arc appears at the estimated position the aircraft will intercept the Selected Altitude; refer to the Flight Management Section for additional information about the Selected Altitude Intercept Arc. AUDIO PANEL & CNS Setting the Selected Altitude: T urn the ALT SEL Knob to set the Selected Altitude in 100-ft increments (up to the aircraft’s service ceiling. When meters are displayed, Selected Altitude is adjusted in 50 meter increments. If set, the Minimum Descent Altitude/Decision Height (MDA/DH) value is also available for the Selected Altitude. If desired, press the ALT SEL Knob to synchronize the selected altitude to the displayed altitude to the nearest 10 ft. Selected Altitude Bug Indicated Altitude Indicated Altitude (Meters) AFCS Altitude Trend Vector Selected Altitude Selected Altitude (Meters) HAZARD AVOIDANCE Selected Altitude Bug FLIGHT MANAGEMENT ADDITIONAL FEATURES APPENDICES Barometric Setting Box (Hectopascals) Barometric Setting Figure 2-7 Altimeter Settings, In Hg and Metric INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 55 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. 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. AUDIO PANEL & CNS 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 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. FLIGHT MANAGEMENT Selecting the altimeter barometric pressure setting: Turn the BARO Knob to select the desired setting. HAZARD AVOIDANCE Selecting standard barometric pressure: Press the BARO Knob to select standard pressure; STD BARO is displayed in the Barometric Setting box. Or: 1) Press the PFD Softkey to display the second-level softkeys. AFCS 2) Press the STD BARO Softkey; STD BARO is displayed in the Barometric Setting box. ADDITIONAL FEATURES Figure 2-8 Standard Barometric Altimeter Setting Changing altimeter barometric pressure setting units: 1) Press the PFD Softkey to display the second-level softkeys. APPENDICES 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 4) Press the BACK Softkey to return to the top-level softkeys. 56 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 barometric pressure setting flashing light blue 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. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight ON or OFF 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) With the altitude field highlighted, turn the small FMS Knob to set desired 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 Baro Transition Alert (AUX - System Setup Page) APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 57 SYSTEM OVERVIEW Flight Instruments Vertical Speed Indicator (VSI) FLIGHT INSTRUMENTS The Vertical Speed Indicator (VSI) displays the aircraft vertical speed with numeric labels and tick marks at 1000 and 2000 fpm in each direction on the non-moving tape. Minor tick marks are at intervals of 500 fpm. The current vertical speed is displayed in the pointer, which also points to that speed on the non-moving tape. 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 corresponding edge of the tape and the rate appears inside the pointer. EIS A magenta chevron bug is displayed as the Required Vertical Speed Indication (RVSI; Figure 2-10) for reaching a VNV Target Altitude once the “TOD [Top of Descent] within 1 minute” alert has been generated. See the Flight Management and AFCS sections 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 Vertical Deviation FLIGHT MANAGEMENT The Vertical Deviation Indicator (VDI; Figure 2-10) uses a magenta chevron to indicate the baro-VNV vertical deviation when Vertical Navigation (VNV) is being used; the VDI appears in conjunction with the “TOD within 1 minute” alert. Full-scale deflection (two dots) is 1000 feet. The VDI is removed from the display if vertical deviation becomes invalid. See the Flight Management and AFCS sections for details on VNV features, and refer to Section 2.2, Supplemental Flight Data, for more information about VNV indications on the PFDs. HAZARD AVOIDANCE The Glideslope Indicator (Figure 2-11) appears to the left of the Altimeter whenever an ILS frequency is tuned in the active NAV field and the aircraft heading and selected course are within 107°. A green diamond acts as the Glideslope Indicator, like a glideslope needle on a conventional indicator. If a localizer frequency is tuned and there is no glideslope, “NO GS” is displayed in place of the diamond. The glidepath is analogous to the glideslope for GPS approaches supporting SBAS 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 (Figure 2-12) appears as a magenta diamond during the approach. If the approach type downgrades past the final approach fix (FAF), “NO GP” is displayed in place of the diamond. AFCS Full-scale deflection of two dots is 1000 feet. VNV Target Altitude Marker Beacon Annunciation ADDITIONAL FEATURES Vertical Speed Indicator APPENDICES Vertical Deviation Indicator Required Vertical Speed Indicator Glideslope Indicator Glidepath Indicator INDEX Vertical Speed Pointer Figure 2-10 Vertical Speed and Deviation Indicators (VSI and VDI) 58 Figure 2-11 Glideslope Indicator Figure 2-12 Glidepath Indicator Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 and numeric labels occur every 30˚. Major tick marks are at 10˚ intervals and minor tick marks 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 bug. The HSI also presents turn rate, course deviation, bearing, and navigation source information and is available in two formats (360˚ compass rose and 140˚ arc). Changing the HSI display format: 1) Press the PFD Softkey. EIS 2) Press the HSI FRMT Softkey. 3) Press the 360 HSI or ARC HSI Softkey. 13 12 FLIGHT MANAGEMENT 14 1 11 10 4 9 5 8 6 7 Course Deviation Indicator 4 Navigation Source 5 To/From Indicator 6 Course Pointer 7 Rotating Compass Rose Lateral Deviation Scale 9 Aircraft Symbol 10 Flight Phase 11 Selected Heading Bug 12 Lubber Line 13 Current Heading 14 Turn Rate Indicator APPENDICES 3 8 ADDITIONAL FEATURES 2 Turn Rate/Heading Trend Vector Current Track Indicator AFCS 3 HAZARD AVOIDANCE 2 1 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. Figure 2-13 Horizontal Situation Indicator (HSI) INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 59 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, To/From Indicator, a sliding deviation indicator (the To/From and deviation indicators are combined), 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). EIS Course Pointer AUDIO PANEL & CNS Navigation Source Lateral Deviation Scale Flight Phase Annunciation Course Deviation and To/From Indicator Figure 2-14 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 bug on the compass rose corresponds to the Selected Heading. While the HSI is displayed as an arc, if the Selected 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 (see OBS Mode for adjusting a GPS course). Current Track Indicator Current Heading APPENDICES Selected Heading Selected Course INDEX Heading Bug Figure 2-15 Heading and Course Indications (Magnetic) 60 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 2-16 Heading and Course Indications (True) Changing the navigation angle setting: AUDIO PANEL & CNS 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. • TRUE - References angles to true north (T) • MAGNETIC - Angles corrected to the computed magnetic variation (Mag Var) FLIGHT MANAGEMENT 4) Turn the small FMS Knob to highlight the desired setting and press the ENT Key. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 2-17 Navigation Angle Settings (AUX - System Setup Page) INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 61 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 Standard Turn Rate AUDIO PANEL & CNS Arrow Shown for Turn Rate > 4 deg/sec FLIGHT MANAGEMENT Figure 2-18 Turn Rate Indicator and Trend Vector Bearing Pointer and Information Window HAZARD AVOIDANCE One bearing pointer and associated information can be displayed on the HSI for NAV, GPS, and ADF sources. The pointer is a light blue single-line arrow (BRG); an icon is shown in the respective information window to indicate the pointer. The bearing pointer never override the CDI and is visually separated from the CDI by a white ring (shown when bearing pointer is selected but not necessarily visible due to data unavailability). Tuning Mode AFCS Frequency Distance Bearing Pointer ADDITIONAL FEATURES DME Information Window APPENDICES Distance to Bearing Source Bearing Source Station Identifier Pointer Icon Bearing Information Window INDEX Figure 2-19 HSI with Bearing and DME Information 62 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 (BRG = single line) • GPS-derived great circle distance to bearing source • Frequency (NAV, ADF) FLIGHT INSTRUMENTS • Bearing source (NAV, GPS) EIS If the NAV radio is the bearing source and is tuned to an ILS frequency (refer to the Audio Panel and CNS Section for information on tuning the radios), the bearing pointer is removed from the HSI and the frequency is replaced with “ILS”. 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 in lieu of a frequency. The bearing pointer is removed from the HSI and “NO DATA” is displayed in the information window if: AUDIO PANEL & CNS • The NAV radio is not receiving the tuned VOR station • GPS is the bearing source and an active waypoint is not selected Selecting bearing display and changing sources: FLIGHT MANAGEMENT 1) Press the PFD Softkey. 2) Press the BRG Softkey to display the bearing pointer and information window with NAV1 source. 3) Press the BRG Softkey again to change the bearing source to NAV2. 4) Press the BRG Softkey a third time to change the bearing source to GPS. HAZARD AVOIDANCE 5) Press the BRG Softkey a fourth time to change the bearing source to ADF (ADF Radio installation is optional). 6) To remove the bearing pointer and information window, press the BRG Softkey again. DME Information Window AFCS 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. ADDITIONAL FEATURES Displaying the DME Information Window: 1) Press the PFD Softkey. 2) Press the DME Softkey to display the DME Information Window. APPENDICES 3) To remove the DME Information Window, press the DME Softkey again. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 63 SYSTEM OVERVIEW Flight Instruments Course Deviation Indicator (CDI) FLIGHT INSTRUMENTS 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. 360˚ HSI Arc HSI Flight Phase EIS Navigation Source Crosstrack Error AUDIO PANEL & CNS CDI Navigation Source CDI Scale Flight Phase CDI Scale FLIGHT MANAGEMENT Figure 2-20 Course Deviation Indicator APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE The CDI can display two sources of navigation: GPS or NAV (VOR, localizer). Color indicates the current navigation source: magenta (for GPS) or green (for VOR and LOC); the Selected Course readout also follows these color indications. When coupled to GPS, the full scale limits for the CDI are defined by a GPS-derived distance. When coupled to a VOR or localizer (LOC), the CDI has the same angular limits as a mechanical CDI. If the CDI exceeds the maximum deviation on the scale (two dots) while coupled to GPS, the crosstrack error (XTK) is displayed below the white aircraft symbol. INDEX Figure 2-21 Navigation Sources 64 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Instruments SYSTEM OVERVIEW Changing navigation sources: 1) Press the CDI Softkey to change from GPS to VOR1 or LOC1. The NAV1 standby frequency in the upper left corner of the MFD is light blue. FLIGHT INSTRUMENTS 2) Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2. The NAV2 standby frequency in the upper left corner of the MFD is light blue. 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 Pressing the CDI Softkey Cycles through Navigation Sources Figure 2-22 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 • 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 AFCS • 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 (see the Flight Management Section) also causes the CDI to switch to LOC navigation source; GPS steering guidance is not provided after this switch. APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 65 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 be displayed rather than the flight phase annunciation. Receiver Autonomous Integrity Monitoring (RAIM) protection limits follow the selected CDI scale and corresponding flight phases. Changing the selected GPS CDI setting: AUDIO PANEL & CNS 1) Use the FMS Knob to select the AUX - System Setup Page on the MFD. 2) Press the FMS Knob to activate the cursor. 3) Turn the large FMS Knob to highlight Selected in the GPS CDI box. FLIGHT MANAGEMENT 4) Turn the small FMS Knob to highlight the desired setting and press the ENT Key. ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE 5) To cancel the selection, press the FMS Knob or the CLR Key. APPENDICES Figure 2-23 GPS CDI Settings (AUX - System Setup Page) INDEX When set to ‘Auto’ (default), the GPS CDI scale automatically adjusts to the desired limits based upon the current phase of flight (Figure 2-24, Table 2-1). 66 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 Figure 2-24 Automatic CDI Scaling AUDIO PANEL & CNS • Once a departure procedure is activated, the CDI is scaled for departure (0.3 nm). • The system switches from departure to terminal CDI scaling (1.0 nm) under the following conditions: - The next leg in the departure procedure is not aligned with the departure runway FLIGHT MANAGEMENT - The next leg in the departure procedure is not a CA, CD, CF, CI, CR, DF, FA, FC, FD, FM, IF, or TF leg - After any leg in the departure procedure that is not a CA or FA leg • At 30 nm from the departure airport the enroute phase of flight is automatically entered and CDI scaling changes to 2.0 nm over a distance of 1.0 nm, except under the following conditions: HAZARD AVOIDANCE - When navigating with an active departure procedure, the flight phase and CDI scale does not change until the aircraft arrives at the last departure waypoint (if more than 30 nm from the departure airport) or the leg after the last departure waypoint has been activated or a direct-to waypoint is activated. • If after completing the departure procedure the nearest airport is more than 200 nm away from the aircraft and the approach procedure has not yet commenced, the CDI is scaled for oceanic flight (2.0 nm). AFCS • 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: ADDITIONAL FEATURES - 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 arrive route (if within 31 nm from the destination airport). • During approach, the CDI scale ramps down even further (see Figures 2-25 and 2-26). This transition normally occurs within 2.0 nm of the Final Approach Fix (FAF). The CDI switches to approach scaling automatically once the approach procedure is active or if Vectors-To-Final (VTF) are selected. APPENDICES - If the active waypoint is the FAF, the ground track and the bearing to the FAF must be within 45° of the final approach segment course. - If the active waypoint is part of the missed approach procedure, the active leg and the preceding missed approach legs must be aligned with the final approach segment course and the aircraft must not have passed the turn initiation point. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 67 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 2-25 Typical LNAV and LNAV+V Approach CDI Scaling Figure 2-26 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 leg HAZARD AVOIDANCE - After any leg in the missed approach procedure that is not a CA or FA leg Flight Phase Departure Terminal Enroute Oceanic Annunciation* DPRT TERM ENR OCN Approach (Non-precision) LNAV ADDITIONAL FEATURES AFCS 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 (see Figure 2-25) LNAV + V L/VNAV LPV MAPR 1.0 nm decreasing to a specified course width, then 0.3 nm, depending on variables (see Figure 2-26) 0.3 nm APPENDICES * 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 68 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 Mode is enabled, a course line is drawn through the “active-to” waypoint on the moving map. If desired, the course to/from the waypoint can now be adjusted. When OBS Mode is disabled, the GPS flight plan returns to normal operation with automatic sequencing of waypoints, following the course set in OBS Mode. The flight path on the moving map retains the modified course line. 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 2-27 Omni-bearing Selector (OBS) Mode AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 69 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 a CRS Knob to select the desired course to/from the waypoint. Press a 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 2-28. Pressing the SUSP Softkey, deactivates the suspension and resumes automatic sequencing of approach waypoints. HAZARD AVOIDANCE Pressing the SUSP Softkey Suspends Automatic Waypoint Sequencing SUSP Annunciation INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 2-28 Suspending Automatic Waypoint Sequencing 70 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Instruments SYSTEM OVERVIEW 2.2 Supplemental Flight Data Note: Pressing the DFLTS Softkey (a second-level PFD softkey) turns off metric Altimeter display, the Inset FLIGHT INSTRUMENTS 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. Temperature Display EIS The Outside Air Temperature (OAT) is displayed in degrees Celsius (°C) by default in the lower left of the PFD under normal display conditions, or below the true airspeed in reversionary mode. It may also be displayed in degrees Fahrenheit from the AUX - System Setup Page on the MFD. AUDIO PANEL & CNS Normal Display FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS Reversionary Mode ADDITIONAL FEATURES APPENDICES INDEX Figure 2-29 Outside Air Temperature 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 71 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 2-30 Temperature Selection (AUX - System Setup Page) 72 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Instruments SYSTEM OVERVIEW Wind Data 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 two different ways. Option 1 EIS Option 2 AUDIO PANEL & CNS No Data FLIGHT MANAGEMENT Figure 2-31 Wind Data Displaying wind data: HAZARD AVOIDANCE 1) Press the PFD Softkey. 2) Press the WIND Softkey to display wind data. 3) Press one of the OPTN softkeys to change how wind data is displayed: • OPTN 1: Wind direction arrow with numeric True direction and speed • OPTN 2: Headwind/tailwind and crosswind arrows with numeric speed components AFCS 4) To remove the window, press the OFF Softkey. ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 73 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 Table 2-2. Top of Descent Message EIS VNV Target Altitude FLIGHT MANAGEMENT AUDIO PANEL & CNS Vertical Deviation Indicator Required Vertical Speed Indicator HAZARD AVOIDANCE GPS is Selected Navigation Source Terminal Phase of Flight Figure 2-32 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 * If the flight director has been engaged to fly a VNV flight plan, the VNV Target Altitude being held remains displayed while on level flight plan legs. INDEX Table 2-2 VNV Indication Removal Criteria 74 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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. Marker Beacon Annunciations Marker Beacon Annunciations are displayed on the PFD to the left of the Selected Altitude. Outer marker reception is indicated in blue, middle in amber, and inner in white. Refer to the Audio Panel and CNS Section for more information on Marker Beacon Annunciations. Middle Marker EIS Outer Marker Inner Marker AUDIO PANEL & CNS Altimeter FLIGHT MANAGEMENT Figure 2-33 Marker Beacon Annunciations Traffic Annunciation HAZARD AVOIDANCE The Perspective™ system displays traffic symbolically on the Inset Map (PFD), the Navigation Map Page (MFD), and various other MFD page maps. Refer to the Hazard Avoidance Section for more details about the optional Traffic Advisory Systems (TAS). When a Traffic Advisory (TA) is detected, the following automatically occurs: • The PFD Inset Map is enabled, displaying traffic AFCS • A flashing black-on-yellow TRAFFIC annunciation (Figure 2-34) appears to the top left of the Attitude Indicator for 5 seconds and remains displayed until no TAs are detected in the area ADDITIONAL FEATURES • An aural traffic alert may be generated. Refer to the applicable traffic advisory system (TAS) documentation for alerts generated by TAS equipment. If additional TAs appear, new aural and visual alerts are generated. APPENDICES Traffic Symbol Figure 2-34 Traffic Annunciation INDEX Figure 2-35 Inset Map with Traffic Displayed 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 75 SYSTEM OVERVIEW Flight Instruments TAWS Annunciations HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Terrain Awareness and Warning System (TAWS) annunciations appear on the PFD to the upper left of the Altimeter (also where the marker beacon annunciations appear). Refer to the Hazard Avoidance Section and Appendix for information on TAWS alerts and annunciations. INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 2-36 Traffic and Example TAWS Annunciations 76 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Instruments SYSTEM OVERVIEW Altitude Alerting FLIGHT INSTRUMENTS The Altitude Alerting function provides the pilot with visual and aural alerts 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. The following occur when approaching the Selected Altitude: • Upon passing through 1000 feet of the Selected Altitude, the Selected Altitude (shown above the Altimeter) changes to black text on a light blue background and flashes for 5 seconds. • When the aircraft passes within 200 ft of the Selected Altitude, the Selected Altitude changes to light blue text on a black background and flashes for 5 seconds and a single chime is heard. Within 200 ft Deviation of ±200 ft AUDIO PANEL & CNS Within 1000 ft EIS • After reaching the Selected Altitude, if the pilot flies outside the deviation band (±200 feet of the Selected Altitude), the Selected Altitude changes to yellow text on a black background, flashes for 5 seconds, and the word “Altitude” is heard. Figure 2-37 Altitude Alerting Visual Annunciations FLIGHT MANAGEMENT Low Altitude Annunciation NOTE: The Low Altitude Annunciation is available only for aircraft with GIA 63W Integrated Avionics Units HAZARD AVOIDANCE when SBAS is available. This annunciation is not shown for systems with TAWS or TERRAIN-SVS, unless terrain alerting is inhibited.. AFCS When the Final Approach Fix (FAF) is the active waypoint in a GPS SBAS 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 Altimeter Figure 2-38 Low Altitude on GPS SBAS Approach APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 77 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), based on barometric altitude can be set. When active, the altitude setting is displayed to the lower left of the Altimeter and with a bug at the corresponding altitude along the Altimeter (once the altitude is within the range of the tape). The following visual annunciations alert the pilot when approaching the MDA or 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 the MDA/DH, the bug and text turn yellow and the aural alert, “Minimums Minimums”, is generated. AUDIO PANEL & CNS Alerting is inhibited while the aircraft is on the ground and until the aircraft reaches 150 feet above the setting for the alert. If the aircraft proceeds to climb after having reached the MDA/DH, once it reaches 50 feet above the MDA/DH, alerting is disabled. FLIGHT MANAGEMENT Within 2500 feet Within 100 feet Altitude Reached HAZARD AVOIDANCE MDA/DH Bug MDA/DH Setting Figure 2-39 Minimum Descent Altitude/Decision Height Alerting Visual Annunciations AFCS The MDA/DH may be set from either PFD and is synchronized on both PFDs. The function is reset when the power is cycled. Setting the Minimums Descent Altitude/Decision Height: ADDITIONAL FEATURES 1) Press the TMR/REF Softkey. 2) Turn the large FMS Knob to highlight the Minimums field. 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. APPENDICES 4) Use the small FMS Knob to enter the desired altitude (from zero to 16,000 feet). 5) To remove the window, press the CLR Key or the TMR/REF Softkey. INDEX Figure 2-40 MDA/DH Setting (Timer/References Window) 78 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Instruments SYSTEM OVERVIEW 2.4 Abnormal Operations Abnormal GPS Conditions FLIGHT INSTRUMENTS The annunciations listed in Table 2-3 can appear on the HSI when abnormal GPS conditions occur; see the figure for examples. Refer to the Flight Management Section for more information on Dead Reckoning Mode. Annunciation LOI AUDIO PANEL & CNS 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 Table 2-3 Abnormal GPS Conditions Annunciated on HSI FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 2-41 Example HSI Annunciations As a result of operating in DR Mode, all GPS-derived data is computed based upon an estimated position and is displayed in yellow on the display to denote degraded navigation source information. This data includes the following: AFCS • Navigation Status Box fields except Active Leg, TAS, and DTK • Course Deviation Indicator (removed after 20 minutes) • GPS Bearing Pointer ADDITIONAL FEATURES • Wind data and pointers in the Wind Data Box on the PFD • Track Indicator • All Bearing Pointer Distances APPENDICES • Active Flight Plan distances, bearings, and ETE values Also, while the Perspective™ system is in DR Mode, the autopilot will not couple to GPS, and terrain alerting (if installed) is disabled. Additionally, the accuracy of all nearest information (airports, airspaces, and waypoints) is questionable. Finally, airspace alerts continue to function, but with degraded accuracy. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 79 SYSTEM OVERVIEW Flight Instruments Unusual Attitudes FLIGHT INSTRUMENTS When the aircraft enters an unusual pitch attitude, red extreme pitch warning chevrons pointing toward the horizon are displayed on the Attitude Indicator, starting at 50˚ above and 30˚ below the horizon line. Nose Low AUDIO PANEL & CNS EIS Nose High Figure 2-42 Pitch Attitude Warnings HAZARD AVOIDANCE FLIGHT MANAGEMENT If pitch exceeds +30˚/-20˚ or bank exceeds 65˚, some information displayed on the PFD is removed. The Altimeter and Airspeed, Attitude, Vertical Speed, and Horizontal Situation indicators remain on the display and the Bearing Information, Alerts, and Annunciation windows can be displayed during such situations. The following information is removed from the PFD (and corresponding softkeys are disabled) when the aircraft experiences unusual attitudes: • Traffic Annunciations • System Time • AFCS Annunciations • PFD Setup Menu • Minimum Descent Altitude/ Decision Height readout • Flight director Command Bars • Windows displayed in the lower right corner of the PFD: • Vertical Deviation, Glideslope, and Glidepath Indicators • Outside Air Temperature – Timer/References • Altimeter Barometric Setting • DME Information Window – Nearest Airports • Selected Altitude • Wind data – Flight Plan • VNV Target Altitude • Selected Heading Box – Alerts • Selected Course Box – Procedures • Transponder Status Box – DME Tuning INDEX APPENDICES ADDITIONAL FEATURES AFCS • Inset Map 80 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Engine Indication System SYSTEM OVERVIEW Section 3 Engine Indication System FLIGHT INSTRUMENTS The Engine Indication System (EIS) displays critical engine, electrical, fuel, optional ice protection, and other system parameters on the left side of the Multi Function Display (MFD) during normal operations (Figure 3-1). EIS information can be fully expanded to an entire page (EIS - Engine Page) using the ENGINE Softkey. In Reversionary Mode, the display-combines Primary Flight Display (PFD) symbology with the EIS. EIS Display EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 3-1 MFD (SR20) AFCS Green bands on the instruments indicate normal ranges of operation; yellow and red bands indicate caution and warning, respectively. White or uncolored bands indicate areas outside of normal operation not yet in the safe ranges. When unsafe operating conditions occur, the corresponding readouts, pointers and labels change color corresponding to the level of the condition; warnings also flash (except fuel at destination). If sensory data to an instrument becomes invalid or unavailable, a red 'X' is displayed across the instrument. However the numeric readouts in the Fuel Calculation Box, TKS FIKI Anti Ice Box (optional), and the density altitude in the Air Data Box are replaced with dashes instead of red 'X's when the data is invalid or out of range. ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 81 SYSTEM OVERVIEW Engine Indication System 3.1 EIS Display FLIGHT INSTRUMENTS NOTE: Refer to the Pilot’s Operating Handbook (POH) for engine operating limitations. NOTE: Depictions of equipment may differ from the installed equipment. Examples shown may differ from AUDIO PANEL & CNS EIS actual aircraft configurations. 1 Percent Power Indicator (% Pwr) Displays engine power as a percentage 2 Tachometer (RPM) Displays propeller speed in revolutions per minute 3 Engine Manifold Pressure Indicator (Man “Hg) Fuel Flow Indicator (FFlow GPH) Displays manifold pressure in inches of Mercury to indicate engine power Displays fuel flow in gallons per hour (Turbo models only – displays a light blue target fuel flow indicator to the right of the fuel flow indicator strip, shown in Figure 3-3) Displays the fuel used in gallons 4 FLIGHT MANAGEMENT 5 8 Gallons Used Indicator (Gal Used) Oil Temperature Indicator (Oil ºF) Oil Pressure Indicator (Oil PSI) Ammeter (Batt1 A) 9 Voltmeter (ESS Bus V) 10 Cylinder Head Temperature Displays the head temperature of the hottest cylinder (CHT; cylinder number is shown below bar) Indicator (CHT ºF) Exhaust Gas Temperature Displays the exhaust gas temperature (cylinder number is shown below bar) (naturally aspirated models only) Indicator (EGT ºF) 6 AFCS HAZARD AVOIDANCE 7 11 Displays engine oil temperature in degrees Fahrenheit Displays pressure of oil supplied to the engine in pounds per square inch (psi) Displays the battery 1 load in amperes Displays the essential bus voltage in volts ADDITIONAL FEATURES Exhaust Gas Temperature/ Displays the exhaust gas temperature and turbine inlet temperature Turbine Inlet Temperature (cylinder number or turbine inlet side is shown below bar) (Turbo models only, shown in Figure 3-3) Indicator (EGT/TIT ºF) Left and Right Turbine Inlet Displays the temperature at the left (L) and right (R) turbine inlet (Turbo models only, shown in Figure 3-3). Temperature INDEX APPENDICES 12 82 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Engine Indication System SYSTEM OVERVIEW FLIGHT INSTRUMENTS 1 EIS 2 3 AUDIO PANEL & CNS 4 FLIGHT MANAGEMENT 5 6 7 8 HAZARD AVOIDANCE 9 10 AFCS 11 ADDITIONAL FEATURES Figure 3-2 EIS Display (SR20) APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 83 AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Engine Indication System 1 1 1 2 2 2 3 3 3 4 4 4 AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT Target Fuel Flow 5 5 5 6 6 6 7 7 7 8 8 8 9 9 9 10 10 10 11 11 SR22 (Naturally Aspirated) ADDITIONAL FEATURES Target Fuel Flow 12 SR22T 12 11 SR22TN INDEX APPENDICES Figure 3-3 EIS Display (SR22) 84 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A ENGINE (Optional) ENGINE ASSIST DCLTR Engine Indication System FUEL CO RST SYSTEM OVERVIEW 3.2 Engine PageSoftkey to Press the ENGINE return to the top-level softkeys. FLIGHT INSTRUMENTS TABS FULL Pressing the ENGINE Softkey accesses the EIS - Engine Page, which displays allUNDO engine,ENTER fuel, fuel calculation, electrical, air data, and optional ice protection information. Pressing the optional ANTI-ICE Softkey accesses the second-level softkeys. Pressing the FUEL Softkey accesses the second-level softkeys. Press the UNDO or ENTER Softkey to return to the second-level softkeys. NOTE: The ice protection system (optional) must be operated in accordance with the approved flight manual limitations. This option is only available on SR22 models. EIS ENGINE The ANTI-ICE Softkey and its secondlevel softkeys are only available with the TKS FIKI system installed. ANTI-ICE ASSIST DCLTR AUDIO PANEL & CNS (Optional) ENGINE FUEL CO RST Press the ENGINE Softkey to return to the top-level softkeys. (Optional) (Optional) (Optional) AUTO RIGHT FULL TABS FLIGHT MANAGEMENT LEFT BACK UNDO ENTER HAZARD AVOIDANCE Press the UNDO or ENTER Softkey to return to the second-level softkeys. Figure 3-4 Engine Page Softkeys INDEX Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T APPENDICES 190-00820-06 Rev. A ADDITIONAL FEATURES ANTI-ICE LEFT AUTO RIGHT DCLTR ASSIST CO RST FUEL FULL TABS UNDO ENTER Displays full Engine Page and second-level engine softkeys; press again to return to the Engine Strip and top-level softkeys (see the EIS Section for more information) Displays Anti-Ice softkeys (optional-TKS FIKI only; See Operational Note above) Selects manual mode and opens the left tank valve and closes the right tank valve Selects auto tank selection mode Selects manual mode and opens the right tank valve and closes the left tank valve Removes bars and temperature readouts from the Engine Temperature Box Identifies temperature peaks Resets the CO Guardian Accesses the Initial Usable Fuel Page Resets fuel totalizer to full (usable fuel) Resets fuel totalizer to tabs (usable fuel) Resets to the initial usable fuel amount shown on the Initial Usable Fuel Page Saves the usable fuel amount as displayed on the Initial Usable Fuel Page AFCS • ENGINE 85 SYSTEM OVERVIEW Engine Indication System Percent Power Indicator Displays engine power as a percentage (% Pwr) 2 Tachometer (RPM x100) Displays propeller speed in revolutions per minute 3 Engine Manifold Pressure Indicator (Man “Hg) Displays manifold pressure in inches of Mercury to indicate engine power 4 Fuel Flow Indicator (FFlow GPH) Oil Temperature and Pressure Indicators (Oil °F PSI) Displays fuel flow in gallons per hour (SR22T models only – displays a light blue target fuel flow indicator shown on top of the fuel flow gauge) Displays oil temperature in degrees Fahrenheit (°F) and pressure in pounds per square inch (psi) 6 Electrical Group (Electrical) Displays the alternator and battery current in amperes and the essential and main bus voltage 7 Fuel Calculation Group Displays calculated fuel at destination, fuel used, fuel remaining, time remaining, range (in nautical miles) and economy (in nautical miles per (Fuel Calculation) gallon) based on the displayed fuel remaining and the fuel flow totalizer 8 Air Data Displays density altitude, outside air temperature (OAT) in °F and °C, and international standard atmosphere (ISA) temperature deviation 9 Oxygen Pressure Indicator Displays oxygen pressure in tank in pounds per square inch (optional) 10 Anti-Ice Fluid Quantity TKS NH – Displays the quantity of anti-ice fluid remaining in the single tank (optional – See Operational Note below). Indicator (TKS NH and TKS FIKI) TKS FIKI – Displays the quantity of anti-ice fluid remaining in the left (L) and right (R) tanks in gallons (optional – See Operational Note below). 11 Engine Temperature Group (Engine Temperature) AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS 5 ADDITIONAL FEATURES NOTE: Refer to the Pilot’s Operating Handbook (POH) for engine operating limitations. 1 EIS FLIGHT INSTRUMENTS Displays head (CHT) and exhaust gas temperatures (EGT) of all cylinders in °F (all models) and turbine inlet temperatures (turbo models only) APPENDICES NOTE: The ice protection system (optional) must be operated in accordance with the approved flight manual INDEX limitations. This option is only available on SR22 models. 86 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Engine Indication System SYSTEM OVERVIEW NOTE: Depictions of equipment may differ from the installed equipment. Examples shown may not represent all possible aircraft configurations. 2 3 4 FLIGHT INSTRUMENTS 1 5 EIS AUDIO PANEL & CNS 6 12 7 FLIGHT MANAGEMENT 8 1 2 3 4 HAZARD AVOIDANCE Figure 3-5 Engine Page (SR20) 5 AFCS ADDITIONAL FEATURES 6 12 APPENDICES 7 11 8 INDEX Figure 3-6 Engine Page (SR22) with TKS NH Anti-Ice Option 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 87 SYSTEM OVERVIEW Engine Indication System 2 3 Target Fuel Flow Indicator 4 5 EIS FLIGHT INSTRUMENTS 1 6 AUDIO PANEL & CNS 11 7 10 8 FLIGHT MANAGEMENT 9 Figure 3-7 Engine Page (SR22T) with TKS FIKI and Oxygen 2 3 Target Fuel Flow Indicator 4 5 AFCS HAZARD AVOIDANCE 1 6 ADDITIONAL FEATURES 12 APPENDICES 7 10 8 INDEX Figure 3-8 Engine Page (SR22TN) with Oxygen 88 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Engine Indication System SYSTEM OVERVIEW Fuel Calculations NOTE: Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time FLIGHT INSTRUMENTS the fuel was reset. Fuel used (Used), time remaining (Time Rem), range (in nautical miles, Range), and economy (Econ) are calculated based on the displayed fuel remaining (Rem) and the fuel flow totalizer. The calculated range is based upon ground speed, distance, economy and fuel remaining. See the Flight Management Section for information regarding the map feature related to the EIS Fuel Calculations. EIS Adjusting the fuel totalizer quantity: 1) Press the ENGINE Softkey to display the Engine Page. AUDIO PANEL & CNS 2) Press the FUEL Softkey to access the Initial Usable Fuel Page. 3) Turn the FMS Knob (small knob adjusts in 1 gallon increments and large knob in 10 gallon increments) to increase or decrease the initial usable fuel displayed. FLIGHT MANAGEMENT Calculated Fuel Used Fuel Remaining Calculated Time Remaining Calculated Range HAZARD AVOIDANCE Calculated Economy Figure 3-9 Fuel Calculations Group AFCS ADDITIONAL FEATURES APPENDICES 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX Figure 3-10 Full Fuel (SR20) Initial Usable Fuel Page 89 AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Engine Indication System ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT Figure 3-11 Fuel to TABS (SR22) Initial Usable Fuel Page INDEX APPENDICES Figure 3-12 Full Fuel (SR22) Initial Usable Fuel Page 90 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Engine Indication System SYSTEM OVERVIEW Ice Protection Systems FLIGHT INSTRUMENTS The Perspective™ System interfaces with either of two optional ice protection systems, TKS No-Hazard (NH) or TKS Flight Into Known Icing (FIKI) anti-ice systems. Refer to the applicable Pilot’s Operating Handbook (POH) for a detailed system description of the installed ice protection system. NOTE: The ice protection system (optional) must be operated in accordance with the approved flight manual limitations. This option is only available on SR22 models. The TKS NH system displays a single quantity gauge on the full Engine Page to indicate the amount of antiice fluid available. EIS AUDIO PANEL & CNS Figure 3-13 TKS NH System Fluid Quantity Gauge FLIGHT MANAGEMENT TKS Flight Into Known Icing (FIKI) Anti-Ice System HAZARD AVOIDANCE The FIKI system offers five pilot-selectable (external to the Perspective™ System) modes of operation and a more sophisticated quantity indicator located on the full Engine Page. To accommodate the additional modes, the TKS FIKI system employs several additional sensors. The Perspective™ System receives inputs from these sensors and provides indications as to the status of the TKS FIKI system. Auto Tank Selection Mode AFCS In the default tank selection mode (AUTO), Perspective™ assures that the fluid levels of the two tanks are kept relatively even by periodically closing the tank with the lowest level. The system uses the anti-ice fluid tank quantities to control the tank shut-off valves. When the system is on and operating in AUTO mode, the shut-off valves close under the following conditions: • The fluid quantity is empty (indicated from the fluid level sensor and level switch) ADDITIONAL FEATURES • The left and right tank level imbalance is greater than 0.25 gallons (low tank will be closed until level balance is within 0.15 gallons) • The fluid quantity is unreliable (a miscompare between the level sensor and level switch or an out of range level sensor value) APPENDICES While operating in AUTO mode a white box is displayed around the ‘L’ and ‘R’, located on top of each fluid quantity indicator, when both tanks are open. During normal operation, the white box will highlight the left or right tanks as the fluid levels change (Figure 3-14). INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 91 FLIGHT INSTRUMENTS SYSTEM OVERVIEW Engine Indication System Figure 3-14 AUTO Tank Mode (Normal) FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS If a fluid level comparison fault is detected (the fluid level sender disagrees with the fluid level switch for a particular tank) the corresponding fluid quantity indicator is grayed out (Figure 3-15) and that quantity is not used in the endurance and range calculations. When the fluid level sender is out of range, the fluid quantity indicator is marked with a red ‘X’ (Figure 3-16). HAZARD AVOIDANCE Figure 3-15 Fluid Level Unreliable Figure 3-16 Fluid Level Out Of Range Manual Tank Mode AFCS Manual tank mode allows the pilot to control either tank’s shut-off valve. Manual may be selected by pressing the ANTI-ICE Softkey to access the second-level softkeys LEFT, AUTO, and RIGHT. A light blue box is displayed around the selected tank, gallons remaining in the selected tank, and pump operating mode. • LEFT Softkey – opens left tank valve and closes right tank valve • AUTO Softkey – returns to AUTO tank mode ADDITIONAL FEATURES • RIGHT Softkey – opens right tank valve and closes left tank valve INDEX APPENDICES While operating in manual tank mode, only the selected/open tank’s quantity is used for the range and endurance calculations. Figure 3-17 Manual Tank Mode (Left tank selected) 92 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Engine Indication System SYSTEM OVERVIEW Pump Operating Modes The Ice Protection systems consists of various pump operating modes listed below. FLIGHT INSTRUMENTS NOTE: The ice protection system (optional) must be operated in accordance with the approved flight manual limitations. This option is only available on SR22 models. Operating Mode OFF NORM Comments No modes selected Provides 50% flow rate for light/moderate icing EIS Provides 100% flow rate for moderate icing Provides 200% flow rate for severe icing or to expedite the removal of previous ice buildup This mode is used in the event of a timer box failure or when BKUP mode is selected. Pump #2 provides 100% flow rate, bypassing the timer box AUDIO PANEL & CNS HIGH MAX (momentary) PUMP BKUP System Operation System Off Both pumps operate on a timed, repeating cycle – 30 seconds ON and 90 seconds OFF A single pump (#1) operates continuously Both pumps operate continuously for 120 seconds A single pump (#2) operates continuously FLIGHT MANAGEMENT Refer to the POH for pilot recommended actions Table 3-1 FIKI System Operating Modes HAZARD AVOIDANCE Figure 3-20 Max Operating Mode Figure 3-21 Pump Backup Mode ADDITIONAL FEATURES Figure 3-19 High Operating Mode AFCS Figure 3-18 Normal Operating Mode APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 93 SYSTEM OVERVIEW Engine Indication System 3.3 Leaning Assist Mode FLIGHT INSTRUMENTS NOTE: The pilot should follow the engine manufacturer’s recommended leaning procedures in the Pilot’s Operating Handbook (POH). A leaning assist function is available on the Engine Page to assist in the leaning process. Accessing Leaning Assist Mode: 1) Press the ENGINE Softkey to display the Engine Page. EIS 2) Press the ASSIST Softkey to identify peaks. AUDIO PANEL & CNS When the ASSIST Softkey is pressed, the system initially highlights the number and places a light blue box around the EGT readout of the cylinder with the hottest EGT. The ∆ Peak temperature is the difference between the peak temperature and the present temperature for the peaked cylinder. When the first peak is detected, “1st” is annunciated below that cylinder’s EGT bar and the temperature is enclosed in a light blue box. FLIGHT MANAGEMENT The system continues to detect peak EGTs for each cylinder lean of peak as the fuel flow is decreased, and the peak of each cylinder’s EGT is indicated by a light blue marker on the graph. Once all cylinders are lean of peak, the last cylinder to peak is denoted by the “Last” annunciation below its bar on the graph. HAZARD AVOIDANCE Light Blue Box Represents Peak AFCS Temperature Deviation from Peak INDEX APPENDICES ADDITIONAL FEATURES Figure 3-22 Leaning Assist Mode 94 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Engine Indication System SYSTEM OVERVIEW 3.4 EIS Display in Reversionary Mode FLIGHT INSTRUMENTS In reversionary mode, the display combines PFD symbology with the EIS Display (refer to the System Overview for information about display Reversionary Mode). In reversionary mode, the EIS is separated into two displays: Engine (identical to the normal EIS Display on the MFD) and System. For a description of the EIS Display, refer to Section 3.1. The System Display shows various system parameters and fuel calculations. EIS EIS Display AUDIO PANEL & CNS FLIGHT MANAGEMENT INSET SENSOR PFD OBS CDI DME XPDR IDENT TMR/REF NRST HAZARD AVOIDANCE (optional) ENGINE ALERTS Figure 3-23 Reversionary Mode (SR22T) AFCS ENGINE SYSTEM BACK ADDITIONAL FEATURES ENGINE ALERTS Press the BACK Softkey to return to the top-level softkeys. APPENDICES Figure 3-24 EIS Softkeys (Reversionary Mode) INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 95 SYSTEM OVERVIEW Engine Indication System System Display FLIGHT INSTRUMENTS NOTE: Fuel calculations do not use the aircraft fuel quantity indicators and are calculated anytime the initial usable fuel is changed. NOTE: Refer to the Pilot’s Operating Handbook (POH) for limitations. The EIS System Display shows the engine, fuel calculations, electrical, and various system parameters. Fuel calculations are based on the displayed fuel remaining and the fuel flow totalizer. EIS Accessing the EIS System Display: 1) Press the ENGINE Softkey. AUDIO PANEL & CNS 2) Press the SYSTEM Softkey. 3) To return to the default Engine Display, press the ENGINE or BACK Softkey. FLIGHT MANAGEMENT 1 2 3 HAZARD AVOIDANCE 4 5 Displays engine power as a percentage Engine Manifold Pressure Indicator (Man “Hg) Fuel Calculation Group (Fuel Calc) Displays manifold pressure in inches of Mercury to indicate engine power Displays calculated fuel at destination, fuel used, fuel remaining, time remaining, range (in nautical miles) and economy (in nautical miles per gallon) based on the displayed fuel remaining and the fuel flow totalizer Displays the alternator and battery current in amperes and the essential and main bus voltage Displays engine hours and anti-ice gallons (optional) and oxygen pressure (optional) Electrical Group (Electrical) Miscellaneous (Misc) Shows propeller speed in revolutions per minute INDEX APPENDICES ADDITIONAL FEATURES AFCS 6 Percent Power Indicator (% Pwr) Tachometer (RPM) 96 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Engine Indication System SYSTEM OVERVIEW FLIGHT INSTRUMENTS 1 EIS 2 3 4 AUDIO PANEL & CNS FLIGHT MANAGEMENT 5 HAZARD AVOIDANCE 6 6 AFCS SR20 SR22 Models with optional Anti-Ice and Oxygen ADDITIONAL FEATURES Figure 3-25 System Display APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 97 FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Engine Indication System INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Blank Page 98 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 A/C or Mode S transponder. The System Overview Section provides a block diagram description of the Audio Panels and CNS system interconnection. CNS operation in the avionics system is performed by the following Line Replaceable Units (LRUs): • Multifunction Display (MFD) • Mode A/C or Mode S Transponder • Integrated Avionics Unit (2) • Control Unit AUDIO PANEL & CNS • Audio Panel EIS • Primary Flight Display (PFD) 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 system, 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 or Mode A/C transponder is controlled with softkeys and the FMS Knob located on the Primary Flight Display (PFD) and also the Control Unit. The Transponder Data Box is located to the left of the System Time Box. The data box displays the active four-digit code, mode, and a reply status (Figures 4-1 and 4-2). AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 99 SYSTEM OVERVIEW Audio Panel and CNS MFD/PFD Controls and Frequency Display 2 3 4 FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 1 5 HAZARD AVOIDANCE 6 7 8 INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 4-1 PFD Controls, COM Frequency Tuning Boxes, Transponder Code, and DME Tuning Window 100 1 COM Frequency Box – Displays COM standby and active frequency fields and volume. The selected COM transceiver frequency is displayed in green. 2 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. 3 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. 4 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. 5 DME Tuning Window – Displays DME frequency pairing mode. Display by pressing the DME Softkey. 6 ENT Key – Validates or confirms DME pairing mode and Auto-tune selection. Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Audio Panel and CNS 10 11 SYSTEM OVERVIEW 9 12 FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 4-2 MFD Controls and NAV Frequency Tuning Boxes 9 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. 10 NAV Frequency Transfer Key – Transfers the standby and active NAV frequencies. 11 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. 12 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. 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX Transponder Data Box – Indicates the selected transponder code, operating mode, reply, and ident status for the applicable transponder. APPENDICES 8 ADDITIONAL FEATURES FMS Knob – Flight Management System Knob, used to enter transponder codes, select DME modes, and Auto-tune entries when 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. AFCS 7 101 SYSTEM OVERVIEW Audio Panel and CNS GMA 347 Audio Panel Controls 2 3 4 5 6 16 17 18 19 7 8 10 9 EIS FLIGHT INSTRUMENTS 1 12 AUDIO PANEL & CNS 11 13 14 15 20 21 22 23 24 25 Figure 4-3 GMA 347 Audio Panel Controls Marker Beacon Annunciators – Each annunciator lights independently when flying over the associated marker beacon station. 2 MKR/MUTE – Selects marker beacon receiver audio. Mutes the currently received marker beacon receiver audio. Unmutes automatically when new marker beacon audio is received. Enables Music Mute feature. Also, stops play of recorded COM audio. 3 COM1 – When selected, audio from the #1 COM receiver can be heard. 4 COM2 – When selected, audio from the #2 COM receiver can be heard. 5 COM3 – Reserved for optional COM radio. 6 NAV1 – When selected, audio from the #1 NAV receiver can be heard. ADDITIONAL FEATURES 7 NAV2 – When selected, audio from the #2 NAV receiver can be heard. 8 DME – Turns optional DME audio on or off. 9 ADF – Turns optional ADF receiver audio on or off. 10 PLAY – Press once to play the last recorded COM audio. Press again while audio is playing and the previous block of recorded audio will be played. Each subsequent press plays each previously recorded block. Pressing the MKR/MUTE Key during play of a memory block stops play. 11 PILOT Squelch – Turn to adjust Pilot’s squelch. The Pilots volume knob must be pressed to allow manual squelch adjustment. INDEX AFCS HAZARD AVOIDANCE 1 APPENDICES FLIGHT MANAGEMENT NOTE: When a key is selected, an annunciator in the key is illuminated. 102 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Audio Panel and CNS 16 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. 17 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. 18 COM3 MIC – Reserved for optional COM radio. 19 COM 1/2 – Split COM operation key. When selected, the pilot uses the COM 1 transceiver and the copilot uses COM 2. 20 SPKR – Selects and deselects the cabin speaker. COM and NAV receiver audio can be heard on the speaker. Press and hold for 2 seconds for Passenger Address (PA). The SPKR key flashes during PA. 21 TEL – Selects and deselects telephone audio. 22 COPLT – Selects and deselects the copilot intercom isolation. 23 PILOT – Selects and deselects the pilot intercom isolation. 24 COPILOT/PASS Volume – Turn to adjust Copilot/Passenger intercom volume or squelch. Pulling the right volume knob controls passenger volume, pushing in controls Copilot volume. 25 COPILOT/PASS Squelch – Copilot and passenger share the squelch knob. ADDITIONAL FEATURES HI SENS Annunciator – Indicates marker beacon receiver sensitivity, high sensitivity when illuminated, low sensitivity when extinguished. AFCS 15 HAZARD AVOIDANCE SENS – Press to increase marker beacon receiver sensitivity as indicated by illumination of the HI SENS annunciator. Press again to return to low sensitivity and extinguish the HI SENS annunciator. FLIGHT MANAGEMENT 14 AUDIO PANEL & CNS MAN SQ – Manual Squelch annunciator. When lit, pilot and copilot squelch knobs control manual squelch. EIS 13 FLIGHT INSTRUMENTS PILOT Volume – Turn the left (Pilot) volume knob to control pilot’s intercom volume and the ON and OFF function. (Full CCW detent is OFF) Press to switch between manual and automatic squelch control as indicated by illumination of the MAN SQ annunciator. SYSTEM OVERVIEW 12 APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 103 SYSTEM OVERVIEW Audio Panel and CNS Control Unit FLIGHT INSTRUMENTS The Control Unit is a pedestal-mounted interface allowing data entry, COM and NAV tuning, and transponder control. Many procedures can be performed using the Control Unit rather than the MFD/PFD display bezel controls. Annunciators above the FMS, XPDR, NAV, and COM keys are illuminated when their respective control modes are selected. EIS COM and NAV radio tuning can be accomplished from the control unit. The appropriate frequency box on the selected display is outlined by a light blue selection box, which flashes for a few seconds to indicate control unit activity. Selection of a different display control or radio tuning mode results in cancelation of the previous radio tuning mode. 2 3 4 6 5 7 FLIGHT MANAGEMENT AUDIO PANEL & CNS 1 9 HAZARD AVOIDANCE 8 ADDITIONAL FEATURES AFCS 10 12 11 Figure 4-4 Control Unit APPENDICES Tuning Selection Box INDEX Figure 4-5 Frequency Tuning with the Control Unit 104 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Audio Panel and CNS COM Key – Selects COM radio tuning mode on the Control Unit. The COM tuning box is outlined with a light blue selection line when the COM frequency is active on the control unit (Figure 4‑5). 5 FMS Key – Places Control Unit in Flight Management System (FMS) Mode. FMS Knob is used to enter transponder codes, select DME modes, and Auto-tune entries when 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. 6 XPDR Key – Places Control Unit in Transponder Mode. Transponder code entry can be performed with either the number keypad or FMS/XPDR NAV/COM Knob. 7 NAV Key – Selects NAV radio tuning mode on the Control Unit. The NAV tuning box is outlined with a light blue selection line when the NAV frequency is active on the control unit. 8 CLR Key – Erases information, cancels entries, or removes menus. 9 Frequency Transfer Key (EMERG) – Transfers the standby and active COM or NAV frequencies. Press and hold for two seconds to tune the emergency frequency (121.500 MHz) automatically into the COM active frequency field. 10 Alphanumeric Keys – Allows data entry (rather than using the FMS Knob to select characters/ numbers). 11 Decimal Key – Enters a decimal point. 12 BKSP Key – Moves cursor back one character space and removes last character entered. AFCS 4 HAZARD AVOIDANCE FMS/XPDR NAV/COM Knob – NAV/COM Tuning Modes: Acts as the NAV or COM Knob. XPDR Mode: Acts as the XPDR Softkey. FMS Control Modes: Acts as the FMS Knob. FLIGHT MANAGEMENT 3 AUDIO PANEL & CNS ENT Key – Validates or confirms a menu selection or data entry. EIS 2 FLIGHT INSTRUMENTS MENU Key – Displays a list of options for accessing additional features or making setting changes. SYSTEM OVERVIEW 1 ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 105 SYSTEM OVERVIEW Audio Panel and CNS 4.2 COM Operation FLIGHT INSTRUMENTS COM Transceiver Selection and Activation NOTE: During PA Mode (press and hold SPKR Key) 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 avionics 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 displayed on the PFD; 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 (SPKR Key is selected and flashing on the Audio Panel). Frequencies in the standby field are displayed in light blue and white. The standby frequency in the tuning field is white. The other standby frequency is light blue. HAZARD AVOIDANCE Active Fields Standby Fields AFCS Tuning Field ADDITIONAL FEATURES COM2 Radio is Selected on the Audio Panel APPENDICES Figure 4-6 Selecting a COM Radio for Transmit INDEX COM3 is reserved for an optional COM radio. 106 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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. EIS Annunciator Flashes During Transmission Transmit and Receive Indicators AUDIO PANEL & CNS Figure 4-7 COM Radio Transmit and Receive Indications COM Transceiver Manual Tuning FLIGHT MANAGEMENT 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 4-8 COM Frequency Tuning INDEX 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 107 SYSTEM OVERVIEW Audio Panel and CNS Manual frequency tuning from the Control Unit 1) Press the COM Key to select the COM frequency box. FLIGHT INSTRUMENTS 2) Turn the FMS/XPDR COM/NAV Knob to tune the desired frequency in the COM Tuning Box (large knob for MHz; small knob for kHz). 3) Press the Frequency Transfer Key to transfer the frequency to the active field. EIS First, Press the COM Key to Place the Tuning Selection Box on the COM frequencies and Activate COM tuning from the FMS/XPDR COM/NAV Knob AUDIO PANEL & CNS Second, Turn the COM/NAV Knob to Enter a Frequency into the COM Standby Frequency Field FLIGHT MANAGEMENT Third, Press the Frequency Transfer Key to Move the Frequency to the Active Field. Figure 4-9 Frequency Tuning from the Control Unit Selecting the Radio to be Tuned AFCS HAZARD AVOIDANCE Press the small COM Knob to transfer the light blue frequency tuning field and Frequency Transfer Arrow between the upper and lower radio frequency fields. ADDITIONAL FEATURES Press the COM Knob to Switch the Tuning Field From One COM Radio to the Other Figure 4-10 Switching COM Tuning Fields Quick-tuning and Activating 121.500 MHz INDEX APPENDICES Pressing and holding the COM Frequency Transfer Key for two seconds automatically loads the emergency COM frequency (121.500 MHz) in the active field of the COM radio selected for tuning (the one with the transfer arrow). In the example shown, pressing the Audio Panel COM2 MIC Key activates the transceiver. Press for Two Seconds to Load 121.500 MHz Figure 4-11 Quickly Tuning 121.500 MHz 108 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Audio Panel and CNS SYSTEM OVERVIEW Auto-tuning the COM Frequency FLIGHT INSTRUMENTS COM frequencies can be automatically tuned from the following: • Nearest Airports Window (PFD) • NRST – Nearest Frequencies Page (ARTCC, FSS, WX) • WPT – Airport Information Page • NRST – Nearest Airspaces Page • NRST – Nearest Airports Page Auto-tuning from the PFD 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 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX Figure 4-12 Nearest Airports Window (PFD) 109 SYSTEM OVERVIEW Audio Panel and CNS Auto-tuning from the MFD FLIGHT INSTRUMENTS Frequencies can be automatically loaded into the COM Frequency field from pages in the NRST or WPT page group by highlighting the frequency and pressing the ENT Key (Figures 4-13, 4-14, and 4-15). 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 4-15). 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 Field FLIGHT MANAGEMENT Turn the FMS Knob to Scroll Through a List of Frequencies Figure 4-13 Frequency Auto-Tuning from the MFD HAZARD AVOIDANCE Or: 1) On the Nearest Airports, Frequencies, or Airspaces page, 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. 5) Press the ENT Key to load the COM frequency into the standby field of the selected COM radio. APPENDICES ADDITIONAL FEATURES 6) Press the Frequency Transfer Key to transfer the frequency to the COM Active Frequency Field. INDEX Nearest Airports Menu Nearest Frequencies Menu Nearest Airspaces Menu Figure 4-14 Nearest Pages Menus 110 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 Selected Airport Identifier and Information EIS AUDIO PANEL & CNS Runway Information FLIGHT MANAGEMENT Press ENT Key to load frequency into COM Standby Field. Cursor then advances to the next frequency. HAZARD AVOIDANCE Press INFO-1 Softkey for AIRPORT, RUNWAYS, and FREQUENCIES Windows COM Frequency Loads into PFD Standby Frequency Field AFCS Figure 4-15 Airport Information Page and PFD Frequency Display ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 111 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 4-16 NRST – Nearest Airspaces, NRST – Nearest Airports, and NRST – Nearest Frequencies Pages 112 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Audio Panel and CNS SYSTEM OVERVIEW Frequency Spacing FLIGHT INSTRUMENTS The COM radios can tune either 25-kHz spacing (118.000 to 136.975 MHz) or 8.33-kHz spacing (118.000 to 136.990 MHz) for 760-channel or 3040-channel configuration. When 8.33-kHz channel spacing is selected, all of the 25-kHz channel spacing frequencies are also available in the complete 3040-channel list. 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 4-17 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 softkeys are blank. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Select 8.33-kHz or 25.0-kHz COM Frequency Channel Spacing INDEX Figure 4-18 AUX – System Setup Page 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 113 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 When Automatic Squelch is disabled, a white SQ appears next to the COM frequency. Squelch Indication Press the COM VOL/ SQ Knob to turn off Automatic Squelch. Press again to restore Automatic Squelch. AUDIO PANEL & CNS Figure 4-19 Overriding Automatic Squelch Volume HAZARD AVOIDANCE 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. INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 4-20 COM Volume Level COM Volume Level Remains for Two Seconds 114 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 displayed on the MFD; 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 light blue NAV tuning field and the Frequency Transfer Arrow are placed by the active NAV Frequency. 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 (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 (not 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 AFCS Tuning Field The NAV Radio is Selected by Pressing the CDI Softkey ADDITIONAL FEATURES Figure 4-21 Selecting a NAV Radio for Navigation APPENDICES See the Flight Instruments Section for selecting the DME and Bearing Information windows and using VOR as the source for the bearing pointer. INDEX 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 115 SYSTEM OVERVIEW Audio Panel and CNS 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 speakers (if selected). All radios can be selected individually or simultaneously. EIS Figure 4-22 Selecting a NAV Radio Receiver NAV Receiver Manual Tuning AUDIO PANEL & CNS The NAV frequency controls and frequency boxes are on the left side of the PFDs. Manually tuning a NAV frequency: 1) Turn the NAV Knob to tune the desired frequency in the NAV Tuning Box. FLIGHT MANAGEMENT 2) Press the Frequency Transfer Key to transfer the frequency to the NAV Active Frequency Field. 3) Adjust the volume level with the NAV VOL/ID Knob. 4) Press the NAV VOL/ID Knob to turn the Morse code identifier audio on and off. HAZARD AVOIDANCE 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 AFCS Turn the NAV Knob to Tune the Frequency in the Tuning Field ADDITIONAL FEATURES Figure 4-23 NAV Frequency Tuning Selecting the Radio to be Tuned APPENDICES Press the small NAV Knob to transfer the frequency tuning box and Frequency Transfer Arrow between the upper and lower radio frequency fields. INDEX Press the NAV Knob to Switch the Tuning Field From One NAV Radio to the Other Figure 4-24 Switching NAV Tuning Boxes 116 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Audio Panel and CNS SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS In the example shown, in order to listen to either station identifier, press the NAV1 or NAV2 Key on the Audio Panel. Pressing the VOL/ID Knob turns off the Morse code audio only in the radio with the NAV Tuning Box. To turn off both NAV IDs, transfer the NAV Tuning Box between NAV1 and NAV2 by pressing the small NAV Knob and pressing the VOL/ID Knob again to turn the Morse code off in the other radio. EIS The Morse Code Identifier for the VORs is On Station Identifiers AUDIO PANEL & CNS Figure 4-25 NAV Radio ID Indication Volume FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE NAV Volume Level Remains for Two Seconds Figure 4-26 NAV Volume Levels Auto-tuning a NAV Frequency from the MFD AFCS NAV frequencies can be selected and loaded from the following MFD pages: • WPT – Airport Information • NRST – Nearest VOR • NRST – Nearest Frequencies (FSS, WX) • NRST – Nearest Airports • NRST – Nearest Airspaces ADDITIONAL FEATURES • WPT – VOR Information APPENDICES 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 4-27, 4-28, and 4-29). Auto-tuning a NAV frequency from the WPT and NRST Pages: INDEX 1) From any page that the NAV 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 NAV identifier or NAV frequency. 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 117 SYSTEM OVERVIEW Audio Panel and CNS 3) On the Nearest VOR, Nearest Airspaces, and Nearest Airports pages, press the FREQ Softkey to place the cursor on the NAV frequency (Figure 4-29). 4) Press the ENT Key to load the NAV frequency into the standby field of the selected NAV radio. FLIGHT INSTRUMENTS 5) Press the Frequency Transfer Key to transfer the frequency to the NAV Active Frequency Field. AUDIO PANEL & CNS EIS 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 Field Figure 4-27 NAV Frequency Auto-Tuning from the MFD Or: FLIGHT MANAGEMENT 1) When on the NRST pages, press the MENU Key to display the page menu. 2) Turn the large FMS Knob to scroll through the menu options. 3) Press the ENT Key to place the cursor in the desired window. 4) Scroll through the frequency selections with the FMS Knob. HAZARD AVOIDANCE 5) Press the ENT Key to load the NAV frequency into the standby field of the selected NAV radio. ADDITIONAL FEATURES AFCS 6) Press the Frequency Transfer Key to transfer the frequency to the NAV Active Frequency Field. Nearest Airports Menu Nearest VOR Menu Nearest Frequencies Menu Nearest Airspaces Menu INDEX APPENDICES Figure 4-28 Nearest Pages Menus 118 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Audio Panel and CNS SYSTEM OVERVIEW 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 INSTRUMENTS EIS AUDIO PANEL & CNS Press the FREQ Softkey to Place the Cursor on the VOR Frequency HAZARD AVOIDANCE Press the VOR Softkey to Place the Cursor on the VOR Identifier FLIGHT MANAGEMENT Press the ENT Key to Load the Frequency into the NAV Standby Field. Figure 4-29 Loading the NAV Frequency from the NRST – Nearest VOR Page AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 119 SYSTEM OVERVIEW Audio Panel and CNS APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 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. INDEX Figure 4-30 NRST – Nearest Frequencies, WPT – VOR Information, WPT – Airport Information, and NRST – Nearest Airports Pages 120 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Audio Panel and CNS SYSTEM OVERVIEW Auto-tuning NAV Frequencies on Approach Activation NOTE: The primary NAV frequency is auto-tuned upon loading a VOR or ILS/Localizer approach. FLIGHT INSTRUMENTS NOTE: When an ILS/LOC approach has been activated in GPS Mode, the system switches to NAV Mode as the final approach course is intercepted (within 15 nm of the FAF). See the GPS Navigation 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 or NAV2 active frequency fields. The frequency that was previously in the NAV1 or NAV2 active frequency fields are transferred to standby. • If the current CDI navigation source is GPS, and if the approach frequency is already loaded into the NAV1 or NAV2 standby frequency field, the standby frequency is transferred to active. FLIGHT MANAGEMENT • 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. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 121 SYSTEM OVERVIEW Audio Panel and CNS 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. EIS The receiver detects the three marker tones – outer, middle, and inner – and provides the marker beacon annunciations located on the Audio Panel and to the left of the Altimeter on the PFD. Operation of the two marker beacon indications may not be synchronized. Middle Marker Indication Inner Marker Indication FLIGHT MANAGEMENT AUDIO PANEL & CNS Outer Marker Indication AFCS HAZARD AVOIDANCE Figure 4-31 Marker Beacon Annunciations on the PFD ADDITIONAL FEATURES The Audio Panels provide three different states of marker beacon operation; On, Muted, and Deselected. Pressing the MKR/MUTE Key selects and deselects marker beacon audio. The key annunciator indicates when marker beacon audio is selected. APPENDICES During marker beacon audio reception, pressing the MKR/MUTE Key mutes the audio but does not affect the marker annunciations. 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. INDEX Figure 4-32 Marker Beacon Keys and Annunciator Lights Pressing the 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. 122 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Audio Panel and CNS SYSTEM OVERVIEW DME Tuning NOTE: When another auxiliary window is turned on, the DME Tuning Window is replaced on the PFD. FLIGHT INSTRUMENTS NOTE: When turning on the Avionics for use, the system remembers the last frequency used for DME tuning and the NAV1, NAV2, or HOLD state prior to shutdown. The PFD tunes the optional DME transceiver. 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. EIS The DME Tuning Window is located to the right of the HSI in the lower right corner of the PFD. The DME transceiver is tuned by selecting NAV1, NAV2, or HOLD in the DME Tuning Window. Pressing the DME Softkey switches the DME Tuning Window on and off. AUDIO PANEL & CNS DME Modes FLIGHT MANAGEMENT Figure 4-33 DME Tuning Window HAZARD AVOIDANCE The following DME transceiver pairings can be selected: • NAV1 – Pairs the DME frequency from the selected NAV1 frequency. • NAV2 – Pairs the DME frequency from the selected NAV2 frequency. AFCS • HOLD – When in the HOLD position, the DME frequency remains paired with the last selected NAV frequency. Selecting DME transceiver pairing: 1) Press the DME Softkey to display the DME Tuning Window. ADDITIONAL FEATURES 2) Turn the small FMS Knob to select the DME tuning mode. 3) Press the ENT Key to complete the selection. APPENDICES Pressing the CLR Key or FMS Knob while in the process of DME pairing cancels the tuning entry and reverts back to the previously selected DME tuning state. Pressing the FMS Knob activates/deactivates the cursor in the DME Tuning Window. See the Flight Instruments Section for displaying the DME information window. INDEX 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 123 SYSTEM OVERVIEW Audio Panel and CNS 4.4 GTX 32/GTX 33 Transponder The GTX 32 Transponder provides Mode A and Mode C interrogation and reply capabilities. 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 EIS • Flight ID (Flight Identification) reporting – The Mode S Transponder reports aircraft identification as either the aircraft registration or a unique Flight ID. • Altitude reporting AUDIO PANEL & CNS • Airborne status determination • 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. HAZARD AVOIDANCE • Extended squitter (optional) – Transmits the Automatic Dependent Surveillance-Broadcast (ADS-B) position, velocity, and heading information periodically without requiring an interrogation. The Hazard Avoidance Section provides more details on traffic avoidance systems. Transponder Controls AFCS 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. ADDITIONAL FEATURES 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, pressing the BKSP Softkey moves the code selection cursor to the previous digit. Pressing the BKSP Softkey again moves the cursor to the next previous digit. 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. APPENDICES The code can also be entered with the FMS Knob on the PFD or the XPDR Key and numeric keypad or FMS/XPDR NAV/COM Knob. Code entry must be completed with either the softkeys, numeric keypad, or the FMS Knob, but not a combination of both. 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 control inactivity, the system reverts back to the top-level softkeys. 124 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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. EIS 0 1 2 3 4 5 6 7 IDENT BKSP BACK ALERTS AUDIO PANEL & CNS Pressing the BACK Softkey returns to the mode selection softkeys. Figure 4-34 Transponder Softkeys (PFD) FLIGHT MANAGEMENT Transponder Mode Selection 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. HAZARD AVOIDANCE Selecting a transponder mode: 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 selecting any one of the Mode Selection Softkeys. A green GND indication and transponder code appear in the mode field of the Transponder Data Box. 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. APPENDICES GND Mode Figure 4-35 Ground Mode INDEX 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 125 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 pressed, 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 inhibited. AUDIO PANEL & CNS EIS STBY Mode (White Code Number and Mode) Figure 4-36 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) AFCS Figure 4-37 ON Mode Altitude Mode (Automatic or Manual) ADDITIONAL FEATURES Altitude Mode is automatically selected when the aircraft becomes airborne. Altitude Mode may also be selected manually by pressing the ALT Softkey. 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. APPENDICES ALT Mode (Mode C Altitude Reporting) INDEX Figure 4-38 Altitude Mode 126 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Audio Panel and CNS SYSTEM OVERVIEW 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 INSTRUMENTS Reply to Interrogation EIS Figure 4-39 Reply Indication Entering a Transponder Code AUDIO PANEL & CNS Entering a transponder code with softkeys: 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. FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE Entering a Code Figure 4-40 Entering a Code with Softkeys AFCS Entering a transponder code with the PFD FMS Knob: 1) Press the XPDR and the CODE Softkey as in the previous procedure to enable code entry. ADDITIONAL FEATURES 2) Turn the small FMS Knob to enter the first two code digits. 3) Turn the large FMS Knob to move the cursor to the next code field. 4) Enter the last two code digits with the small FMS Knob. APPENDICES 5) Press the ENT Key to complete code digit entry. INDEX 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 127 SYSTEM OVERVIEW Audio Panel and CNS FLIGHT INSTRUMENTS Pressing the CLR Key or small FMS Knob before code entry is complete cancels code entry and restores the previous code. Waiting for 10 seconds after code entry is finished activates the code automatically. Turn the Small FMS Knob to Enter Two Code Digits at a Time Press the ENT Key to Complete Code Entry Turn the Large FMS Knob to Move the Cursor to the Next Code Field EIS Figure 4-41 Entering a Code with the FMS Knob Entering a transponder code with the Control Unit AUDIO PANEL & CNS 1) Press the XPDR Key to select the transponder function on the FMS/XPDR COM/NAV Knob. 2) Turn the small FMS/XPDR COM/NAV Knob to enter the first two code digits. 3) Turn the large FMS/XPDR COM/NAV Knob to move the cursor to the next code field. FLIGHT MANAGEMENT 4) Enter the last two code digits with the small FMS/XPDR COM/NAV Knob. HAZARD AVOIDANCE 5) Press the ENT Key to complete code digit entry. Or: Enter a Code with the Numeric Keypad. Five seconds after the fourth digit has been entered, the transponder code becomes active. 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. AFCS First, Press the XPDR Key to Select Transponder Code Entry from the FMS/XPDR COM/NAV Knob ADDITIONAL FEATURES Second, Turn the FMS/XPDR COM/NAV Knob to Enter a Code, Small Knob Enters Code Digits, Large Knob Moves Cursor to the Next Code Field. APPENDICES Third, Press the ENT Key to Complete Code Entry INDEX Or Enter a Code with the Numeric Keypad Figure 4-42 Entering a Code with the Control Unit 128 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 AUDIO PANEL & CNS Figure 4-43 VFR Code IDENT Function FLIGHT MANAGEMENT NOTE: In Standby Mode, the IDENT Softkey is inoperative. HAZARD AVOIDANCE 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. After the IDENT Softkey is pressed while in Mode or Code Selection, the system reverts to the top-level softkeys. IDNT Indication AFCS ADDITIONAL FEATURES Press the IDENT Softkey to Initiate the ID Function Figure 4-44 IDENT Softkey and Indication APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 129 SYSTEM OVERVIEW Audio Panel and CNS 4.5 Additional Audio Panel Functions FLIGHT INSTRUMENTS Power-Up 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, 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. 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. HAZARD AVOIDANCE The speaker volume is adjustable within a nominal range. Contact a Garmin-authorized service center for volume adjustment. Figure 4-45 Speaker Key AFCS Intercom APPENDICES ADDITIONAL FEATURES The Audio Panel includes a four-position intercom system (ICS) and two stereo music inputs for the pilot, copilot and up to two passengers. The intercom provides Pilot and Copilot isolation from the passengers and aircraft radios. INDEX Figure 4-46 Intercom Controls 130 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Audio Panel and CNS OFF ON ON OFF OFF ON OFF ON OFF ON OFF ON ON ON ON OFF ON ON Selected radios, aural alerts, pilot, copilot, TEL audio Copilot Selected radios, aural alerts, pilot, passengers, music2, TEL audio Pilot, passengers Selected radios, aural alerts, pilot, copilot Passengers, music2, TEL audio Passengers Selected radios, aural alerts, pilot, copilot, TEL audio Passengers, music2 Pilot, copilot AFCS ON Selected radios, aural alerts, pilot; passengers, music1, TEL audio Selected radios, aural alerts, pilot, copilot Copilot HAZARD AVOIDANCE OFF Selected radios, Selected radios, aural alerts, pilot; Copilot, TEL audio aural alerts, pilot, passengers, music1 passengers, music2 FLIGHT MANAGEMENT OFF AUDIO PANEL & CNS OFF EIS OFF Pilot Copilot Passenger Input to Hears Hears Hears Phone Selected radios, Selected radios, Selected radios, aural alerts, pilot, aural alerts, pilot, aural alerts, pilot, None copilot, passengers, copilot, passengers, copilot, passengers, music1 music1 music2 Selected radios, Selected radios, Selected radios, aural alerts, pilot, aural alerts, pilot, aural alerts, pilot, Pilot, copilot, copilot, passengers, copilot, passengers, copilot, passengers, passengers music1, TEL audio music1, TEL audio music2, TEL audio Copilot, Copilot, Selected radios, Copilot, passengers, passengers, passengers aural alerts, pilot music1, TEL audio music2, TEL audio Selected radios, Copilot, Copilot, Pilot aural alerts, pilot, passengers, music1 passengers, music2 TEL audio FLIGHT INSTRUMENTS OFF SYSTEM OVERVIEW PILOT KEY COPLT KEY TEL KEY Annunciator Annunciator Annunciator Table 4-1 ICS Isolation Modes & Telephone Distribution 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. APPENDICES 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. 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. 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 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. 131 SYSTEM OVERVIEW Intercom Volume and Squelch FLIGHT INSTRUMENTS Audio Panel and CNS Each microphone input has an automatic squelch threshold. Manual squelch is available by pressing the Pilot side VOL/SQ knob. When the MAN SQ annunciation is lit the large squelch knobs control pilot and copilot/passenger squelch threshold. Turning either knob clockwise increases the squelch threshold level. Turning either knob counterclockwise decreases the squelch threshold level. Two volume controls, one for the pilot and a combined copilot/passenger control, set intercom audio level. EIS When the MAN SQ annunciation is not lit, squelch is automatic and the large squelch knobs have no function. AUDIO PANEL & CNS Manual Squelch Annunciation; Off for Automatic Squelch, On for Manual Squelch FLIGHT MANAGEMENT Rotating the Pilot Volume Knob controls ON and OFF function. (Full CCW detent is OFF) Pressing the Pilot volume knob switches between manual and automatic squelch. Pilot Volume, On/Off, and Manual Squelch Pulling the right volume knob controls passenger volume, pushing in controls Copilot volume. Copilot and passenger share the large squelch knob. Copilot/Passenger Volume and Manual Squelch Figure 4-47 Intercom Volume and Squelch Controls HAZARD AVOIDANCE Passenger Address (PA) System ADDITIONAL FEATURES AFCS A passenger address system is available for delivering voice messages over the cabin speaker. Press and hold the SPKR Key for two seconds to activate the passenger address. The SPKR Key Annunciator flashes about once per second when the passenger address is active. A Push-to-Talk (PTT) must be pressed to deliver PA announcements. PA is Selected on the Audio Panel INDEX APPENDICES Figure 4-48 SPKR Key Selected for PA Announcements 132 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Audio Panel and CNS SYSTEM OVERVIEW Clearance Recorder and Player FLIGHT INSTRUMENTS 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. The PLAY Key controls the play function. Pressing the PLAY Key once plays the latest recorded memory block. 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. EIS 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. Powering off the unit automatically clears all recorded blocks. AUDIO PANEL & CNS Figure 4-49 Play Key FLIGHT MANAGEMENT NOTE: Split COM performance is affected by the distance between the COM antennas and the separation 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. HAZARD AVOIDANCE 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. AFCS 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. ADDITIONAL FEATURES 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. COM1 Radio is Used by the Pilot APPENDICES COM2 Radio is Used by the Copilot INDEX Figure 4-50 Split COM Operation 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 133 SYSTEM OVERVIEW Audio Panel and CNS Entertainment Inputs NOTE: Music1 and Music2 audio cannot be completely turned off. Audio level for the crew and passengers FLIGHT INSTRUMENTS can be adjusted by a Garmin-authorized service center. EIS The Audio Panel provides two stereo auxiliary entertainment inputs: Music1 and Music2. The pilot and copilot hear Music1 and the passengers hear Music2. These inputs are compatible with popular portable entertainment devices such as MP3 and CD players. Two 3.5-mm stereo phone jacks are installed in convenient locations for audio connection. The headphone outputs of the entertainment devices are plugged into the Music1 or Music2 jacks. The current ICS state of isolation affects the distribution of the entertainment input (see Table 4‑1). AUDIO PANEL & CNS Crew Music Crew music, either XM Radio or Music1, can be heard by the pilot and copilot when both the PILOT and the COPLT ICS Annunciators are extinguished. Crew music can also be heard by the pilot when the COPLT Annunciator is illuminated and by the copilot when the PILOT Annunciator is illuminated. FLIGHT MANAGEMENT Music Muting HAZARD AVOIDANCE Crew music muting occurs when aircraft radio or marker beacon activity is heard. Crew music is always soft muted when an interruption occurs from these sources. Soft muting is the gradual return of music to its original volume level. The time required for music volume to return to normal is between one-half and four seconds. Music Muting Enable/Disable AFCS Pressing and holding the MKR/MUTE Key for three seconds switches crew music muting on and off. When switching, either one or two beeps are heard; one beep indicates that music muting is enabled, two beeps indicate music muting is disabled. Crew music muting is reset (enabled) during power up. Passenger Music Passenger music, either XM Radio or Music2, can be heard only by the passengers and is never muted. ADDITIONAL FEATURES XM Radio Entertainment APPENDICES 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 Connecting a stereo input to the audio jack removes the XM Radio Audio from that input. 134 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Audio Panel and CNS SYSTEM OVERVIEW Multifunction Controls FLIGHT INSTRUMENTS The Pilot side volume knob controls the ON and OFF function, the pilot’s intercom volume plus manual and automatic squelch. When pressed, manual squelch is selected and the MAN SQ LED is ON indicating that squelch is adjusted manually. When pressed again the MAN SQ LED turns OFF and squelch is automatic. The Copilot side volume knob controls the Copilot and passenger intercom volume level. Pulling the right volume knob controls passenger volume, pushing in controls Copilot volume. EIS Pilot Volume, On/Off, and Manual Squelch Copilot/Passenger Volume and Manual Squelch AUDIO PANEL & CNS Figure 4-51 Intercom Volume and Squelch Controls The MKR/MUTE key selects marker audio and silences the marker signal. It also turns On/Off Music Muting, plus cancels the COM clearance recorder audio playback. FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 4-52 Marker/Mute Key The SPKR key turns the cabin speaker ON and OFF. Pressing and holding for 2 seconds selects PA mode. The SPKR key annunciator blinks when PA is active. AFCS Figure 4-53 Speaker Key ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 135 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 is activated, 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. FLIGHT MANAGEMENT AUDIO PANEL & CNS After powering up the avionics System, the following steps will aid in maximizing the use of the Audio Panel as well as prevent pilot and copilot induced issues. These preflight procedures should be performed each time a pilot boards the aircraft to insure awareness of all audio levels in the Audio Panel and radios. HAZARD AVOIDANCE Automatic/Manual Squelch Annunciation Pilot and Copilot ICS Isolation Keys Copilot/Passenger Volume and Manual Squelch Pilot Volume and Manual Squelch Figure 4-54 Audio Panel Preflight Controls AFCS Setting the Audio Panel during preflight: 1) Verify that the PILOT and COPLT Annunciators are extinguished. 2) Verify that manual squelch is set to full open. ADDITIONAL FEATURES 3) Turn the PILOT Knob and COPILOT Knob fully clockwise. This will set the headset intercom 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 Knob and COPILOT Knob volume to the desired intercom level. APPENDICES 6) Reset squelch to automatic, or adjust to the appropriate level manually. INDEX Once this procedure has been completed, the pilot and copilot can change settings, keeping in mind the notes above. 136 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Audio Panel and CNS SYSTEM OVERVIEW 4.7 Abnormal Operation FLIGHT INSTRUMENTS Abnormal operation includes equipment failures of the avionics components and failure of associated equipment, including switches and external devices. Audio Panel Fail-safe Operation 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 during fail-safe operation. Fail-safe operation may be tested by turning the Audio Panel off. EIS Stuck Microphone AUDIO PANEL & CNS If the push-to-talk (PTT) Key becomes stuck, the COM transmitter stops transmitting after 35 seconds of continuous operation. An alert appears on the PFD to advise the crew of a stuck microphone. The COM1 MIC or COM2 MIC Key Annunciator on the Audio Panel flashes as long as the PTT Key remains stuck. FLIGHT MANAGEMENT Figure 4-55 Stuck Microphone Alert HAZARD AVOIDANCE 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. AFCS Emergency Channel Loaded Automatically ADDITIONAL FEATURES Figure 4-56 COM Tuning Failure APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective ™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 137 FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Audio Panel and CNS INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Blank Page 138 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Section 5 Flight Management FLIGHT INSTRUMENTS 5.1 Introduction Perspective™ is an integrated flight, engine, communication, navigation and surveillance system. This section of the Pilot’s Guide explains flight management using the system. EIS The most prominent part of the system 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 The Inset Map is a small version of the MFD Navigation Map and can be displayed in the lower left corner of the PFD. When the system is in reversionary mode, the Inset Map is displayed in the lower right corner. The Inset Map is displayed by pressing the INSET Softkey. Pressing the INSET Softkey again, then pressing the OFF Softkey removes the Inset Map. HAZARD AVOIDANCE 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 pressing 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). AFCS 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. ADDITIONAL FEATURES 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). APPENDICES 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 139 SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS Navigation Status Box GPS Track (dashed line) 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 Destination Airport Info - Identifier - Fuel Remaining - Distance - Estimated Time Enroute - Bearing Navigation Page Title Navigation Map HAZARD AVOIDANCE - Aviation Data - Geographic Data - Topographic Data - Hazard Data Map Orientation Flight Plan Leg Aircraft Icon at Present Position AFCS Active Flight Plan Leg ADDITIONAL FEATURES Map Range Figure 5-2 GPS Navigation Information on the MFD Navigation Page APPENDICES Navigation Status Box The Navigation Status Box located at the top of the PFD contains two fields displaying the following information: INDEX PFD Navigation Status Box 140 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management • Distance (DIS) and Bearing (BRG) to the next waypoint or flight plan annunciations (e.g., ‘TOD within 1 minute’) • Bearing (BRG) The symbols used in the PFD status bar are: Symbol Direct-to Left Procedure Turn Right Holding Pattern • Desired Track (DTK) • Endurance (END) • Enroute Safe Altitude (ESA) • Estimated Time of Arrival (ETA) • Estimated Time Enroute (ETE) • Fuel on Board (FOB) • Ground Speed (GS) • Minimum Safe Altitude (MSA) • True Air Speed (TAS) • Track Angle Error (TKE) Vector to Final • Track (TRK) FLIGHT MANAGEMENT Left Holding Pattern Right DME Arc AUDIO PANEL & CNS Right Procedure Turn • Distance (DIS) EIS Description Active Leg FLIGHT INSTRUMENTS The Navigation Status Box located at the top of the MFD contains four data fields, each displaying one of the following items: SYSTEM OVERVIEW • Active flight plan leg (e.g., ‘D-> KICT’ or ‘KIXD -> KCOS’) or flight plan annunciations (e.g., ‘Turn right to 021˚ in 8 seconds’) • Vertical Speed Required (VSR) HAZARD AVOIDANCE • Crosstrack Error (XTK) Left DME Arc MFD Navigation Status Box AFCS 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. ADDITIONAL FEATURES Changing a field in the MFD Navigation Status Box: 1) Select the System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. APPENDICES 3) Turn the large FMS Knob to highlight the desired field number in the MFD Data Bar Fields Box. 4) Turn the small FMS Knob to display and scroll through the data options list. 5) Select the desired data. 6) Press the ENT Key. Pressing the DFLTS Softkey returns all fields to the default setting. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 141 SYSTEM OVERVIEW Flight Management 5.2 Using Map Displays FLIGHT INSTRUMENTS Map displays are used extensively in Perspective to provide situational awareness in flight. Most Perspective maps can display the following information: • Airports, NAVAIDs, airspaces, airways, land data (highways, cities, lakes, rivers, borders, etc.) with names AUDIO PANEL & CNS EIS • Map Pointer information (distance and bearing to pointer, location of pointer, name, and other pertinent information) • Aircraft icon (representing present position) • Nav range ring • Fuel range ring • Flight plan legs • User waypoints • Map range • Track vector • Wind direction and speed • Topography scale • Map orientation • Topography data • Icons for enabled map features HAZARD AVOIDANCE FLIGHT MANAGEMENT • Obstacle data 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 Map Orientation APPENDICES ADDITIONAL FEATURES AFCS 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 INDEX • 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. • Heading up (HDG UP) aligns the top of the map display to the current aircraft heading. 142 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS Note: Map orientation can only be changed on the Navigation Map Page. All other displays (except the PFD Inset Map) that show navigation data reflect the orientation selected for the Navigation Map Page. The PFD Inset Map is always Heading Up (if heading is invalid, then track up). Changing the Navigation Map orientation: EIS 1) With the Navigation Map Page displayed, press the MENU Key. The cursor flashes on the ‘Map Setup’ option. AUDIO PANEL & CNS Map Setup Selection FLIGHT MANAGEMENT Figure 5-4 Navigation Map Page Menu Window 2) Press the ENT Key to display the Map Setup Window. HAZARD AVOIDANCE 3) Turn the large FMS Knob, or press the ENT Key once, to select the ‘ORIENTATION’ field. Map Group Selection Orientation Field AFCS ADDITIONAL FEATURES APPENDICES Figure 5-5 Map Setup Menu Window - Map Group 4) Turn the small FMS Knob to select the desired orientation. 5) Press the ENT Key to select the new orientation. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX 6) Press the FMS Knob to return to the base page. 143 SYSTEM OVERVIEW Flight Management Map Range FLIGHT INSTRUMENTS 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 Perspective 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. AUDIO PANEL & CNS EIS Range Overzoom FLIGHT MANAGEMENT Figure 5-6 Map Range Auto Zoom HAZARD AVOIDANCE Auto zoom allows Perspective 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). AFCS 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. ADDITIONAL FEATURES 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. APPENDICES • 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. INDEX • 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. 144 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW • The ‘time out’ time (configurable on the Map Setup Page for the Map Group) determines how long auto zoom is overridden by a manual adjustment of the range knob. At the expiration of this time, the auto zoom range is restored. Setting the ‘time out’ value to zero causes the manual override to never time out. FLIGHT INSTRUMENTS • 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. Manual Range Override Expiration Time EIS Auto Zoom: Off, MFD Only, PFD Only, All On Maximum Look Forward Time Minimum Look Forward Time AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-7 Map Setup Menu Window - Map Group, Auto Zoom HAZARD AVOIDANCE Configuring automatic zoom: 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Select the ‘Map’ group. AFCS 4) Press the ENT Key. 5) Highlight the ‘AUTO ZOOM’ field. ADDITIONAL FEATURES 6) Select ‘Off’, ‘MFD Only’, ‘PFD Only’, or ‘ALL On’. 7) Press the ENT Key to accept the selected option. The flashing cursor highlights the ‘MAX LOOK FWD’ field. Times are from zero to 999 minutes. 8) Use the FMS Knobs to set the time. Press the ENT Key. APPENDICES 9) Repeat step 8 for ‘MIN LOOK FWD’ (zero to 99 minutes) and ‘TIME OUT’ (zero to 99 minutes). 10) Press the FMS Knob to return to the Navigation Map Page. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 145 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. 146 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 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. AFCS Information about Airspace ADDITIONAL FEATURES Map Pointer on Airspace APPENDICES INDEX Figure 5-10 Navigation Map - Map Pointer on Airspace 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 147 SYSTEM OVERVIEW Flight Management Panning the map: 1) Press the Joystick to display the Map Pointer. FLIGHT INSTRUMENTS 2) Move the Joystick to move the Map Pointer around the map. 3) Press the Joystick to remove the Map Pointer and recenter the map on the aircraft’s current position. 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. AUDIO PANEL & CNS EIS 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. AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT NAVAID Information GO BACK Softkey INDEX APPENDICES ADDITIONAL FEATURES Figure 5-11 Navigation Map - Information Window - NAVAID 148 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Viewing airspace information for a special-use or controlled airspace: 1) Place the Map Pointer on an open area within the boundaries of an airspace. 2) Press the ENT Key to display an options menu. FLIGHT INSTRUMENTS 3) ‘Review Airspaces’ should already be highlighted, if not select it. Press the ENT Key to display the Airspace Information Page for the selected airspace. 4) Press the CLR or ENT Key to exit the Airspace Information Page. EIS Airspace Information AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 5-12 Navigation Map - Information Window - Airspace AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 149 SYSTEM OVERVIEW Flight Management 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. FLIGHT MANAGEMENT Measurement Line Pointer Lat/Long ADDITIONAL FEATURES AFCS Measurement Information HAZARD AVOIDANCE 5) To exit the Measure Bearing/Distance option, press the Joystick; or select ‘Stop Measuring’ from the Page Menu and press the ENT Key. INDEX APPENDICES Figure 5-13 Navigation Map - Measuring Bearing and Distance 150 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 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. Topographic data can also be displayed on the selectable profile map at the bottom of the navigation map. Navigation Map Topographic Data Navigation Map Black Background EIS AUDIO PANEL & CNS TOPO Softkey Not Enabled Topographic Data on Profile Map TOPO Softkey Enabled Figure 5-14 Navigation Map - Topographic Data TOPO On FLIGHT MANAGEMENT TOPO Off 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’. 7) Press the FMS Knob to return to the Navigation Map Page. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 151 FLIGHT INSTRUMENTS SYSTEM OVERVIEW Flight Management AUDIO PANEL & CNS EIS TOPO DATA On/Off TOPO DATA Range Figure 5-15 Navigation Map Setup Menu - TOPO DATA Setup FLIGHT MANAGEMENT The topographic data range is the maximum map range on which topographic data is displayed. Note: Since the PFD Inset Map is much smaller than the MFD navigation maps, items are removed on the HAZARD AVOIDANCE PFD Inset Map two range levels smaller than the range selected in the Map Setup pages (e.g., a setting of 100 nm removes the item at ranges above 100 nm on MFD navigation maps, while the PFD Inset Map removes the same item at 50 nm). Selecting a topographical data range (TOPO DATA): 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. AFCS 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘TOPO DATA’ range field. TOPO ranges are from 500 ft to 2000 nm. ADDITIONAL FEATURES 6) To change the TOPO range setting, turn the small FMS Knob to display the range list. 7) Select the desired range using the small FMS Knob. 8) Press the ENT Key. APPENDICES 9) Press the FMS Knob to return to the Navigation Map Page. INDEX 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. 152 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Maximum Displayed Elevation Minimum Displayed Elevation FLIGHT INSTRUMENTS Aircraft Altitude (MSL) Range of Displayed Elevations Ground Elevation at Map Pointer Location (only visible when Map Pointer is displayed) EIS AUDIO PANEL & CNS Figure 5-16 Navigation Map - TOPO SCALE Displaying/removing the topographic scale (TOPO SCALE): FLIGHT MANAGEMENT 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 select the ENT Key. 4) Highlight the ‘TOPO SCALE’ field. HAZARD AVOIDANCE 5) Select ‘On’ or ‘Off’. 6) Press the FMS Knob to return to the Navigation Map Page. AFCS ADDITIONAL FEATURES APPENDICES TOPO SCALE On/Off Figure 5-17 Navigation Map Setup Menu - TOPO SCALE Setup INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 153 SYSTEM OVERVIEW Flight Management 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 EIS (Text label size can be None, Small, Medium (Med), or Large (Lrg)) Symbol Latitude/Longitude (LAT/LON) Default Maximum Range (nm) Range (nm) Off 2000 ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS Highways and Roads Interstate Highway (FREEWAY) 300 800 International Highway (FREEWAY) 300 800 US Highway (NATIONAL HWY) 30 80 State Highway (LOCAL HWY) 15 30 Local Road (LOCAL ROAD) 8 15 Railroads (RAILROAD) 15 30 LARGE CITY (> 200,000) 800 1500 MEDIUM CITY (> 50,000) 100 200 SMALL CITY (> 5,000) States and Provinces (STATE/PROV) 20 800 50 1500 Rivers and Lakes (RIVER/LAKE) 200 500 USER WAYPOINT 150 300 N/A INDEX APPENDICES Table 5-1 Land Symbol Information 154 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Aviation Symbols The following items are configured on the aviation menu: Aviation Symbols Symbol Default Maximum Range (nm) Range (nm) 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 See Airports, NAVAIDs See Additional Features N/A APPENDICES 2000 250 150 50 3 Off 15 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) ADDITIONAL FEATURES 2000 AFCS 2000 HAZARD AVOIDANCE Non-active Flight Plan Leg (ACTIVE FPL) FLIGHT MANAGEMENT 2000 AUDIO PANEL & CNS 2000 EIS Active Flight Plan Leg (ACTIVE FPL) FLIGHT INSTRUMENTS (Text label size can be None, Small, Medium (Med), or Large (Lrg)) Table 5-2 Aviation Symbol Information INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 155 SYSTEM OVERVIEW Flight Management Symbol Setup FLIGHT INSTRUMENTS All pages with maps can display land symbols (roads, lakes, borders, etc). Land symbols can be removed totally (turned off). Displaying/removing all land symbols: 1) Press the MENU Key with the Navigation Map Page displayed. The Page Menu is displayed and the cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Group Menu is displayed and the cursor flashes on the ‘Map’ option. EIS 3) Highlight the ‘LAND DATA’ field. 4) Select ‘On’ or ‘Off’. FLIGHT MANAGEMENT AUDIO PANEL & CNS 5) Press the FMS Knob to return to the Navigation Map Page. HAZARD AVOIDANCE LAND DATA On/Off AFCS Figure 5-18 Navigation Map Setup Menu - LAND DATA Setup The label size (TEXT) sets the size at which labels appear on the display (none, small, medium, and large). The range (RNG) sets the maximum range at which items appear on the display. 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. INDEX 7) Press the ENT Key to accept the selected size. 8) Select the desired range. 156 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 9) Press the ENT Key to accept the selected range. 10) Press the FMS Knob to return to the Navigation Map Page. FLIGHT INSTRUMENTS Maximum Display Range EIS Text Label Size (None, Small, Med, or Lrg) AUDIO PANEL & CNS Figure 5-19 Navigation Map Setup Menu - LAND GROUP Setup FLIGHT MANAGEMENT HAZARD AVOIDANCE Text Label Size (None, Small, Med, or Lrg) Maximum Display Range AFCS ADDITIONAL FEATURES Figure 5-20 Navigation Map Setup Menu - AVIATION GROUP Setup APPENDICES 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). INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 157 SYSTEM OVERVIEW Flight Management Map Declutter FLIGHT INSTRUMENTS The declutter feature allows the pilot to progressively step through four levels of removing map information. The declutter level is displayed in the DCLTR Softkey and next to the Declutter Menu Option. Declutter Level EIS DCLTR Softkey Navigation Map Page Menu AUDIO PANEL & CNS Figure 5-21 Navigation Map - Declutter Level Indications FLIGHT MANAGEMENT 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: 1) Press the MENU Key with the Navigation Map Page displayed. 2) Select ‘Declutter’. The current declutter level is shown. HAZARD AVOIDANCE 3) Press the ENT Key. Decluttering the PFD Inset Map: 1) Press the INSET Softkey. INDEX APPENDICES ADDITIONAL FEATURES AFCS 2) Press the DCLTR Softkey. The current declutter level is shown. With each selection, another level of map information is removed. 158 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Table 5-3 lists the items displayed at each declutter level. The ‘X’ represents map items displayed for the various levels of declutter. Item FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES 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 Table 5-3 Navigation Map Items Displayed by Declutter Level INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 159 SYSTEM OVERVIEW Flight Management 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. FLIGHT MANAGEMENT When airways are selected for display on the map, the airway waypoints (VORs, NDBs and Intersections) are also displayed. AFCS HAZARD AVOIDANCE Low Altitude Airway (Victor Airway) APPENDICES ADDITIONAL FEATURES High Altitude Airway (Jet Route) INDEX Figure 5-22 Airways on MFD Navigation Page 160 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 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 (AIRWAY ON). 3) Select the softkey again to display Low Altitude Airways only (AIRWAY LO). 4) Select the softkey again to display High Altitude Airways only (AIRWAY HI). EIS 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. 6) Press the FMS Knob to return to the Navigation Map Page. Off, All, LO Only, HI Only HAZARD AVOIDANCE Airway Display Selection Low Altitude Airway Range High Altitude Airway Range Figure 5-23 Navigation Map Setup Menu - AIRWAYS Setup AFCS The airway range is the maximum map range on which airways are displayed. Selecting an airway range (LOW ALT AIRWAY or HI ALT AIRWAY): 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) Turn the small FMS Knob to select the ‘Airways’ group, and press the ENT Key. APPENDICES 4) Highlight the ‘LOW ALT AIRWAY’ or ‘HI ALT AIRWAY’ range field. 5) To change the range setting, turn the small FMS Knob to display the range list. 6) Select the desired range using the small FMS Knob. 7) Press the ENT Key. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX 8) Press the FMS Knob to return to the Navigation Map Page. 161 SYSTEM OVERVIEW Flight Management The following range items are configurable on the airways menu: Airway Type Symbol FLIGHT INSTRUMENTS Low Altitude Airway (LOW ALT AIRWAY) Default Maximum Range (nm) Range (nm) 200 500 High Altitude Airway (HI ALT AIRWAY) 300 500 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: 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. AFCS 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Select the ‘Map’ group. 4) Press the ENT Key. ADDITIONAL FEATURES 5) Highlight the ‘TRACK VECTOR’ field. 6) Select ‘On’ or ‘Off’. Press the ENT Key to accept the selected option. The flashing cursor highlights the look ahead time field. Use the FMS Knob to select the desired time. Press the ENT Key. INDEX APPENDICES 7) Press the FMS Knob to return to the Navigation Map Page. 162 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Nav Range Ring On/Off FLIGHT INSTRUMENTS Wind Vector On/Off Track Vector - On/Off - Look Ahead Time EIS 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 FLIGHT MANAGEMENT Wind Vector The map displays a wind vector arrow in the upper right-hand portion of the screen. Wind vector information is displayed as a white arrow pointing in the direction in which the wind is moving for wind speeds greater than or equal to 1 kt. HAZARD AVOIDANCE Wind Direction Wind Speed Figure 5-26 Navigation Map - Wind Vector AFCS Note: The wind vector is not displayed until the aircraft is moving. It is not displayed on the Waypoint Information pages. ADDITIONAL FEATURES Displaying/removing the wind vector: 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Select the ‘Map’ group. APPENDICES 4) Press the ENT Key. 5) Highlight the ‘WIND VECTOR’ field. 6) Select ‘On’ or ‘Off’. 7) Press the FMS Knob to return to the Navigation Map Page. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 163 SYSTEM OVERVIEW Flight Management Nav Range Ring FLIGHT INSTRUMENTS 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). AUDIO PANEL & CNS EIS Range (radius) FLIGHT MANAGEMENT Nav Range Ring HAZARD AVOIDANCE Figure 5-27 Navigation Map - Nav Range Ring Note: The Nav Range Ring is not displayed on the Waypoint Information pages, Nearest pages, or Direct-to Window map. Displaying/removing the Nav Range Ring: 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 INDEX - System Setup Page. 164 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 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 Time to Reserve Fuel EIS AUDIO PANEL & CNS Range to Reserve Fuel FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Select the ‘Map’ group. 4) Press the ENT Key. 5) Highlight the ‘FUEL RNG (RSV)’ field. AFCS 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. ADDITIONAL FEATURES 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. APPENDICES 10) Press the FMS Knob to return to the Navigation Map Page. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 165 SYSTEM OVERVIEW Flight Management 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. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS Lateral Field of View Boundaries Figure 5-29 Navigation Map - Field of View Displaying/removing the field of view: HAZARD AVOIDANCE 1) Press the MENU Key with the Navigation Map Page displayed. The cursor flashes on the ‘Map Setup’ option. 2) Press the ENT Key. The Map Setup Menu is displayed. 3) Select the ‘Map’ group. 4) Press the ENT Key. AFCS 5) Highlight the ‘FIELD OF VIEW’ field. 6) Select ‘On’ or ‘Off’. INDEX APPENDICES ADDITIONAL FEATURES 7) Press the FMS Knob to return to the Navigation Map Page. 166 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Selected Altitude Intercept Arc The map can display the location along the current track where the aircraft will intercept the selected altitude. The location will be shown as a light blue arc when the aircraft is actually climbing or descending. FLIGHT INSTRUMENTS Range to Altitude Arc EIS AUDIO PANEL & CNS Figure 5-30 Navigation Map - Range to Altitude Arc Displaying/removing the selected altitude intercept arc: FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 4) Press the ENT Key. 5) Highlight the ‘SEL ALT ARC’ field. 6) Select ‘On’ or ‘Off’. 7) Press the FMS Knob to return to the Navigation Map Page. AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 167 SYSTEM OVERVIEW Flight Management Destination Airport Information The destination airport for which the information is displayed is determined as follows. FLIGHT INSTRUMENTS • The destination airport is the last airport in the active flight plan if: - No arrival or approach is loaded, or - An arrival waypoint is part of the active leg and no approach is loaded, or - The active leg is past the MAP • The destination airport is the airport prior to the procedure(s) in the active flight plan if: EIS - An arrival and/or approach is loaded and neither are active • The destination airport is the airport associated with the approach if: AUDIO PANEL & CNS - An arrival waypoint is part of the active leg and an approach is loaded, or - The approach is active • The destination airport is the Direct-to waypoint if: FLIGHT MANAGEMENT - The Direct-to waypoint is not in the active flight plan and is an airport If none of these conditions are met, then the destination airport is undefined and the destination information fields are shown as dashes. HAZARD AVOIDANCE Valid Destination Airport Airport Identifier Fuel Remaining at Airport AFCS Enroute Distance Estimated Time Enroute Bearing to Airport ADDITIONAL FEATURES Invalid Destination Airport INDEX APPENDICES Figure 5-31 Destination Airport Information 168 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 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 Audio Panel and CNS section for details on autotuning. - Waypoint Identifier - Type (symbol) - Facility Name - City FLIGHT MANAGEMENT City Entry Field Facility Entry Field AUDIO PANEL & CNS Identifier Entry Field 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 Perspective. As a waypoint identifier, facility name, or location is entered, The system’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. HAZARD AVOIDANCE Entered Waypoint on Map Map Area Showing Entered Waypoint AFCS Waypoint Location ADDITIONAL FEATURES Figure 5-32 Waypoint Information Window APPENDICES 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. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 169 SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS Identifier with Duplicates AUDIO PANEL & CNS EIS Duplicate Waypoints FLIGHT MANAGEMENT Duplicate Message Airports Figure 5-33 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. INDEX APPENDICES 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. This information is viewed on the Airport Information Page by pressing the INFO softkey until INFO-1 is displayed. 170 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Airport Information FLIGHT INSTRUMENTS - ID/Facility/City - Usage Type/Region - Lat/Long/Elev - Fuel Available - Time Zone (UTC Offset) Navigation Map Showing Selected Airport Runway Information - Designation - Length/Width/Surface - Lighting Available EIS COM/NAV Freq. Info. Airport/Runway Diagram AUDIO PANEL & CNS - Identification - Frequency - Availability - Additional Information FLIGHT MANAGEMENT Softkeys Figure 5-34 Airport Information Page The following descriptions and abbreviations are used on the Airport Information Page: HAZARD AVOIDANCE • Usage type: Public, Military, Private, or Heliport • Runway surface type: Hard, Turf, Sealed, Gravel, Dirt, Soft, Unknown, or Water • Runway lighting type: No Lights, Part Time, Full Time, Unknown, or PCL Freq (for pilot-controlled lighting) • COM Availability: TX (transmit only), RX (receive only), PT (part time), i (additional information available) AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 171 SYSTEM OVERVIEW Flight Management The AOPA directory information is viewed on the Airport Directory Page by pressing the INFO softkey until INFO-2 is displayed. The following are types of AOPA airport directory informantion shown (if available) on the Airport Directory Page: FLIGHT INSTRUMENTS • Airport: Identifier, Site Number, Name, City, State • Phones: Phone/Fax Numbers AUDIO PANEL & CNS EIS • Hours: Facility Hours, Light Hours, Tower Hours, Beacon Hours • Location: Sectional, Magnetic Variation • Frequencies: Type/Frequency FLIGHT MANAGEMENT • Transportation: Ground Transportation Type Available HAZARD AVOIDANCE • Approach: Approach Facility Name, Frequency, Frequency Parameter • Traffic Pattern Altitudes (TPA): Aircraft Class/Altitude • Weather: Service Type, Frequency, Phone Number • Flight Service Station (FSS): FSS Name, Phone Numbers • Runway: Headings, Length, Width, Obstructions, Surface • Obstructions: General Airport Obstructions • Special Operations at Airport • Instrument Approaches: Published Approach, Frequency • NAVAIDS: Type, Identifier, Frequency, Radial, Distance • Noise: Noise Abatement Procedures • Services Available: Category, Specific Service • Charts: Low Altitude Chart Number • FBO: Type, Frequencies, Services, Fees, Fuel, Credit Cards, Phone/Fax Numbers Airport Information • Notes: Airport Notes • Pilot Controlled Lighting: High/Med/Low Clicks/Second Airport Directory Information APPENDICES ADDITIONAL FEATURES AFCS - ID/Facility/City - Usage Type/Region Softkeys INDEX Figure 5-35 Airport Directory Page Example 172 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Selecting an airport for review by identifier, facility name, or location: 1) From the Airport Information Page, press the FMS Knob. 2) Use the FMS Knobs and enter an identifier, facility name, or location. FLIGHT INSTRUMENTS 3) Press the ENT Key. 4) Press the FMS Knob to remove the cursor. Selecting a runway: 1) With the Airport Information Page displayed, press the FMS Knob to activate the cursor. EIS 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. AUDIO PANEL & CNS 4) To remove the flashing cursor, press the FMS Knob. Viewing a destination airport: From the Airport Information Page press the MENU Key. Select ‘View Destination Airport’. The Destination Airport is displayed. FLIGHT MANAGEMENT The Airport Frequencies Box uses the descriptions and abbreviations listed in the following table: Navigation Frequencies ILS LOC HAZARD AVOIDANCE AFCS 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 ADDITIONAL FEATURES * May include Additional Information Table 5-5 Airport Frequency Abbreviations APPENDICES 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). Perspective provides a NRST Softkey on the PFD, which gives the pilot quick access to nearest airport information (very useful if an immediate landing is required). The Nearest Airports Window displays a list of up to 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. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 173 SYSTEM OVERVIEW Flight Management Bearing/Distance to Airport FLIGHT INSTRUMENTS Airport Identifier/ Type Approach Available Length of Longest Runway COM Freq. Info. - Identification - Frequency AUDIO PANEL & CNS EIS Additional Airports (within 200 nm) NRST Softkey Figure 5-36 Nearest Airports Window on PFD HAZARD AVOIDANCE FLIGHT MANAGEMENT Pressing the ENT Key displays the PFD Airport Information Window for the highlighted airport. Pressing the ENT Key again returns to the Nearest Airports Window with the cursor on the next airport in the list. Continued presses of the ENT Key sequences through the information pages for all airports in the Nearest Airports list. Airport Information - ID/Type/City - Facility Airport Information - Usage/Time/Elev - Region AFCS Airport Information ADDITIONAL FEATURES - Lat/Long APPENDICES Figure 5-37 Airport Information Window on PFD The Nearest Airports Page on the MFD is first in the group of NRST pages because of its potential use in the event of an in-flight emergency. In addition to displaying a map of the currently selected airport and surrounding area, the page displays nearest airport information in five boxes labeled ‘NEAREST AIRPORTS’, ‘INFORMATION’, ‘RUNWAYS’, ‘FREQUENCIES’, and ‘APPROACHES’. INDEX 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 three frequencies, and up to three approaches are visible at one time. If there are more than can be shown, each list can be scrolled. 174 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS Nearest Airports - ID/Type - Bearing/Distance Airport Information - Facility/City/Elevation EIS Runway Information Nearest Airport - Designation/Surface - Length/Width AUDIO PANEL & CNS COM/NAV Freq. Info. - Identification - Frequency Navigation Map Showing Nearest Airport Approaches Available Figure 5-38 Nearest Airport Page FLIGHT MANAGEMENT Window Selection Softkeys LD APR Softkey (only available if an approach is highlighted) HAZARD AVOIDANCE Viewing information for a nearest airport on the PFD: 1) Press the NRST Softkey to display the Nearest Airports Window. Press the FMS Knob to activate the cursor. 2) Highlight the airport identifier with the FMS Knob and press the ENT Key to display the Airport Information Window. 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.) ADDITIONAL FEATURES 4) Press the CLR Key or the NRST Softkey to close the PFD Nearest Airports Window. Viewing information for a nearest airport on the MFD: 1) Turn the large FMS Knob to select the NRST page group. APPENDICES 2) Turn the small FMS Knob to select the Nearest Airports Page (it is the first page of the group, so it may already be selected). If there are no Nearest Airports available, “NONE WITHIN 200 NM” is displayed. 3) 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. INDEX 4) Turn the FMS Knob to highlight the desired airport. (Pressing the ENT Key also moves to the next airport.) 5) Press the FMS Knob to remove the flashing cursor. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 175 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 5-39 System Setup Page - Nearest Airport Selection Criteria 176 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 5-40 Intersection Information Page AFCS Selecting 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 177 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 5-41 Nearest Intersections Page 178 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 5-42 NDB Information Page Note: Compass locator (LOM, LMM): a low power, low or medium frequency radio beacon installed in conjunction with the instrument landing system. When LOM is used, the locator is at the Outer Marker; when LMM is used, the locator is at the Middle Marker. AFCS Selecting 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 179 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 5-43 Nearest NDB Page 180 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 is displayed as VOR-DME. In addition to displaying a map of the currently selected VOR and surrounding area, the VOR Information Page displays VOR information in four boxes labeled ‘VOR’, ‘INFORMATION’, ‘FREQUENCY’, and ‘NEAREST AIRPORT’. 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 Nearest Airport Info Selected VOR - Identifier/Type (symbol) - Bearing/Distance to Airport HAZARD AVOIDANCE Figure 5-44 VOR Information Page AFCS The VOR classes used in the VOR information box are: LOW ALTITUDE, HIGH ALTITUDE, and TERMINAL. Selecting 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. 190-00820-06 Rev. A INDEX 3) Press the FMS Knob to remove the flashing cursor. Or: Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 181 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. 5) 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. FLIGHT MANAGEMENT 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 Navigation Map Showing Nearest VOR HAZARD AVOIDANCE - Bearing/Distance to VOR from aircraft position VOR Information AFCS - Facility Name/City - Class/Magnetic Variation - Lat/Long VOR Frequency ADDITIONAL FEATURES Nearest VOR INDEX APPENDICES Figure 5-45 Nearest VOR Page 182 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW User Waypoints FLIGHT INSTRUMENTS The system can create and store up to 1,000 user-defined waypoints. User waypoints can be created from any map page (except PFD Inset Map, AUX-Trip Planning Page, or Procedure Pages) by selecting a position on the map using the Joystick, or from the User Waypoint Information Page by referencing a bearing/distance from an existing waypoint, bearings from two existing waypoints, or entering a latitude/longitude. Once a waypoint has been created, it can be renamed, deleted, or moved. Temporary user waypoints are erased upon system power down. User Waypoint Info User Wpt Comment Navigation Map Showing Selected User Waypoint EIS - Identifier - Temporary/Normal - Waypoint Type AUDIO PANEL & CNS Reference Wpt/Info - Identifier/Rad/Dist or - Identifiers/Radials or - Region/Lat/Long Selected User Waypoint User Waypoint List FLIGHT MANAGEMENT - Identifier - Comment # User Wpts Used HAZARD AVOIDANCE Displayed if User Wpt was created on map page Softkeys Figure 5-46 User Waypoint Information Page AFCS Selecting a User Waypoint: 1) With the User Waypoint Information Page displayed, enter the name of the User Waypoint, or scroll to the desired waypoint in the User Waypoint List using the large FMS Knob. ADDITIONAL FEATURES 2) Press the ENT Key. 3) Press the FMS Knob to remove the flashing cursor. Or: APPENDICES 1) With the Nearest User Waypoints Page displayed, press the FMS Knob. 2) Press the ENT Key or turn either FMS Knob to select an identifier in the Nearest USR Box. 3) Press the FMS Knob to remove the flashing cursor. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 183 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 5-47 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. APPENDICES ADDITIONAL FEATURES AFCS 4) If desired, define the type and location of the waypoint in one of the following ways: a) Select “RAD/RAD” using the small FMS Knob, press the ENT Key, and enter the two reference waypoint identifiers and radials into the REFERENCE WAYPOINTS window using the FMS Knobs. Or: b) Select “RAD/DIS” using the small FMS Knob, press the ENT Key, and enter the reference waypoint identifier, the radial, and the distance into the REFERENCE WAYPOINTS window using the FMS Knobs. Or: c) Select “LAT/LON” using the small FMS Knob, press the ENT Key, and enter the latitude and longitude into the INFORMATION window using the FMS Knobs. 5) Press the ENT Key to accept the new waypoint. INDEX 6) If desired, change the storage method of the waypoint to “TEMPORARY” or “NORMAL” by moving the cursor to “TEMPORARY” and selecting the ENT Key to check or uncheck the box. 7) Press the FMS Knob to remove the flashing cursor. 184 Or: Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 1) Press the FMS Knob to activate the cursor. 2) Enter a user waypoint name (up to six characters). FLIGHT INSTRUMENTS 3) Press the ENT Key. The message ‘Are you sure you want to create the new User Waypoint AAAAAA?’ is displayed. 4) With ‘YES’ highlighted, press the ENT Key. 5) If desired, define the type and location of the waypoint in one of the following ways: a) Select “RAD/RAD” using the small FMS Knob, press the ENT Key, and enter the two reference waypoint identifiers and radials into the REFERENCE WAYPOINTS window using the FMS Knobs. Or: b) Select “RAD/DIS” using the small FMS Knob, press the ENT Key, and enter the reference waypoint identifier, the radial, and the distance into the REFERENCE WAYPOINTS window using the FMS Knobs. Or: c) Select “LAT/LON” using the small FMS Knob, press the ENT Key, and enter the latitude and longitude into the INFORMATION window using the FMS Knobs. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT 6) Press the ENT Key to accept the new waypoint. 7) If desired, change the storage method of the waypoint to “TEMPORARY” or “NORMAL” by moving the cursor to “TEMPORARY” and selecting the ENT Key to check or uncheck the box. 8) Press the FMS Knob to remove the flashing cursor. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Figure 5-48 User Waypoint Information Page Menu Creating user waypoints from map pages: APPENDICES 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. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 185 SYSTEM OVERVIEW Flight Management Note: If the pointer has highlighted a map database feature, one of three things happens upon pressing FLIGHT INSTRUMENTS the ENT Key: 1) information about the selected feature is displayed instead of initiating a new waypoint, 2) a menu pops up allowing a choice between ‘Review Airspaces’ or ‘Create User Waypoint’, or 3) a new waypoint is initiated with the default name being the selected map item. 3) Enter a user waypoint name (up to six characters). 4) Press the ENT Key to accept the selected name. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 5) If desired, define the type and location of the waypoint in one of the following ways: a) Select “RAD/RAD” using the small FMS Knob, press the ENT Key, and enter the two reference waypoint identifiers and radials into the REFERENCE WAYPOINTS window using the FMS Knobs. Or: b) Select “RAD/DIS” using the small FMS Knob, press the ENT Key, and enter the reference waypoint identifier, the radial, and the distance into the REFERENCE WAYPOINTS window using the FMS Knobs. Or: c) Select “LAT/LON” using the small FMS Knob, press the ENT Key, and enter the latitude and longitude into the INFORMATION window using the FMS Knobs. 6) Press the ENT Key to accept the new waypoint. 7) If desired, change the storage method of the waypoint to “TEMPORARY” or “NORMAL” by moving the cursor to “TEMPORARY” and selecting the ENT Key to check or uncheck the box. HAZARD AVOIDANCE 8) Press the FMS Knob to remove the flashing cursor. 9) Press the GO BACK Softkey to return to the map page. Editing User Waypoints AFCS Editing a user waypoint comment or location: 1) With the User Waypoint Information Page displayed, press the FMS Knob to activate the cursor. 2) Select a user waypoint in the User Waypoint List, if required, and press the ENT Key. ADDITIONAL FEATURES 3) Move the cursor to the desired field. 4) Turn the small FMS Knob to make any changes. 5) Press the ENT Key to accept the changes. APPENDICES 6) Press the FMS Knob to remove the flashing cursor. Renaming user waypoints: 1) Highlight a user waypoint in the User Waypoint List. Press the RENAME Softkey, or press the MENU Key and select ‘Rename User Waypoint’. INDEX 2) Enter a new name. 186 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 5) Press the FMS Knob to remove the flashing cursor. Changing the location of an existing waypoint to the aircraft present position: 1) Enter a waypoint name or select the waypoint in the User Waypoint List, then press the ENT Key. 2) Press the MENU Key. EIS 3) Select ‘Use Present Position’. 4) Press the ENT Key twice. The new waypoint’s location is saved. 5) Press the FMS Knob to remove the flashing cursor. AUDIO PANEL & CNS 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: FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE The default type of user waypoint (normal or temporary) can be changed using the user waypoint information page menu. Temporary user waypoints are automatically deleted upon the next power cycle. Changing the user waypoint storage duration default setting: 1) With the User Waypoint Information Page displayed, press the MENU Key. AFCS 2) Move the cursor to select ‘Waypoint Setup’, and press the ENT Key. 3) Select ‘NORMAL’ or ‘TEMPORARY’ as desired, and press the ENT Key. 4) Press the FMS Knob to remove the flashing cursor and return to the User Waypoint Information Page. ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 187 SYSTEM OVERVIEW Flight Management 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 Note: The option to ‘Delete All User Waypoints’ is not available while the aircraft is in flight. Deleting all user waypoints: 1) Highlight a User Waypoint in the User Waypoint List. HAZARD AVOIDANCE 2) Press the MENU Key. 3) Select ‘Delete All User Waypoints’. 4) Press the ENT Key twice to confirm the selection. INDEX APPENDICES ADDITIONAL FEATURES AFCS 5) Press the FMS Knob to remove the flashing cursor. 188 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 5.4 Airspaces FLIGHT INSTRUMENTS Perspective 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 Restricted Area AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Alert Area Class C Airspace AFCS ADDITIONAL FEATURES ADIZ Warning Area APPENDICES Figure 5-49 Airspaces 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 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. 189 SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS The Airspace Alerts Box allows the pilot to turn the controlled/special-use airspace message alerts on or off. This does not affect the alerts listed on the Nearest Airspaces Page or the airspace boundaries depicted on the Navigation Map Page. It simply turns on/off the warning provided when the aircraft is approaching or near an airspace. An altitude buffer is also provided which “expands” the vertical range above or below an airspace. For example, if the buffer is set at 500 feet, and the aircraft is more than 500 feet above/below an airspace, an alert message is not generated, but if the aircraft is less than 500 feet above/below an airspace and projected to enter it, the pilot is notified with an alert message. The default setting for the altitude buffer is 200 feet. EIS Changing the altitude buffer distance setting: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. AUDIO PANEL & CNS 3) Turn the large FMS Knob to highlight the altitude buffer field in the Airspace Alerts Box. 4) Use the FMS Knob to enter an altitude buffer value and press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor. FLIGHT MANAGEMENT Turning an airspace alert on or off: 1) Use the FMS Knob to select the AUX - System Setup Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. 3) Turn the large FMS Knob to highlight the desired field in the Airspace Alerts Box. HAZARD AVOIDANCE 4) Turn the small FMS Knob clockwise to turn the airspace alert ON or counterclockwise to turn the alert OFF. AFCS 5) Press the FMS Knob to remove the flashing cursor. Airspace Alerts Box APPENDICES ADDITIONAL FEATURES - Airspace Altitude Buffer - Alert On/Off (Default Settings Shown) INDEX DFLTS Softkey Figure 5-50 System Setup Page - Airspace Alerts 190 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 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 Airspace 1 AUDIO PANEL & CNS - Name - Proximity (Ahead, Inside, Ahead < 2nm, Within 2nm) - Time till Intercept (only if Ahead or Ahead < 2nm) 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 5-51 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 Airspaces Page. 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. APPENDICES 3) Select the desired airspace. 4) Press the FMS Knob to remove the flashing cursor. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 191 SYSTEM OVERVIEW Flight Management Pressing the PFD ALERTS Softkey displays the message window on the PFD. The following airspace alerts are displayed in the message window: EIS FLIGHT INSTRUMENTS Message INSIDE ARSPC – Inside airspace. ARSPC AHEAD – Airspace ahead – less than 10 minutes. ARSPC NEAR – Airspace near and ahead. ARSPC NEAR – Airspace near – less than 2 nm. Comments The aircraft is inside the airspace. Special use airspace is ahead of aircraft. The aircraft penetrates the airspace within 10 minutes. Special use airspace is near and ahead of the aircraft position. Special use airspace is within 2 nm of the aircraft position. INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS Table 5-6 PFD Airspace Alert Messages 192 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 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 system establishes a point-to-point course line from the present position to the selected direct-to destination. Course guidance is provided until the direct-to is replaced with a new direct-to or flight plan, or cancelled. 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. 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. AUDIO PANEL & CNS Direct-to Point Info VNV Constraints - Altitude at Arrival - Along Track Offset FLIGHT MANAGEMENT - Identifier/Symbol/Region - Facility Name - City Map of Selected Point HAZARD AVOIDANCE Location of Destination - Bearing/Distance AFCS Desired Course Figure 5-52 Direct-to Window - MFD ADDITIONAL FEATURES Direct-to Point Info VNV Constraints - Altitude at Arrival - Along Track Offset APPENDICES - Identifier/Symbol/City - Facility Name Direct-to Point Info - Bearing/Distance - Desired Course INDEX Activation Command Figure 5-53 Direct-to Window - PFD 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 193 SYSTEM OVERVIEW Flight Management 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. AUDIO PANEL & CNS 4) Press the ENT Key to activate the direct-to. Any waypoint contained in the active flight plan can be selected as a direct-to waypoint from the Direct-to Window, the Active Flight Plan Page, or the Active Flight Plan Window. Waypoint Submenu HAZARD AVOIDANCE FLIGHT MANAGEMENT - Flight Plan Waypoints - Nearest Airports - Recent Waypoints - User Waypoints - Airway Waypoints (only available when active leg is part of an airway) Figure 5-54 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?’. APPENDICES 5) Press the ENT Key again to activate the direct-to. Or: 1) Select the Active Flight Plan Page on the MFD, or the Active Flight Plan Window on the PFD. 2) Select the desired waypoint. INDEX 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. 194 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Any NRST, RECENT, USER, or AIRWAY waypoints can be selected as a direct-to destination in the Direct-to Window. Selecting a NRST, RECENT, USER, or AIRWAY waypoint as a direct-to destination: FLIGHT INSTRUMENTS 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 FPL waypoints (the FPL list is populated only when navigating a flight plan, and the AIRWAY list is available only when the active leg is part of an airway). 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.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. FLIGHT MANAGEMENT Selecting any waypoint as a direct-to destination: 1) Select the page or window containing the desired waypoint type and select the desired waypoint. 2) Press the Direct-to Key to display the Direct-to Window with the selected waypoint as the direct-to destination. HAZARD AVOIDANCE 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 and press the FMS Knob. 2) Select the desired airport (the nearest one is already selected). 3) Press the Direct-to Key. ADDITIONAL FEATURES 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. 2) Move the Joystick to place the pointer at the desired destination location. INDEX 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. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 195 SYSTEM OVERVIEW Flight Management 5) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 6) Press the ENT Key again to activate the direct-to. FLIGHT INSTRUMENTS Cancelling a Direct-to: 1) Press the Direct-to Key to display the Direct-to Window. 2) Press the MENU Key. EIS 3) With ‘Cancel Direct-To NAV’ highlighted, press the ENT Key. If a flight plan is still active, the system resumes navigating the flight plan along the closest leg. Page Menu HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS - Cancel Direct-To Navigation AFCS Figure 5-55 Direct-to Window - Cancelling Direct-to Navigation When navigating a direct-to, the system sets a direct great circle course to the selected destination. The course to a destination can also be manually selected using the course field (‘COURSE’) on the Direct-to Window. 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. APPENDICES 3) Enter the desired course. 4) Press the ENT Key. The cursor is now displayed on ‘ACTIVATE?’. 5) Press the ENT Key again to activate the direct-to. Reselecting the direct course from the current position: 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. 196 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 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: 1) Press the Direct-to Key to display the Direct-to Window. HAZARD AVOIDANCE 2) Press the MENU Key. 3) With ‘Clear Vertical Constraints’ highlighted, press the ENT Key. AFCS Page Menu - Clear Vertical Navigation Constraints ADDITIONAL FEATURES APPENDICES INDEX Figure 5-56 Direct-to Window - Clearing Vertical Constraints 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 197 SYSTEM OVERVIEW Flight Management 5.6 Flight Planning FLIGHT INSTRUMENTS Flight planning on Perspective 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. Perspective allows flight planning information to be entered from either the MFD or PFD. The flight plan is displayed on maps using different line widths, colors, and types, based on the type of leg and the segment of the flight plan currently being flown (departure, enroute, arrival, approach, or missed approach). Flight Plan Leg Type Symbol EIS Active non-heading Leg AUDIO PANEL & CNS Active heading Leg Non-heading Leg in the current flight segment FLIGHT MANAGEMENT Heading Leg not in the current flight segment Non-heading Leg not in the active flight segment HAZARD AVOIDANCE Turn Anticipation Arc Table 5-7 Flight Plan Leg Symbols ADDITIONAL FEATURES 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 system uses the waypoint information from the current database to define the waypoints. If the database is changed or updated, the system automatically updates the information if the procedure has not been modified. If an approach, departure, or arrival procedure is no longer available, the procedure is deleted from the affected stored flight plan(s), and an alert is displayed (see Miscellaneous Messages in Appendix A) advising that one or more stored flight plans need to be edited. 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. 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 reloads the sequence of waypoints between the entry and exit waypoints (the sequence may change when the database is updated). The update of an airway can fail during this process. If that happens, the airway waypoints are changed to regular (non-airway) flight plan waypoints, and an alert is displayed (see Miscellaneous Messages in Appendix A). 198 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 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) • Flight Plan Catalog Page on the MFD (create/modify a stored flight plan) AUDIO PANEL & CNS Active FPL Waypoint List Active Flight Plan Leg FLIGHT MANAGEMENT - Comment - Procedure Header - Waypoint Identifier - Airway Identifier - Desired Track to Waypoint - Distance to Waypoint - Waypoint Altitude Constraint HAZARD AVOIDANCE Vertical Navigation Profile - Active Vertical WPT Alt/ID - Vertical Speed Target - Flight Path Angle - Vertical Speed Target - Time to Top of Descent - Vertical Deviation Turn Anticipation Arc Non-Active, Flight Plan Leg Figure 5-57 Active Flight Plan Page AFCS Selected Waypoint Weather - Textual METAR - Reporting Station Location (see the Hazard Avoidance Section for details on METARS) ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 199 SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS Active Flight Plan Comment Active Flight Plan Leg Active Flight Plan Waypoint List EIS - Waypoint ID - Desired Track to Waypoint - Distance to Waypoint - Airway Identifier AUDIO PANEL & CNS Figure 5-58 Active Flight Plan Window on PFD Catalog Contents FLIGHT MANAGEMENT - # Used - # Empty 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 ADDITIONAL FEATURES Figure 5-59 Flight Plan Catalog Page APPENDICES 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 Perspective 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). Creating an active flight plan with the FMS Knob: 1) Press the FPL Key. INDEX 2) Press the FMS Knob to activate the cursor (only on MFD). 200 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 3) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway waypoints). FLIGHT INSTRUMENTS 4) Enter the identifier, facility, or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key. The active flight plan is modified as each waypoint is entered. 5) Repeat step numbers 3 and 4 to enter each additional flight plan waypoint. 6) When all waypoints have been entered, press the FMS Knob to remove the cursor. EIS Creating an active flight plan with the Quick Select Box: 1) Press the FPL Key. AUDIO PANEL & CNS 2) Enter the identifier, facility, or city name of the departure waypoint using the alphanumeric keys on the PFD/MFD Control Unit and press the ENT Key. The active flight plan is modified as each waypoint is entered. 3) Repeat step number 2 to enter each additional flight plan waypoint. Creating a stored flight plan with the FMS Knob: FLIGHT MANAGEMENT 1) Press the FPL Key. 2) Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page. 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. HAZARD AVOIDANCE 4) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway waypoints). AFCS 5) Enter the identifier, facility, or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key. 6) Repeat step numbers 4 and 5 to enter each additional flight plan waypoint. ADDITIONAL FEATURES 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. Flight plans can be imported from an SD Card or exported to an SD Card from the Stored Flight Plan Page. Importing a Flight Plan from an SD Card APPENDICES 1) Insert the SD card containing the flight plan in the top card slot on the MFD. 2) Press the FPL Key on the Control Unit to display the Active Flight Plan Page on the MFD. 3) Turn the small FMS Knob to select the Flight Plan Catalog Page. 4) Press the FMS Knob to activate the cursor. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX 5) Turn either FMS Knob to highlight an empty or existing flight plan. 201 SYSTEM OVERVIEW Flight Management 6) Press the IMPORT Softkey; or press the MENU Key, select “Import Flight Plan”, and press the ENT Key. If an empty slot is selected, a list of the available flight plans on the SD card will be displayed. FLIGHT INSTRUMENTS Or: If an existing flight plan is selected, an “Overwrite existing flight plan? OK or CANCEL” prompt is displayed. Press the ENT Key to choose to overwrite the selected flight plan and see the list of available flight plans on the SD card. If overwriting the existing flight plan is not desired, select “CANCEL” using the FMS Knob, press the ENT Key, select another flight plan slot, and press the IMPORT Softkey again. 7) Turn the small FMS Knob to highlight the desired flight plan for importing. EIS 8) Press the ENT Key to initiate the import. 9) Press the ENT Key again to confirm the import. AUDIO PANEL & CNS Note: If the imported flight plan contains a waypoint with a name that duplicates the name of a waypoint ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT already stored on the system, the system compares the coordinates of the imported waypoint with those of the existing waypoint. If the coordinates are different, the imported waypoint is automatically renamed by adding characters to the end of the name. APPENDICES Import/Export Softkeys List of Flight Plans to Import & Details for the Selected File Import Successful INDEX Figure 5-60 Flight Plan Import 202 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Exporting a Flight Plan to an SD Card 1) Insert the SD card into the top card slot on the MFD. 2) Press the FPL Key on the Control Unit to display the Active Flight Plan Page on the MFD. FLIGHT INSTRUMENTS 3) Turn the small FMS Knob to select the Flight Plan Catalog Page. 4) Press the FMS Knob to activate the cursor. 5) Turn the large FMS Knob to highlight the flight plan to be exported. 6) Press the EXPORT Softkey; or press the MENU Key, select “Export Flight Plan”. EIS 7) If desired, change the name for the exported file by turning the large FMS Knob to the left to highlight the name, then use the small and large FMS knobs to enter the new name, and press the ENT Key. 8) Press the ENT Key to initiate the export. AUDIO PANEL & CNS 9) Press the ENT Key to confirm the export. Note: The exported flight plan will not contain any procedures or airways. FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Stored Flight Plan to be Exported & Exported Flight Plan Name Export Successful APPENDICES Import/Export Softkeys Figure 5-61 Flight Plan Export INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 203 SYSTEM OVERVIEW Flight Management 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 FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS - Memory Slot - Comment - Procedure Identifier - Waypoint Identifier - Airway Identifier - Desired Track to Waypoint - Distance to Waypoint - Waypoint Altitude Constraint HAZARD AVOIDANCE Softkeys INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 5-62 Stored Flight Plan Page 204 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW FLIGHT INSTRUMENTS Flight Plan Full Message EIS AUDIO PANEL & CNS Figure 5-63 Active Flight Plan Page - FPL Full Adding a waypoint to a stored flight plan: 1) On the Flight Plan Catalog Page, press the FMS Knob to activate the cursor. FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 4) Select the point in the flight plan to add the new waypoint. The new waypoint is placed directly in front of the highlighted waypoint. 5) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway waypoints). AFCS 6) Enter the identifier, facility, or city name of the waypoint or select a waypoint from the submenu of waypoints and press the ENT Key. The new waypoint now exists in the flight plan. ADDITIONAL FEATURES Note: If the identifier entered in the Waypoint Information Window has duplicates, a Duplicate Waypoint Window is displayed. Use the FMS Knob to select the correct waypoint. APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 205 AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Flight Management Figure 5-64 Duplicate Waypoints Window Adding a waypoint to the active flight plan using the FMS Knob: 1) Press the FPL Key. FLIGHT MANAGEMENT 2) Press the FMS Knob to activate the cursor (not required on the PFD). 3) Select the point in the flight plan before which to add the new waypoint. The new waypoint is placed directly in front of the highlighted waypoint. HAZARD AVOIDANCE 4) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway waypoints). 5) Enter the identifier, facility, or city name of the waypoint or select a waypoint from the submenu of waypoints and press the ENT Key. The active flight plan is modified as each waypoint is entered. AFCS Adding a waypoint to the active flight plan using the Quick Select Box: 1) Press the FPL Key. ADDITIONAL FEATURES 2) Use the Joystick to position the Quick Select Box and the associated Insertion Point Indicator at the location to insert the waypoint. 3) Enter the identifier, facility, or city name of the waypoint using the alphanumeric keys on the PFD/MFD Control Unit and press the ENT Key. The active flight plan is modified as each waypoint is entered. APPENDICES 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. INDEX 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. 206 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Adding Airways to a Flight Plan FLIGHT INSTRUMENTS 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. Perspective also anticipates the desired airway and exit point based on loaded flight plan waypoints. Airway Entry Waypoint EIS Selected Airway Airways Available at TOP AUDIO PANEL & CNS Airway Waypoint Sequence Preview of Selected Airway FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 5-65 Select Airway Page - Selecting Airway Adding an airway to a flight plan using the FMS Knob: AFCS 1) Press the FPL Key. 2) Press the FMS Knob to activate the cursor (not required on the PFD). ADDITIONAL FEATURES 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. APPENDICES 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). 5) Turn the FMS Knob to select the desired airway from the list, and press the ENT Key. Low altitude airways are shown first in the list, followed by “all” altitude airways, and then high altitude airways. 6) Turn the FMS Knob to select the desired airway exit point from the list, and press the ENT Key. ‘LOAD?’ is highlighted. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX 7) Press the ENT Key. The system returns to editing the flight plan with the new airway inserted. 207 SYSTEM OVERVIEW Flight Management Adding an airway to a flight plan using the Quick Select Box: 1) Press the FPL Key. FLIGHT INSTRUMENTS 2) Use the Joystick to place the QuickSelect Box on 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. 3) Press the MENU Key and select “Load Airway”. The Select Airway Page is displayed. 4) 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. EIS 5) Turn the FMS Knob to select the desired airway exit point from the list, and press the ENT Key. ‘LOAD?’ is highlighted. AUDIO PANEL & CNS 6) Press the ENT Key. The system returns to editing the flight plan with the new airway inserted. Airway Entry Waypoint Selected Airway Selected Exit Point FLIGHT MANAGEMENT Preview of Selected Airway Selected Airway Exit Point AFCS HAZARD AVOIDANCE Airway Exit Points Available INDEX APPENDICES ADDITIONAL FEATURES Figure 5-66 Select Airway Page - Selecting Exit Point 208 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW FLIGHT INSTRUMENTS Inserted Airway Header - Airway Identifier: [airway identifier].[exit waypoint identifier] (e.g., V4.SLN) EIS AUDIO PANEL & CNS Figure 5-67 Active Flight Plan Page - Airway Inserted FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 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. AFCS In the US, airways that are “one-way” for specified hours of operation are not uncommon. These airways are always bidirectional in the system database. ADDITIONAL FEATURES 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. APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 209 SYSTEM OVERVIEW Flight Management Adding Procedures to a Stored Flight Plan FLIGHT INSTRUMENTS Perspective 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 5-68 Stored Flight Plan Page 210 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 5-69 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 runway served by the selected departure, if required. Press the ENT Key. 6) Select a transition for the selected departure. Press the ENT Key. APPENDICES 7) Press the ENT Key to load the selected departure procedure. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 211 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 5-70 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 5-71 Stored Flight Plan Page - Departure Inserted 212 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 5-72 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 213 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 5-73 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 5-74 Stored Flight Plan Page - Arrival Inserted 214 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 BARO Minimum Preview of Selected Approach Approach Waypoint Sequence FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 5-75 Approach Loading Page - Selecting the Approach Loading an approach procedure into a stored flight plan: 1) Select a stored flight plan from the Flight Plan Catalog Page. 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. APPENDICES 6) Press the ENT Key to skip setting BARO minimums; or rotate small FMS Knob to select ‘BARO’, and press the ENT Key to enter the minimum altitude using the small FMS Knob or the FMS Control Unit keyboard. Press the ENT Key. 7) Press the ENT Key to load the selected approach procedure. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 215 SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS Destination Airport Selected Approach Selected Transition Transitions Available with Selected Approach AUDIO PANEL & CNS EIS Preview of Selected Approach Approach Waypoint Sequence Load Approach? HAZARD AVOIDANCE FLIGHT MANAGEMENT Figure 5-76 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 5-77 Stored Flight Plan Page - Approach Inserted 216 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Flight Plan Storage FLIGHT INSTRUMENTS Perspective can store up to 99 flight plans, numbered 1 through 99. The active flight plan is erased when the system is powered off or when another flight plan is activated. Details about each stored flight plan can be viewed on the Flight Plan Catalog Page and on the Stored Flight Plan Page. Viewing information about a stored flight plan: 1) Press the FPL Key on the MFD to display the Active Flight Plan Page. 2) Turn the small FMS Knob clockwise 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 5-78 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. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 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. 217 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, erases the active flight plan, and replaces it with the flight plan being activated (the stored flight plan is not changed). FLIGHT MANAGEMENT Activating a stored flight plan on the MFD: 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan. HAZARD AVOIDANCE 3) Press the ACTIVE Softkey; or press the ENT Key twice; or press the MENU Key, highlight ‘Activate Flight Plan’, and press the ENT Key. The ‘Activate Stored Flight Plan?’ window is displayed. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. Inverting and activating a stored flight plan on the MFD: AFCS 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. ADDITIONAL FEATURES 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. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. APPENDICES Copy a Flight Plan Perspective 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. INDEX Copying a stored flight plan on the MFD: 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan. 218 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 system 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 Note: The option to delete all stored flight plans is not available while the aircraft is in flight. Deleting all stored flight plans: 1) Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page. HAZARD AVOIDANCE 2) Press the MENU Key. 3) Highlight ‘Delete All’ and press the ENT Key. A ‘Delete all flight plans?’ confirmation window is displayed. 4) With ‘OK’ highlighted, press the ENT Key to delete all flight plans. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. AFCS Flight Plan Editing The active flight plan or any stored flight plan can be edited. The edits made to the active flight plan affect navigation as soon as they are entered. ADDITIONAL FEATURES Deleting the Active Flight Plan Perspective allows deleting an active flight plan. Deleting the active flight plan suspends navigation by the system. APPENDICES Deleting the active flight plan: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, highlight ‘Delete Flight Plan’, and press the ENT Key. The ‘Delete all waypoints in flight plan?’ window is displayed. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX 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. 219 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. Or: Use the Joystick to place the Quick Select Box on the waypoint to be deleted (MFD only). AUDIO PANEL & CNS 3) Press the CLR Key. The ‘Remove XXXXX?’ 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. FLIGHT MANAGEMENT 5) Press the FMS Knob to remove the flashing cursor, if required. Deleting an entire airway from the active flight plan: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). HAZARD AVOIDANCE 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. Or: Use the Joystick to place the Quick Select Box on the white header of the airway to be deleted (MFD only). 3) Press the CLR Key. The ‘Remove?’ window is displayed. AFCS 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, if required. ADDITIONAL FEATURES Deleting an entire procedure from the active flight plan: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). APPENDICES 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. Or: Use the Joystick to place the Quick Select Box on the white header of the procedure to be deleted (MFD only). 3) Press the CLR 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. 5) Press the FMS Knob to remove the flashing cursor, if required. 220 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 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 ’. FLIGHT INSTRUMENTS 3) Press the ENT Key. The ‘Remove from flight plan?’ window is displayed. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. Deleting an individual waypoint from a stored flight plan: EIS 1) Press the FPL Key to display the Active Flight Plan Page. 2) Turn the small FMS Knob clockwise 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. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 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. 8) Press the FMS Knob to remove the flashing cursor. HAZARD AVOIDANCE Deleting an entire airway from a stored flight plan: 1) Press the FPL Key to display the Active Flight Plan Page. 2) Turn the small FMS Knob clockwise 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. AFCS 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 white header of the airway to be deleted. ADDITIONAL FEATURES 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. APPENDICES Deleting an entire procedure from a stored flight plan: 1) Press the FPL Key to display the Active Flight Plan Page. 2) Turn the small FMS Knob clockwise 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. INDEX 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. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 221 SYSTEM OVERVIEW Flight Management 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. FLIGHT INSTRUMENTS 7) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. 8) Press the FMS Knob to remove the flashing cursor. Or: 1) Press the FPL Key to display the Active Flight Plan Page. EIS 2) Turn the small FMS Knob clockwise 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. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 7) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. 8) Press the FMS Knob to remove the flashing cursor. Changing Flight Plan Comments (Names) HAZARD AVOIDANCE The comment field (or name) of each flight plan can be changed to something that is useful for identification and sorting. Changing the active flight plan comment: 1) Press the FPL Key to display the Active Flight Plan Page. AFCS 2) Press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the comment field. 3) Use the FMS Knobs to edit the comment. 4) Press the ENT Key to accept the changes. ADDITIONAL FEATURES 5) Press the FMS Knob to remove the flashing cursor. Or: 1) Press the FPL Key to display the Active Flight Plan Page. APPENDICES 2) Use the Joystick to place the Quick Select Box on the comment field. 3) Use the alphanumeric keys on the PFD/MFD Control Unit to edit the comment. 4) Press the ENT Key to accept the changes. Changing a stored flight plan comment: INDEX 1) Press the FPL Key to display the Active Flight Plan Page. 2) Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page. 222 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 5) Turn the large FMS Knob to highlight the comment field. 6) Use the FMS Knobs to edit the comment. 7) Press the ENT Key to accept the changes. 8) Press the FMS Knob to remove the flashing cursor. EIS Along Track Offsets AUDIO PANEL & CNS A waypoint having an “along track offset” distance from an existing waypoint can be entered into a flight plan. Along track offset waypoints lie along the path of the existing flight plan, and can be used to make the system reach a specified altitude before or after reaching the specified flight plan waypoint. Offset distances can be entered from 1 to 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 MANAGEMENT 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. HAZARD AVOIDANCE 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. AFCS ADDITIONAL FEATURES Along Track Offset Waypoint and Distance from Flight Plan Waypoint Along Track Offset Waypoint and Distance APPENDICES INDEX Figure 5-79 Along Track Offset 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 223 SYSTEM OVERVIEW Flight Management 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). FLIGHT INSTRUMENTS 2) Press the FMS Knob to activate the cursor (not required on the PFD) and turn the large FMS Knob to highlight the waypoint for the along track offset. 3) 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). EIS 5) Press the ENT Key to create the offset waypoint. INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS 6) Press the FMS Knob to remove the flashing cursor. 224 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 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. Note: Vertical navigation is unavailable while the Parallel Track feature is active. EIS AUDIO PANEL & CNS Active Flight Plan prior to Parallel Track Selecting Parallel Track FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 5-80 Active Flight Plan Window - Selecting Parallel Track Activating parallel track: AFCS 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, highlight ‘Parallel Track’, and press the ENT Key. The Parallel Track Window is displayed with the direction field highlighted. ADDITIONAL FEATURES 3) Turn the small FMS Knob to select ‘Left’ or ‘Right’ and press the ENT Key. The ‘DISTANCE’ field is highlighted. 4) Turn the small FMS Knob to enter a distance from 1-99 nm and press the ENT Key. ‘ACTIVATE PARALLEL TRACK’ is highlighted. APPENDICES 5) Press the ENT Key to activate parallel track. Press the FMS Knob or the CLR Key to cancel the parallel track activation. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 225 SYSTEM OVERVIEW Flight Management Offset Direction Offset Distance AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Activation Prompt HAZARD AVOIDANCE FLIGHT MANAGEMENT Figure 5-81 Parallel Track Window Parallel Track Waypoints - TIFTO-p - TOP-p - SLN-p - LAA-p Activating Parallel Track affects the entire active flight segment (e.g., enroute) AFCS Parallel Track ADDITIONAL FEATURES Original Track INDEX APPENDICES Figure 5-82 Parallel Track Active 226 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 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. EIS Subdued Prompt (Unavailable) AUDIO PANEL & CNS Unavailable Status Invalid Geometry Approach Active FLIGHT MANAGEMENT Figure 5-83 Parallel Track Unavailable HAZARD AVOIDANCE 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. AFCS Offset Direction & Distance Subdued (Unavailable) Cancel Prompt ADDITIONAL FEATURES Active Status APPENDICES Figure 5-84 Cancelling Parallel Track Cancelling parallel track: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). INDEX 2) Press the MENU Key, highlight ‘Parallel Track’, and press the ENT Key. The Parallel Track Window is displayed with ‘CANCEL PARALLEL TRACK?’ highlighted. 3) Press the ENT Key. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 227 SYSTEM OVERVIEW Activating a Flight Plan Leg FLIGHT INSTRUMENTS Flight Management Activating a flight plan leg: Perspective allows selection of a highlighted leg as the “active leg” (the flight plan leg which is currently used for navigation guidance). 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 destination waypoint for the desired leg. Or: Use the Joystick to place the Quick Select Box on the destination waypoint for the desired leg. AUDIO PANEL & CNS 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. HAZARD AVOIDANCE FLIGHT MANAGEMENT 5) Press the FMS Knob to remove the flashing cursor, if required. Current Active Leg ADDITIONAL FEATURES AFCS Selected Destination Waypoint Activate Leg Softkey INDEX APPENDICES Figure 5-85 Active Flight Plan Page - Selecting the Leg Destination Waypoint 228 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW FLIGHT INSTRUMENTS New Active Flight Plan Leg EIS AUDIO PANEL & CNS Confirmation Window Figure 5-86 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 and turn the small FMS Knob to display the Flight Plan Catalog Page. 2) Press the FMS Knob to activate the cursor, and turn the FMS Knob to highlight the desired flight plan. 3) 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. APPENDICES 4) With ‘OK’ highlighted, press the ENT Key. To cancel the request, press the CLR Key, or highlight ‘CANCEL’ and press the ENT Key. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 229 SYSTEM OVERVIEW Flight Management 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. AUDIO PANEL & CNS 3) Press the CUM Softkey to view cumulative waypoint distance, or press the LEG-LEG Softkey to view leg-to-leg waypoint distance. 4) Press the BACK Softkey to return to the top level active flight plan softkeys. Active Flight Plan Cumulative Distance AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT Active Flight Plan Leg to Leg Distance ADDITIONAL FEATURES WIDE Softkey, NARROW Softkey, LEG-LEG Softkey, CUM Softkey Figure 5-87 Active Flight Plan - Leg to Leg vs. Cumulative Distance APPENDICES Switching between wide and narrow view: 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. INDEX 4) Press the BACK Softkey to return to the top level active flight plan softkeys. 230 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Active Flight Plan Narrow View Active Flight Plan Wide View FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS WIDE Softkey, NARROW Softkey, LEG-LEG Softkey, CUM Softkey FLIGHT MANAGEMENT Figure 5-88 Active Flight Plan - Wide vs. Narrow View Collapsing Airways HAZARD AVOIDANCE Perspective allows airways on the active flight plan to be collapsed or expanded from the Active Flight Plan Page/Window. When airways have been collapsed, it is indicated on the airway heading. When airways are collapsed, leg-to-leg computed values such as DIS or ETE shown for the exit waypoint reflect the total of all the legs on the airway that have been hidden in the collapsed display. The DTK value is inhibited because it is not usable in this context. AFCS The Active Flight Plan Page always keeps the following three waypoints visible: “From” waypoint, “To” waypoint, and “Next” waypoint. To prevent one or more of these waypoints from being hidden in a collapsed airway segment, the airway segment that contains either the “To” or the “Next” waypoint is automatically expanded. When an airway is loaded, airways are automatically expanded to facilitate flight plan review. ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 231 SYSTEM OVERVIEW Flight Management Q3.FEPOT Airway EIS FLIGHT INSTRUMENTS Collapsed View Expanded View AUDIO PANEL & CNS Figure 5-89 Expanded/Collapsed Airways 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. INDEX APPENDICES ADDITIONAL FEATURES 3) Enter the identifier of the reference waypoint and press the ENT Key. The system displays the bearing (BRG) and distance (DIS) to the closest point along the flight plan to the selected reference waypoint and creates a user waypoint at this location. The name for the new user waypoint is derived from the identifier of the reference waypoint. 232 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 5.7 Vertical Navigation FLIGHT INSTRUMENTS Note: Perspective 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. Current Vertical Navigation Profile EIS The Perspective 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 Enabled (valid data) AUDIO PANEL & CNS Disabled (fields dashed) FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ENBL VNV Softkey CNCL VNV Softkey Figure 5-90 Enabling/Disabling Vertical Navigation ADDITIONAL FEATURES 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: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. INDEX 2) Press the CNCL VNV Softkey; or press the MENU Key, highlight ‘Cancel VNV’, and press the ENT Key. Vertical navigation is disabled. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 233 SYSTEM OVERVIEW Flight Management 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 EIS Perspective allows a vertical navigation direct-to to any waypoint in the active flight plan with an altitude constraint “designated” for vertical guidance. Pressing 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 Current Vertical Navigation Profile After VNV Direct-to AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT Prior to VNV Direct-to VNV Direct-To Softkey VNV PROF Softkey ADDITIONAL FEATURES Figure 5-91 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. INDEX 2) Press the FMS Knob to activate the cursor and turn the FMS Knob to highlight the desired waypoint. Or: Use the Joystick to place the Quick Select Box on 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. 234 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 3) Select the VNV Direct-To Softkey; or press the MENU Key, highlight ‘VNV Direct-To’, and press the ENT Key. An ‘Activate vertical Direct-to to: NNNNNFT at XXXXXX?’ confirmation window is displayed. 4) Press the ENT Key. Vertical guidance begins to the altitude constraint for the selected waypoint. FLIGHT INSTRUMENTS 5) Press the FMS Knob to remove the flashing cursor. The vertical navigation profile can be modified by directly entering a vertical speed target (VS TGT) and/or flight path angle (FPA) in the CURRENT VNV PROFILE box. Modifying the VS TGT and FPA using the FMS Knob: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. EIS 2) Press 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. AUDIO PANEL & CNS 3) Turn the FMS Knobs as needed to edit the values. 4) Press the FMS Knob to remove the flashing cursor. Modifying the VS TGT and FPA using the Quick Select Box: FLIGHT MANAGEMENT 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Use the Joystick to place the Quick Select Box on VS TGT or FPA. 3) Enter the values using the alphanumeric keys on the PFD/MFD Control Unit and press the ENT Key. Altitude Constraints HAZARD AVOIDANCE Perspective 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. AFCS Displayed Text Examples Cross AT or ABOVE 5,000 ft ADDITIONAL FEATURES Large White Text Large Light Blue Text Cross AT 2,300 ft Cross AT or BELOW 3,000 ft APPENDICES Small Light Blue Text Small Light Blue Subdued Text Altitude Constraint Examples INDEX Small White Text with Altitude Restriction Bar Figure 5-92 Waypoint Altitude Constraints 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 235 SYSTEM OVERVIEW Flight Management AUDIO PANEL & CNS Light Blue Text Light Blue Subdued Text Large Altitude calculated by the system Text estimating the altitude of the aircraft as it passes over the navigation point. This altitude is provided as a reference and is not designated to be used in determining vertical speed and deviation guidance. Altitude has been entered manually. Altitude is designated for use in giving vertical speed and deviation guidance. Altitude does not match the published altitude in navigation database or no published altitude exists. The system cannot use this altitude in determining vertical speed and deviation guidance because of an invalid constraint condition. Small Text Altitude is designated for use in giving vertical speed and deviation guidance. Altitude has been retrieved from the navigation database or has been entered manually and matches a published altitude in the navigation database. The system cannot use this altitude in determining vertical speed and deviation guidance because of an invalid constraint condition. Altitude is not designated to be used in determining vertical speed and deviation guidance. Altitude has been retrieved from the navigation database and is provided as a reference. EIS FLIGHT INSTRUMENTS White Text 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 using the FMS Knob: 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 waypoint altitude to be used for vertical guidance using the Quick Select Box: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Use the Joystick to place the Quick Select Box on the desired waypoint altitude. APPENDICES 3) Use the alphanumeric keys on the PFD/MFD Control Unit to enter the same altitude. 4) Press the ENT Key. The altitude is now shown in blue, indicating it is usable for vertical guidance. Designating a procedure waypoint altitude to be used for vertical guidance: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. INDEX 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude. 236 Or: Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Use the Joystick to place the Quick Select Box on the desired waypoint altitude (MFD only). 3) Press the ENT Key. The altitude is now shown in blue, indicating it is usable for vertical guidance. FLIGHT INSTRUMENTS Altitude constraints are displayed and entered in feet mean sea level (MSL) values to the nearest hundred. An altitude constraint in feet above ground level (AGL) format is supported for airports. When a database altitude restriction is displayed, the system allows entry of a different altitude when creating a waypoint, effectively overriding the database restriction (only before the FAF). When a database altitude restriction of type “AT or ABOVE” or “AT or BELOW” is activated, the system uses the “AT” portion of the restriction to define the vertical profile. An altitude constraint is invalid if: EIS • Meeting the constraint requires the aircraft to climb • Meeting the constraint requires the maximum flight path angle or maximum vertical speed to be exceeded AUDIO PANEL & CNS • The altitude constraint results in a TOD behind the aircraft present position • The constraint is within a leg type for which altitude constraints are not supported • The altitude constraint is added to the FAF of an approach that provides vertical guidance (i.e., ILS or GPS WAAS approach) FLIGHT MANAGEMENT • The altitude constraint is added to a waypoint past the FAF. Entering/modifiying an altitude constraint using the FMS Knob: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. HAZARD AVOIDANCE 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. 3) Enter an altitude constraint value using the FMS Knobs. To enter altitudes as a flight level, turn the small FMS Knob counter-clockwise past zero or clockwise past 9 on the first character, and the system automatically changes to show units of Flight Level. Turn the large FMS Knob clockwise to highlight the first zero and enter the three digit flight level. AFCS 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. Entering/modifiying an altitude constraint using the Quick Select Box: ADDITIONAL FEATURES 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. 2) Use the Joystick to place the Quick Select Box on the desired waypoint altitude constraint. APPENDICES 3) Enter an altitude constraint value using the alphanumeric keys on the PFD/MFD Control Unit. To enter altitudes as a flight level, enter F as the first character. 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. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX Altitude constraints can be modified or deleted after having been added to the flight plan. In the event an altitude constraint is deleted and the navigation database contains an altitude restriction for the lateral waypoint, the system displays the altitude restriction from the database provided no predicted altitude can be provided. The system also provides a way to reinstate a published altitude constraint that has been edited. 237 SYSTEM OVERVIEW Flight Management Deleting an altitude constraint provided by the navigation database: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. FLIGHT INSTRUMENTS 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. Or: Use the Joystick to place the Quick Select Box on the desired waypoint altitude constraint (MFD only). 3) Press the CLR Key. A ‘Remove VNV altitude constraint?’ confirmation window is displayed. 4) Select ‘OK’ and press the ENT Key. EIS Deleting an altitude constraint that has been manually entered: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. AUDIO PANEL & CNS 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. Or: Use the Joystick to place the Quick Select Box on the desired waypoint altitude constraint (MFD only). FLIGHT MANAGEMENT 3) Press the CLR Key. A ‘Remove or Revert to published VNV altitude of nnnnnFT?’ confirmation window is displayed. 4) Select ‘REMOVE’ and press the ENT Key. The manually entered altitude is deleted (it is replaced by a system calculated altitude, if available). HAZARD AVOIDANCE 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. AFCS 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. Or: Use the Joystick to place the Quick Select Box on the desired waypoint altitude constraint (MFD only). 3) Press the CLR Key. A ‘Remove or Revert to published VNV altitude of nnnnnFT?’ confirmation window is displayed. ADDITIONAL FEATURES 4) Select ‘REVERT’ and press the ENT Key. The altitude is changed to the navigation database value. 5) Press the FMS Knob to remove the flashing cursor. Modifying a system calculated altitude constraint: 1) Press the FPL Key to display the Active Flight Plan Page on the MFD. APPENDICES 2) Press the FMS Knob, and turn to highlight the desired waypoint altitude constraint. Or: Use the Joystick to place the Quick Select Box on the desired waypoint altitude constraint (MFD only). INDEX 3) Press the CLR Key. An ‘Edit or Revert to published VNV altitude of nnnnnFT?’ confirmation window is displayed. 4) Select ‘EDIT’ and press the ENT Key. 5) Edit the value using the FMS Knobs, and press the ENT Key. 6) Press the FMS Knob to remove the flashing cursor. 238 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 5.8 Procedures FLIGHT INSTRUMENTS Perspective 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. 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. AUDIO PANEL & CNS 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. Loading a Departure into the Active Flight Plan HAZARD AVOIDANCE Loading a departure into the active flight plan using the PROC Key: 1) Press the PROC Key. The Procedures Window is displayed. 2) Highlight ‘SELECT DEPARTURE’. 3) Press the ENT Key. The Departure Loading Page is displayed. AFCS 4) Use the FMS Knob to select an airport and press the ENT Key. 5) Select a departure from the list and press the ENT Key. ADDITIONAL FEATURES 6) Select a runway (if required) and press the ENT Key. 7) Select a transition (if required) and press the ENT Key. ‘LOAD?’ is highlighted. 8) Press the ENT Key to load the departure procedure. APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 239 SYSTEM OVERVIEW Flight Management Available Procedure Actions AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Departure Airport Loaded Procedures Departure Preview Departure Choices FLIGHT MANAGEMENT Figure 5-93 Departure Selection Loaded Departure ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Selected Departure APPENDICES Procedure Loading Page Selection Softkeys INDEX Figure 5-94 Departure Loading 240 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Viewing available departures at an airport: 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. FLIGHT INSTRUMENTS 2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and press the ENT Key. 3) Turn the large FMS Knob to highlight the Departure. The departure is previewed on the map. 4) Turn the small FMS Knob to view the available departures. Press the ENT Key to select the departure. The cursor moves to the Runway box. The departure is previewed on the map. EIS 5) Turn the small FMS Knob to view the available runways. Press the ENT Key to select the runway. The cursor moves to the Transition box (only if there are available transitions). The departure is previewed on the map. 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-x Softkey to return to the Airport Information Page. Removing a Departure from the Active Flight Plan FLIGHT MANAGEMENT When plans change while flying IFR, departures can be easily removed from the Active Flight Plan. Removing a departure procedure from the active flight plan: 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). HAZARD AVOIDANCE 2) Press the MENU Key, and highlight ‘Remove Departure’. 3) Press the ENT Key. A confirmation window is displayed listing the departure procedure. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT Key. Or: 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, and turn to highlight the departure header in the active flight plan. Or: Use the Joystick to place the Quick Select Box on the departure header. ADDITIONAL FEATURES 3) Press the CLR Key. A confirmation window is displayed listing the departure procedure. APPENDICES 4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT Key. 5) Press the FMS Knob to remove the flashing cursor. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 241 SYSTEM OVERVIEW Flight Management 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’. AUDIO PANEL & CNS 4) Use the FMS Knob to select an airport and press the ENT Key. FLIGHT MANAGEMENT 3) Press the ENT Key. The Arrival Loading Page is displayed. 7) Select a runway (if required) and press the ENT Key. ‘LOAD?’ is highlighted. 5) Select an arrival from the list and press the ENT Key. 6) Select a transition (if required) and press the ENT Key. 8) Press the ENT Key to load the arrival procedure. Available Procedure Actions ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Destination Airport APPENDICES Loaded Procedures Arrival Preview Arrival Choices INDEX Figure 5-95 Arrival Selection 242 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Selected Arrival Loaded Arrival FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS Procedure Loading Page Selection Softkeys FLIGHT MANAGEMENT Figure 5-96 Arrival Loading Viewing available arrivals at an airport: HAZARD AVOIDANCE 1) From the Airport Information Page (first page in the WPT group), select the STAR Softkey. The Arrival Information Page is displayed, defaulting to the airport displayed on the Airport Information Page. 2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and press the ENT Key. 3) Turn the large FMS Knob to highlight the Arrival. The arrival is previewed on the map. 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. 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. ADDITIONAL FEATURES 6) Turn the small FMS Knob to view the available runways. Press the ENT Key to select the runway. The cursor moves to the Sequence box. The arrival is previewed on the map. 7) Press the INFO-x Softkey to return to the Airport Information Page. APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 243 SYSTEM OVERVIEW Flight Management 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: 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, and turn to highlight the arrival header in the active flight plan. Or: Use the Joystick to place the Quick Select Box on the arrival header. FLIGHT MANAGEMENT 3) Press the CLR Key. A confirmation window is displayed listing the arrival procedure. 4) With ‘OK’ highlighted, press the ENT Key. To cancel the removal request, highlight ‘CANCEL’ and press the ENT Key. HAZARD AVOIDANCE 5) Press the FMS Knob to remove the flashing cursor. Approaches 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. ADDITIONAL FEATURES 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. APPENDICES 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. 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 244 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 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. Example on HSI EIS Approach Type AUDIO PANEL & CNS 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 FLIGHT INSTRUMENTS Perspective 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 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: - LNAV - LNAV+V - L/VNAV - LPV FLIGHT MANAGEMENT Table 5-9 Approach Types Loading an Approach into the Active Flight Plan Loading an approach into the active flight plan using the PROC Key: HAZARD AVOIDANCE 1) Press the PROC Key. The Procedures Window is displayed. 2) Highlight ‘SELECT APPROACH’, and press the ENT Key. The Approach Loading Page is displayed. 3) Use the FMS Knob to select an airport and press the ENT Key. 4) Select an approach from the list and press the ENT Key. 5) Select a transition (if required) and press the ENT Key. AFCS 6) Barometric Minimums 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. ADDITIONAL FEATURES Or: b) To skip setting minimums, press the ENT Key. APPENDICES 7) Press the ENT Key with ‘LOAD?’ highlighted to load the approach procedure; or turn the large FMS Knob to highlight ‘ACTIVATE’ and press the ENT Key to load and activate the approach procedure. NOTE: When GPS is not approved for the selected final approach course, the message ‘NOT APPROVED FOR GPS’ is displayed. GPS provides guidance to the approach, but the HSI must to be switched to a NAV receiver to fly the final course of the approach. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 245 SYSTEM OVERVIEW Flight Management Available Procedure Actions AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Destination Airport Loaded Procedures Approach Preview Approach Choices FLIGHT MANAGEMENT Figure 5-97 Approach Selection Loaded Approach ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Selected Approach APPENDICES Procedure Loading Page Selection Softkeys LOAD or ACTIVATE? Annunciation INDEX Figure 5-98 Approach Loading 246 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Viewing available approaches at an airport: 1) From the Airport Information Page (first page in the WPT group), press the APR Softkey. The Approach Information Page is displayed, defaulting to the airport displayed on the Airport information Page. FLIGHT INSTRUMENTS 2) To select another airport, press the FMS Knob to activate the cursor, enter an identifier/facility name/city, and press the ENT Key. 3) Press the FMS Knob, then turn the large FMS Knob to highlight the Approach. The approach is previewed on the map. 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 Transition box. The approach is previewed on the map. 5) Turn the small FMS Knob to view the available transitions. Press the ENT Key to select the transition. The cursor moves to the Minimums box. The approach is previewed on the map. AUDIO PANEL & CNS 6) Turn the small FMS Knob to select BARO minimums on or off. Press the ENT Key. a) When minimums are selected on, the cursor moves to the minimum altitude field . Use the small FMS Knob to select the altitude. Press the ENT Key. The cursor moves to the Sequence box. The approach is previewed on the map. FLIGHT MANAGEMENT Or: b) When minimums are selected off, the cursor moves to the Sequence box. The approach is previewed on the map. 7) Press the INFO-x Softkey to return to the Airport Information Page. HAZARD AVOIDANCE 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. AFCS 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. ADDITIONAL FEATURES 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. 6) Turn the FMS Knob to highlight the desired transition, and press the ENT Key. 7) Barometric Minimums APPENDICES 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. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX 8) Press the ENT Key with ‘LOAD?’ highlighted to load the approach procedure; or turn the large FMS Knob to highlight ‘ACTIVATE’ and press the ENT Key to load and activate the approach procedure. The system continues navigating the current flight plan until the approach is activated. When GPS is not approved for the selected final approach course, the message ‘NOT APPROVED FOR GPS’ is displayed. GPS provides guidance to the approach, but the HSI must to be switched to a NAV receiver to fly the final course of the approach. 247 SYSTEM OVERVIEW Flight Management 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: AUDIO PANEL & CNS 1) Press the PROC Key to display the Procedures Window. 2) Highlight ‘ACTIVATE VECTOR-TO-FINAL’ and press the ENT Key. Loading and activating an approach using the MENU Key: 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: AFCS 1) Press the FPL Key to display the Active Flight Plan Page (MFD) or the Active Flight Plan Window (PFD). 2) Press the MENU Key, and highlight ‘Remove Approach’. 3) Press the ENT Key. A confirmation window is displayed listing the approach procedure. 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). APPENDICES 2) Press the FMS Knob, and turn to highlight the approach header in the active flight plan. Or: Use the Joystick to place the Quick Select Box on the approach header. 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. INDEX 5) Press the FMS Knob to remove the flashing cursor. 248 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 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: Press the Go-Around Button. EIS Course To Altitude 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. FLIGHT MANAGEMENT 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. AFCS ADDITIONAL FEATURES Course to Altitude Leg APPENDICES Figure 5-99 Course to Altitude INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 249 SYSTEM OVERVIEW Flight Management 5.9 Trip Planning FLIGHT INSTRUMENTS Perspective 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 AUDIO PANEL & CNS - FPL Number/Cumulative Legs (CUM or REM) or Leg Number (NN) - Waypoints Defining Selected Flight Plan/Flight Plan Leg Trip Planning Page Mode - Automatic/Manual FLIGHT MANAGEMENT Preview of Selected Flight Plan/ Flight Plan Leg Trip Input Data (sensor/pilot) - Departure Time (local) - Ground Speed - Fuel Flow - Fuel On Board Aircraft - Calibrated Airspeed - Indicated Altitude - Barometric Pressure - Total Air Temperature Trip Statistics HAZARD AVOIDANCE Desired Track Distance Est. Time Enroute Est. Time of Arrival Enroute Safe Altitude Sunrise Time (local) Sunset Time (local) - Other Statistics - Density Altitude - True Airspeed (TAS) AFCS Fuel Statistics ADDITIONAL FEATURES Efficiency Total Endurance Remaining Fuel Remaining Endurance Fuel Required Total Range - Softkeys - Automatic/Manual Page Mode - Flight Plan/Waypoint Mode Figure 5-100 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. INDEX • Indicated altitude (IND ALTITUDE) - The primary source is the barometric altitude, and the secondary source of information is GPS altitude. 250 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Trip Statistics The trip statistics are calculated based on the selected starting and ending waypoints and the trip planning inputs. FLIGHT INSTRUMENTS In flight plan mode (FPL) with a stored flight plan selected (NN), and the entire flight plan (CUM) selected, the waypoints are the starting and ending waypoints of the selected flight plan. In flight plan mode (FPL) with a stored flight plan selected (NN), and a specific leg (NN) selected, the waypoints are the endpoints of the selected leg. 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. - If in waypoint mode then the ETA is the ETE added to the departure time. 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 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 • Destination sunrise and sunset times (SUNRISE, SUNSET) - These times are shown as hours:minutes and are the local time at the destination. Fuel Statistics 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX 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. 251 SYSTEM OVERVIEW • Fuel efficiency (EFFICIENCY) - This value is calculated by dividing the current ground speed by the current fuel flow. FLIGHT INSTRUMENTS Flight Management • Fuel on board upon reaching end of selected leg (REM FUEL) - This value is calculated by taking the amount of fuel onboard and subtracting the fuel required to reach the end of the selected leg. • Time of fuel endurance (TOTAL ENDUR) - This time is shown as hours:minutes. This value is obtained by dividing the amount of fuel on board by the current fuel flow. • Fuel endurance remaining at end of selected leg (REM ENDUR) - This value is calculated by taking the time of fuel endurance and subtracting the estimated time enroute to the end of the selected leg. EIS • Fuel required for trip (FUEL REQ) - This value is calculated by multiplying the time to go by the fuel flow. AUDIO PANEL & CNS • 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. FLIGHT MANAGEMENT • Density altitude (DENSITY ALT) • True airspeed (TRUE AIRSPEED) HAZARD AVOIDANCE The pilot may select automatic (AUTO) or manual (MANUAL) page mode, and flight plan (FPL) or waypoint (WPTS) mode. In automatic page mode, only the FPL, LEG, or waypoint IDs are editable (based on FPL/WPTS selection). Selected Flight Plan NN - Selected Leg(s) 00 is Active FPL 01-99 are Stored FPLs AFCS 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 ADDITIONAL FEATURES Figure 5-101 Trip Planning Page - Flight Plan Mode Selected Flight Plan Selected Leg(s) Not Available Not Available APPENDICES Selected Starting and Ending Waypoints Figure 5-102 Trip Planning Page - Waypoint Mode Selecting automatic or manual page mode: INDEX 252 Press the AUTO Softkey or the MANUAL Softkey; or press the MENU Key, highlight ‘Auto Mode’ or ‘Manual Mode’, and press the ENT Key. Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW Selecting flight plan or waypoint mode: 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. FLIGHT INSTRUMENTS Selecting a flight plan and leg for trip statistics: 1) Press the FMS Knob to activate the cursor in the flight plan number field. 2) Turn the small FMS Knob to select the desired flight plan number. EIS 3) Turn the large FMS Knob to highlight ‘CUM’ or ‘REM’. The statistics for each leg can be viewed by turning the small FMS Knob to select the desired leg. The Inset Map also displays the selected data. Selecting waypoints for waypoint mode: AUDIO PANEL & CNS 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. 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. FLIGHT MANAGEMENT 3) Turn the FMS knobs to select the desired waypoint, and press the ENT Key. The statistics for the selected leg are displayed. In manual page mode, the other eight trip input data fields must be entered by the pilot, in addition to flight plan and leg selection. Entering manual data for trip statistics calculations: HAZARD AVOIDANCE 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. AFCS 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. ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 253 SYSTEM OVERVIEW Flight Management 5.10 RAIM Prediction FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 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. RAIM PREDICTION Box AFCS HAZARD AVOIDANCE - Prediction Waypoint - Arrival Time - Arrival Date - RAIM Status RAIM Softkey SBAS Softkey (displays SBAS Selection) (displays RAIM PREDICTION) INDEX APPENDICES ADDITIONAL FEATURES Figure 5-103 RAIM Prediction 254 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 3) Turn the small FMS Knob to display the Waypoint Information Window. (Turning it clockwise displays a blank Waypoint Information Window, turning it counter-clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan, nearest, recent, user, or airway waypoints). EIS 4) Enter the identifier, facility, or city name of the departure waypoint; or select a waypoint from the submenu of waypoints and press the ENT Key to accept the waypoint entry. 5) Turn the FMS Knobs to enter an arrival time and press the ENT Key. 6) Turn the FMS Knobs to enter an arrival date and press the ENT Key. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 2) Press the FMS Knob. The RAIM Prediction ‘WAYPOINT’ field is highlighted. 3) Press the MENU Key, highlight ‘Set WPT to Present Position’, and press the ENT Key. 4) Press the ENT Key to accept the waypoint entry. HAZARD AVOIDANCE 5) Turn the FMS Knobs to enter an arrival time and press the ENT Key. 6) Turn the FMS Knobs to enter an arrival date and press the ENT Key. 7) Press the ENT Key with ‘COMPUTE RAIM?’ highlighted to begin the computation. Status of the RAIM computation for the selected waypoint, time, and date is displayed at the bottom of the RAIM PREDICTION Box as follows: AFCS • ‘COMPUTE RAIM?’ - RAIM has not been computed. • ‘COMPUTING AVAILABILITY’ - RAIM calculation is in progress. • ‘RAIM AVAILABLE’ - RAIM is predicted to be available. ADDITIONAL FEATURES • ‘RAIM NOT AVAILABLE’ - RAIM is predicted to be unavailable. The Satellite Based Augmentation System (SBAS) provides increased navigation accuracy when available. SBAS can be enabled or disabled manually on the GPS Status Page. APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 255 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) Figure 5-104 SBAS Display - Active Enabling/Disabling SBAS: HAZARD AVOIDANCE 1) Select the AUX-GPS Status Page. 2) Press the SBAS Softkey. 3) Press the FMS Knob. The SBAS SELECTION ‘WAAS’ field is highlighted. AFCS 4) Press the ENT Key to disable SBAS. Press the ENT Key again to enable SBAS. ADDITIONAL FEATURES SBAS Status SBAS SELECTION Box INDEX APPENDICES - WAAS Enable/Disable RAIM Softkey SBAS Softkey (displays SBAS Selection) (displays RAIM PREDICTION) Figure 5-105 SBAS Display - Disabled 256 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 Perspective provides vertical guidance through descents. A lateral flight plan (LNAV) would be navigated in much the same way, but would not include vertical guidance when the final approach course is active. nOTE: The following example flight plan is for instructional purposes only. All database information depicted should be considered not current. EIS 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. AUDIO PANEL & CNS 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 5-106 indicating the active departure leg. After takeoff, ATC assigns a heading of 240º. FLIGHT MANAGEMENT 2) Figure 5-106 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 5-106 Assigned Heading of 240º INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 257 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 5-107. Figure 5-107 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. 258 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 5-108. 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 5-108 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 5-109. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 5-109 Entering V4 Entry Point INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 259 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 5-110. FLIGHT MANAGEMENT Figure 5-110 TOP Inserted into the Flight Plan e) With SLN still highlighted as in Figure 5-110, 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 5-111. Figure 5-111 List of Available Airways for TOP INDEX g) Turn either FMS Knob to highlight V4 in the list as seen in Figure 5-111. 260 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW h) Press the ENT Key. The list of available exits for V4 is now displayed as in Figure 5-112. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-112 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 5-112. HAZARD AVOIDANCE j) Press the ENT Key. The selected airway and exit are displayed, and the prompt “LOAD?” highlighted as in Figure 5-113. AFCS ADDITIONAL FEATURES APPENDICES Figure 5-113 Ready to Load V4 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX k) Press the ENT Key. 261 SYSTEM OVERVIEW Flight Management AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS l) V4 is now loaded into the flight plan as shown in Figure 5-114. FLIGHT MANAGEMENT Figure 5-114 V4 is Loaded in the Flight Plan 5) Making V4 the active leg of the flight plan. a) Press the FMS Knob to activate the cursor. b) Turn the large FMS Knob to highlight SLN. The TO waypoint of the leg is selected in order to activate the leg. AFCS HAZARD AVOIDANCE c) Press the ACT LEG Softkey. The confirmation window is now displayed as in Figure 5-115. Note the TOP to SLN leg is actually part of V4. INDEX APPENDICES ADDITIONAL FEATURES Figure 5-115 Comfirm Active Leg 262 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW FLIGHT INSTRUMENTS d) Verify the displayed leg is the desired leg and press the ENT Key. Note in Figure 5-116, 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 5-116 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 263 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 5-117. Figure 5-117 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 5-118. INDEX APPENDICES Figure 5-118 Turn to Intercept V244 264 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 9) As seen in Figure 5-119, V244 is now the active flight plan leg. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-119 V244 Now Active Leg HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 265 SYSTEM OVERVIEW Flight Management FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 10) At Lamar VOR (LAA) V263 is intercepted. See Figure 5-120. Figure 5-120 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 5-121. INDEX APPENDICES ADDITIONAL FEATURES AFCS c) Press the Direct-to ( Figure 5-121 Direct To OPSHN 266 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW d) Turn the large FMS Knob to place the cursor in the VNV altitude field as shown in Figure 5-122. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-122 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 5-123. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 5-123 Enter VNV Offset Distance 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 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 system gives vertical guidance so the aircraft arrives at an altitude of 10,000 feet three miles prior to OPSHN. 267 SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS h) Press the ENT Key twice to activate the direct-to. Note, in Figure 5-124, 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 theCDI 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 5-124 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. 268 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW b) ‘SELECT APPROACH’ should be highlighted as shown in Figure 5-125. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-125 Procedures Window c) Press the ENT Key. A list of available approaches for the destination airport is displayed as in Figure 5-126. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 5-126 List of Available Approaches d) Turn either FMS Knob to select the LPV approach for 35R as shown in Figure 5-126. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 269 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 5-127. 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 5-127 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. 270 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS Figure 5-128 Barometric Minimums Set FLIGHT MANAGEMENT i) With ‘LOAD?’ highlighted, again press the ENT Key. The selected approach is added to the flight plan as seen in Figure 5-129. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 5-129 Loaded Approach INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 271 SYSTEM OVERVIEW Flight Management 13) Note the altitude constraints associated with each of the approach waypoints as seen in Figure 5-130. 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 5-130. 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 5-130 Vertical Guidance is Active to the FAF 272 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 5-131. 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 5-131 Adjusting the Descent ADDITIONAL FEATURES c) Press the ENT Key. APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 273 SYSTEM OVERVIEW Flight Management FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 15) As seen in Figure 5-132, the aircraft is approaching TOD. Note the target vertical speed required to reach 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 5-133. When the aircraft is within one minute of the TOD, it is annunciated as shown in Figure 5-133, and an aural alert ‘Vertical track’ will be heard. HAZARD AVOIDANCE Figure 5-132 Approaching Top of Descent (TOD) AFCS Target Altitude ADDITIONAL FEATURES Vertical Deviation Indicator (VDI) APPENDICES Required Vertical Speed Indicator (RVSI) INDEX Figure 5-133 VDI & RVSI Upon Reaching Top of Descent (TOD) 274 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 16) Upon reaching TOD, a descent vertical speed is established by placing the VSI pointer in line with the RVSI as shown in Figure 5-134. FLIGHT INSTRUMENTS EIS Keep Vertical Deviation Indicator Centered AUDIO PANEL & CNS Align Actual Vertical Speed with Required Vertical Speed FLIGHT MANAGEMENT Figure 5-134 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 5-135. Upon reaching the offset waypoint for OPSHN, the aircraft is at 10,000 feet. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 5-135 Approaching Bottom of Descent (BOD) at OPSHN Offset Waypoint INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 275 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 5-136. 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 5-136 Turn to intercept OPSHN to FSHER Leg 276 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Flight Management SYSTEM OVERVIEW 19) After passing OPSHN, the next leg of the arrival turns magenta as shown in Figure 5-137. 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 5-137 Tracking the OPSHN to FSHER Leg HAZARD AVOIDANCE 20) The flight continues through the arrival procedure to PYNON (see Figure 5-138). 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 277 APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Flight Management INDEX Figure 5-138 Approaching PYNON 278 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 5-139). FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-139 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 5-140. AFCS c) Press the ENT Key to activate the approach. ADDITIONAL FEATURES APPENDICES Figure 5-140 Manually Activate Approach INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 279 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 5-141 Descending Turn to the Initial Approach Fix (IAF) 280 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 5-142) when the final approach course becomes active. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 5-142 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 5-142. AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 281 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 5-143. Figure 5-143 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. 282 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 5-144. 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 5-144 Missed Approach Active INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 283 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 5-145. Figure 5-145 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 5-146. INDEX Figure 5-146 Hold Established 284 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 Perspective stops using GPS. EIS While in Enroute or Oceanic phase of flight, if the system detects an invalid GPS solution or is unable to calculate a GPS position, the system automatically reverts to Dead Reckoning (DR) Mode. In DR Mode, the system uses its last-known position combined with continuously updated airspeed and heading data (when available) to calculate and display the aircraft’s current estimated position. AUDIO PANEL & CNS It is important to note that estimated navigation data supplied by Perspective 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 Perspective 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 AFCS DR Mode is indicated on the system by the appearance of the letters ‘DR’ superimposed in yellow over the ‘own aircraft’ symbol as shown in Figure 5-147. 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 5-147. The CDI deviation bar remains, but is removed from the display after 20 minutes in DR Mode. The autopilot will remain coupled in DR mode as long as the deviation info is available (20 min.) 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. ADDITIONAL FEATURES 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 5-147. Also, while Perspective is in DR Mode, the autopilot does not couple to GPS, and TAWS, Terrain-SVS, 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 285 SYSTEM OVERVIEW Flight Management FLIGHT INSTRUMENTS Distance & Bearing EIS Dead Reckoning Annunciaion Wind Data GPS Navigation Lost Message AUDIO PANEL & CNS Current Track Indicator Course Deviation Indicator FLIGHT MANAGEMENT Bearing Pointer/ Distance Destination Airport Information Nav Data Bar Wind Data HAZARD AVOIDANCE All data except Active Leg, TAS, and DTK are in yellow AFCS Dead Reckoning Annunciation ADDITIONAL FEATURES Subdued Aircraft Symbol APPENDICES Figure 5-147 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. 286 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW Section 6 Hazard Avoidance FLIGHT INSTRUMENTS Hazard avoidance features available for Perspective™ 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 69/69A XM Satellite Weather (Optional) ® • L-3 STORMSCOPE WX-500 Series II Weather Mapping Sensor (Optional) EIS Terrain Avoidance • Terrain Proximity AUDIO PANEL & CNS • Terrain-SVS (Standard with SVS Option) • Terrain Awareness and Warning System - Class B (TAWS-B) (Optional) • Profile View Terrain Traffic FLIGHT MANAGEMENT • Garmin GTS 800 Traffic Advisory System (TAS) (Optional) ® • Avidyne TAS610 Traffic Advisory System (TAS) (Optional) ® • L-3 SKYWATCH (SKY497) Traffic Advisory System (TAS) (Optional) HAZARD AVOIDANCE 6.1 XM Satellite Weather ® Note: XM Satellite Weather data provides information for avoiding hazardous weather. Do not use XM Weather information to penetrate hazardous weather. AFCS XM® Satellite Weather is provided through the GDL 69/69A, 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. ADDITIONAL FEATURES XM Satellite Radio services are subscription-based. For more information on specific service packages, visit www.xmradio.com. APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 287 SYSTEM OVERVIEW Hazard Avoidance Activating Services FLIGHT INSTRUMENTS Before XM Satellite Weather and XM Satellite Radio can be used, the service must be activated. Service is activated by providing coded IDs unique to the installed GDL 69/69A. XM Satellite Radio and XM Satellite Weather services each have coded IDs. The Data and Audio Radio IDs must be provided 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 Perspective™ to display weather data and/or entertainment programming provided through the GDL 69/69A. 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. Data Radio ID (for XM Weather) ADDITIONAL FEATURES Audio Radio ID (for XM Satellite Radio) APPENDICES Weather Products (Available Products for Service Class Indicated in Green) INDEX Select to Display XM Information page 288 Figure 6-1 XM Information Page Select to Lock Subscription Information Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW Using XM Satellite Weather Products The primary map for viewing XM Weather data is the XM Weather Data Link Page in the Map Page Group. This is the only Perspective™ map display capable of showing information for all available XM weather products. FLIGHT INSTRUMENTS Viewing the XM 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 XM Weather Data Link Page. EIS NEXRAD Weather Product Display Enabled NEXRAD Weather Product Ages (US & Canada) AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 6-2 Weather Data Link Page AFCS NEXRAD Weather Product Selected for Display ADDITIONAL FEATURES When an XM weather product is active on a map, the age of the data is displayed on the screen to the right of the product symbol (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 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. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T INDEX 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. 289 SYSTEM OVERVIEW Hazard Avoidance Weather Product Symbol FLIGHT INSTRUMENTS Next-generation Radar (NEXRAD) Cloud Top (CLD TOP) Echo Top (ECHO TOP) INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 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) Icing Potential (CIP and SLD) (ICNG) Pilot Weather Report (PIREPs) Air Report (AIREPs) Turbulence (TURB) Radar Coverage no product image (RADAR CVRG) Temporary Flight Restrictions no product image (TFRs) Terminal Aerodrome Reports no product image (TAFs) Expiration Time (Minutes) 30 Refresh Rate (Minutes) 5 (U.S.) 10 (Canada) 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 90 22 90 12 90 12 180 12 30 5 60 12 60 12 Table 6-1 Weather Product Symbols and Data Timing 290 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW Echo Top (ECHO TOP) + + + + + + + + + + XM Lightning (LTNG) + + + + Cell Movement (CELL MOV) + + + + SIGMETs/AIRMETs (SIG/AIR) METARs + + + + + Surface Analysis (SFC) + Freezing Levels (FRZ LVL) + Winds Aloft (WIND) +* + Cyclone Warnings (CYCLONE) + Icing Potential (ICNG) + PIREPs + + AIREPs + + Turbulence (TURB) + + + + + + + + + + + + ADDITIONAL FEATURES + AFCS TAFs + HAZARD AVOIDANCE + + + + County Warnings (COUNTY) Radar Coverage + FLIGHT MANAGEMENT City Forecast (CITY) TFRs AUDIO PANEL & CNS Flight Plan Pages + Nearest Page Group Cloud Top (CLD TOP) AUX - Video Page + AUX - Trip Planning Page XM Weather Data Link Page + Weather Information Page Navigation Map Page + 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. * Winds Aloft Data displayed inside Profile View on the Navigation Map Page. Table 6-2 Weather Product Display Maps APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 291 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 XM 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 CYCLONE SFC OFF FRZ LVL SIG/AIR METAR LEGEND MORE WX CHKLIST WIND OFF ICNG OFF TURB OFF AIREPS PIREPS COUNTY LTNG CELL MOV BACK EIS SFC Softkey label changes to reflect current selection. WIND/ICNG/TURB Softkey labels change to reflect current selection. CURRENT AUDIO PANEL & CNS OFF 12 HR 24 HR 36 HR 48 HR Select the BACK Softkey to move up one level. LEGEND BACK ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT PREV and NEXT Softkeys cycle through Winds Aloft, Icing, and Turbulence altitude selection softkeys. PREV OFF SFC 3000 6000 9000 12000 15000 NEXT LEGEND BACK PREV OFF 18000 21000 24000 27000 30000 33000 NEXT LEGEND BACK PREV OFF 36000 39000 42000 NEXT LEGEND BACK PREV OFF 1000 3000 6000 9000 12000 NEXT LEGEND BACK PREV OFF 18000 21000 24000 27000 30000 NEXT LEGEND BACK PREV OFF 21000 24000 27000 30000 33000 NEXT LEGEND BACK PREV OFF 39000 42000 45000 NEXT LEGEND BACK 15000 36000 Figure 6-3 Weather Data Link Weather Product Softkeys INDEX APPENDICES The setup menus for the Navigation Map Page and the XM 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. 292 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW Setting up and customizing the XM Weather Data Link Page: 1) Select the XM 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 small FMS Knob to select ‘Product Group 1’ or ‘Product Group 2’, and press the ENT Key (Figure 6-5). 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections. EIS 6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings, etc.). 7) Press the ENT Key to select an option. 8) Press the FMS Knob or CLR Key to return to the XM Weather Data Link Page with the changed settings. AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 6-4 Weather Data Link Page Menu HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Figure 6-5 Weather Data Link Page Setup Menu Restoring default XM Weather Data Link Page settings: 1) Select the XM Weather Data Link Page. APPENDICES 2) Press the MENU Key. 3) With ‘Weather Setup’ highlighted, press the ENT Key. 4) Press the MENU Key. 5) Highlight the desired default(s) to restore (all or for selection) and press ENT Key. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 293 SYSTEM OVERVIEW Hazard Avoidance Maps besides the XM Weather Data Link Page use settings based on those selected for the Navigation Map Page. FLIGHT INSTRUMENTS Setting up and customizing weather data for the Navigation Map Page: 1) Select the Navigation Map Page. 2) Press the MENU Key. 3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-6). 4) Turn the small FMS Knob to select the ‘Weather’ Group and press the ENT Key (Figure 6-7). EIS 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-8). 6) Turn the small FMS Knob to scroll through options for each product (ON/OFF, range settings). AUDIO PANEL & CNS 7) Press the ENT Key to select an option. HAZARD AVOIDANCE FLIGHT MANAGEMENT 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 APPENDICES Figure 6-7 Navigation Map Page Setup Menu Figure 6-8 Navigation Map Page Setup Menu, Weather Group Each active weather product has an associated legend which can be displayed on the XM Weather Data Link Page. A weather product legend can also be displayed on the Navigation Map Page for active XM weather products displayed on that page. Viewing legends for displayed weather products (on the XM Weather Data Link Page): INDEX 1) Select the XM Weather Data Link Page. 2) Press the LEGEND Softkey to display the legends for the displayed weather products. 294 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW Or: a) Press the MENU Key. b) Select ‘Weather Legend’ and press the ENT Key. FLIGHT INSTRUMENTS 3) Turn the FMS Knob to scroll through the legends if more are available than fit in the window. 4) To remove the Legend Window, press the LEGEND Softkey, the ENT or the CLR Key, or press the FMS Knob. Viewing legends for displayed weather products (on the Navigation Map Page): 1) Select the Navigation Map Page. EIS 2) Press the MAP Softkey. 3) Press the LEGEND Softkey (available if one or more XM weather products are enabled for display). AUDIO PANEL & CNS 4) To remove the Legend Window, press the LEGEND Softkey, the ENT or the CLR Key, or press the FMS Knob. Additional information about the following can be displayed by panning over the display on the map: • METARs • Cloud Tops • County Warnings • Cell Movement • TFRs • SIGMETs • AIREPs • AIRMETs • PIREPs FLIGHT MANAGEMENT • Echo Tops HAZARD AVOIDANCE 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. AFCS Additional Information on Weather Feature Selected with Map Pointer ADDITIONAL FEATURES Severe Thunderstorm Warning Selected with Map Pointer APPENDICES INDEX Figure 6-9 Panning on the Weather Data Link Page 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 295 SYSTEM OVERVIEW Hazard Avoidance NEXRAD NOTE: NEXRAD data cannot be displayed at the same time as terrain, echo tops, turbulence, icing data, or FLIGHT INSTRUMENTS optional Stormscope lightning is displayed. EIS 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. ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS 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 INDEX APPENDICES NEXRAD data can be displayed on the following maps: 296 • PFD Inset Map • Trip Planning Page • Navigation Map Page • Nearest Pages • Weather Data Link Page • Flight Plan Pages • Airport Information Page • AUX - Video Page Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 XM 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 XM 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 297 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. Undetermined precipitation types may be displayed as mixed. • 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 298 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 55°N EIS AUDIO PANEL & CNS Precipitation Above 52°N Always Displays as Mixed FLIGHT MANAGEMENT Figure 6-13 NEXRAD Data - Canada HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 299 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: Echo tops cannot be displayed at the same time as NEXRAD or Cloud Tops are selected for display. Figure 6-14 Echo Tops Data AFCS Displaying Echo Tops information: 1) Select the XM 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 300 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 gray shade of-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 XM 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 301 SYSTEM OVERVIEW Hazard Avoidance XM Lightning Note: XM Lightning data cannot be displayed at the same time as optional Stormscope lightning is selected FLIGHT INSTRUMENTS for display. 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 • AUX - Video Page APPENDICES Displaying XM Lightning information: 1) Press the MAP Softkey (for the PFD Inset Map, press the INSET Softkey). This step is not necessary on the XM Weather Data Link Page. 2) Press the XM LTNG Softkey (LTNG Softkey on the XM Weather Data Link Page). INDEX To display the XM Lightning legend on the XM Weather Data Link Page (Figure 6-19), press the LEGEND Softkey when XM Lightning is selected for display. Figure 6-19 Lightning Legend 302 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 XM Weather Data Link Page, Cell Movement data can be selected independently. Cell Movement data can be displayed on the following maps: • Nearest Pages •Navigation Map • Weather Data Link Page AFCS • PFD Inset Map • AUX - Trip Planning Page ADDITIONAL FEATURES Displaying Cell Movement information: 1) Press the MAP Softkey (for the PFD Inset Map, select the INSET Softkey). This step is not necessary on the XM Weather Data Link Page. APPENDICES 2) Press the NEXRAD Softkey (CEL MOV Softkey on the XM Weather Data Link Page). For Cell Movement to be displayed on maps other than the XM 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 XM 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 303 SYSTEM OVERVIEW Hazard Avoidance SIGMETs and AIRMETs EIS FLIGHT INSTRUMENTS SIGMETs (SIGnificant METeorological Information) and AIRMETs (AIRmen’s METeorological Information) are broadcast for potentially hazardous weather. A Convective SIGMET is issued for hazardous convective weather. A localized SIGMET is a significant weather condition occurring at a localized geographical position. AUDIO PANEL & CNS Convective SIGMET HAZARD AVOIDANCE FLIGHT MANAGEMENT AIRMET Turbulence Figure 6-22 SIGMET/AIRMET Data Displaying SIGMETs and AIRMETs: 1) Select the XM Weather Data Link Page. AFCS 2) Press the SIG/AIR Softkey. 3) To view the text of the SIGMET or AIRMET, press the RANGE Knob and move the Map Pointer over the icon. ADDITIONAL FEATURES 4) Press the ENT key. Figure 6-23 shows sample SIGMET text. INDEX APPENDICES 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 304 Figure 6-24 SIGMET/AIRMET Legend Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 Figure 6-25 METAR Flags on the Weather Data Link Page ADDITIONAL FEATURES TAFs (Terminal Aerodrome Forecasts) are weather predictions for specific airports typically within a 24hour period, and may span up to 36 hours. TAFs may 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 XM Weather Data Link Page, press the METAR Softkey. 2) Press the RANGE Knob and pan to the desired airport. INDEX 3) Press the ENT Key. The Weather Information Page is shown with METAR and TAF text. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 305 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 XM 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 XM 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 306 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 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 XM Weather Data Link Page. 2) Press the MORE WX Softkey. ADDITIONAL FEATURES 3) Press the SFC Softkey. 4) Select the desired forecast time: CURRENT, 12 HR, 24 HR, 36 HR, or 48 HR. The SFC Softkey label changes to reflect the forecast time selected. APPENDICES 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. INDEX Figure 6-29 Surface Analysis Legend 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 307 SYSTEM OVERVIEW Hazard Avoidance Freezing Levels HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Freezing Level data shows the color-coded contour lines for the altitude and location at which the first isotherm is found (Figure 6-30). When no data is displayed for a given altitude, the data for that altitude has not been received, or is out of date and has been removed from the display. New data appears at the next update. Figure 6-30 Freezing Level Data Displaying Freezing Level information: AFCS 1) Select the XM 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 308 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 XM 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 12,000 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 309 SYSTEM OVERVIEW Hazard Avoidance AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Winds Aloft data is also shown inside the Profile View (Figure 6-34) on the Navigation Map Page. Wind direction arrows indicate headwind or tailwind components of greater than five knots along the altitude scale using the same symbols shown in the Winds Aloft legend (Figure 6-33). Winds Aloft Data Age Wind Component Velocity and Direction Arrows FLIGHT MANAGEMENT Altitude Scale HAZARD AVOIDANCE Figure 6-34 Navigation Map Page with Winds Aloft Data on Vertical Profile View Enabling/disabling vertical profile view (containing winds aloft data) 1) Select the Navigation Map Page. AFCS 2) Select the PROFILE Softkey. Or: 1) Press the MENU Key. INDEX APPENDICES ADDITIONAL FEATURES 2) Turn the large FMS Knob to highlight ‘Show Profile View’ or ‘Hide Profile View’ (choice dependent on current state) and press the ENT Key. 310 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW County Warnings FLIGHT INSTRUMENTS County data (Figure 6-35) 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. Additional Information on Flood Warning Selected with Map Pointer EIS AUDIO PANEL & CNS Flood Warning FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 6-35 County Flood Warning AFCS Displaying County Warning information: 1) Select the XM Weather Data Link Page. 2) Press the MORE WX Softkey. ADDITIONAL FEATURES 3) Press the COUNTY Softkey. To display the County Warnings legend (Figure 6-35), press the LEGEND Softkey when County Warnings are selected to be displayed. APPENDICES INDEX Figure 6-36 County Warnings Legend 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 311 SYSTEM OVERVIEW Hazard Avoidance Cyclone FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS The Cyclone weather product (Figure 6-37) shows the current location of cyclones (hurricanes) and tropical storms using the symbol shown below (Figure 6-38). Storm tracks include date and time of arrival inside orange boxes. Cyclone HAZARD AVOIDANCE Figure 6-37 Cyclone Data Selected for Display Displaying cyclone (hurricane) track information: 1) Select the XM Weather Data Link Page. 2) Press the MORE WX Softkey. AFCS 3) Press the CYCLONE Softkey. ADDITIONAL FEATURES To display the Cyclone legend (Figure 6-37), press the LEGEND Softkey when Cyclones are selected to be displayed. INDEX APPENDICES Figure 6-38 Cyclone Legend 312 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW Icing (CIP & SLD) Note: Icing data cannot be displayed at the same time as NEXRAD data is selected for display. FLIGHT INSTRUMENTS Current Icing Product (CIP) data shows a graphical view of the current icing environment (Figure 6-39). Icing severity is displayed in four categories: light, moderate, severe, and extreme (not specific to aircraft type). The CIP product is not a forecast, but a presentation of the current conditions at the time of the analysis. EIS Supercooled Large Droplet (SLD) icing conditions are characterized by the presence of relatively large, super cooled water droplets indicative of freezing drizzle and freezing rain aloft. SLD threat areas are depicted as magenta dots over the CIP colors. Displaying Icing data: 1) Select the XM Weather Data Link Page. AUDIO PANEL & CNS 2) Press the MORE WX Softkey. 3) Press the ICNG Softkey. FLIGHT MANAGEMENT 4) Select the desired altitude level: 1,000 feet up to 30,000 feet. Press the NEXT or PREV Softkey to cycle through the altitude softkeys. The ICNG Softkey label changes to reflect the altitude selected. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 6-39 Icing Data at 18,000 Feet To display the Icing Potential legend (Figure 6-40), press the LEGEND Softkey when Icing is selected for display. INDEX Figure 6-40 Icing Potential Legend 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 313 SYSTEM OVERVIEW Turbulence FLIGHT INSTRUMENTS Hazard Avoidance Turbulence data identifies the potential for erratic movement of high-altitude air mass associated winds. Turbulence is classified as light, moderate, severe or extreme, at altitudes between 21,000 and 45,000 feet. Turbulence data is intended to supplement AIRMETs and SIGMETs. Note: Turbulence data cannot be displayed at the same time as NEXRAD data is selected for display. Displaying Turbulence data: EIS 1) Select the XM Weather Data Link Page. 2) Press the MORE WX Softkey. 3) Press the TURB Softkey. ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS 4) Select the desired altitude level: 21,000 feet up to 45,000 feet. Press the NEXT or PREV Softkey to cycle through the altitude softkeys. The TURB Softkey label changes to reflect the altitude selected. Figure 6-41 Turbulence Data at 24,000 Feet INDEX APPENDICES To display the Turbulence legend (Figure 6-42), press the LEGEND Softkey when Turbulence is selected for display. Figure 6-42 Turbulence Legend 314 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW PIREPs and AIREPs FLIGHT INSTRUMENTS Pilot Weather Reports (PIREPs) provide timely weather information for a particular route of flight. When significant weather conditions are reported or forecast, Air Traffic Control (ATC) facilities are required to solicit PIREPs. A PIREP may contain unforecast adverse weather conditions, such as low in-flight visibility, icing conditions, wind shear, and turbulence. PIREPs are issued as either Routine (UA) or Urgent (UUA). Another type of PIREP is an Air Report (AIREP). AIREPs are used almost exclusively by commerical airlines and are considered lower priority to general aviation pilots. EIS Instructions for Viewing PIREP and AIREP Text AUDIO PANEL & CNS FLIGHT MANAGEMENT Urgent PIREP Selected Routine PIREP HAZARD AVOIDANCE AIREP Figure 6-43 AIREPs and PIREPs on the Weather Data Link Page AFCS Displaying PIREP and AIREP text: 1) Select the XM Weather Data Link Page. 2) Press the MORE WX Softkey. ADDITIONAL FEATURES 3) Press the AIREPS or PIREPS Softkey. 4) Press the RANGE Knob and pan to the desired weather report. A gray circle will appear around the weather report when it is selected. APPENDICES 5) Press the ENT Key. The Weather Information Page is shown with PIREP or AIREP text. The data is first displayed in a decoded fashion, then as raw text. 6) Use the FMS Knob or the ENT Key to scroll through the PIREP or AIREP text. 7) Press the FMS Knob or the CLR Key to return to the XM Weather Data Link Page. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 315 FLIGHT INSTRUMENTS SYSTEM OVERVIEW Hazard Avoidance Decoded PIREP Text Raw PIREP Text AUDIO PANEL & CNS EIS Selected PIREP FLIGHT MANAGEMENT Figure 6-44 PIREP Text on the Weather Information Page To display the PIREP or AIREP legend (Figure 6-45), press the LEGEND Softkey when PIREPs or AIREPs are selected for display. HAZARD AVOIDANCE The PIREP color is determined by the type (routine or urgent). INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 6-45 AIREPs & PIREPs Legend 316 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW 6.2 Stormscope Lightning FLIGHT INSTRUMENTS NOTE: The optional L-3 WX-500 Stormscope® system is not intended for hazardous thunderstorm penetration. Weather information on the Perspective™ MFD is approved for weather avoidance only. Refer to the WX500 User’s Guide for detailed operation information. Note: XM Lightning data cannot be displayed at the same time as Stormscope lightning is selected for display. EIS The following pages can display Stormscope data: • AUX - Trip Planning Page • Nearest Pages AUDIO PANEL & CNS • Stormscope Page • Navigation Map • AUX - Video Page 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 symbols shown in Table 6-3. HAZARD AVOIDANCE Table 6-3 Lightning Age and Symbols AFCS Setting Up Stormscope on the Navigation Map ADDITIONAL FEATURES Setting up Stormscope options on the Navigation Map: 1) On the Navigation Map Page, press the MENU Key. 2) With ‘Map Setup’ selected (Figure 6-45), press the ENT Key. APPENDICES 3) Turn the small FMS Knob to display the group selection window. Turn the small FMS Knob to select ‘Weather’ (Figure 6-46), and press the ENT Key. 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. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T INDEX 7) Press the FMS Knob to return to the Navigation Map Page (Figure 6-47). 317 SYSTEM OVERVIEW Hazard Avoidance The following options are available (Figure 6-47): • 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. AUDIO PANEL & CNS EIS • 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. APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT Figure 6-46 Page Menu INDEX Figure 6-47 Map Setup Menu 318 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW Cell and Strike Mode on the Navigation Map FLIGHT INSTRUMENTS On the Navigation Map, cell mode identifies cells of lightning activity (Figure 6-48). 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. EIS 3) Select the ‘Weather’ group. 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. 7) Press the FMS knob to return to the Navigation Map Page. FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Figure 6-48 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. This is to ensure that the strike and/or cell positions are depicted accurately in relation to the nose of the aircraft. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 319 SYSTEM OVERVIEW Hazard Avoidance Manually clearing Stormscope data on the Navigation Map: 1) Press the MENU Key. FLIGHT INSTRUMENTS 2) Select ‘Clear Stormscope® Lightning’ (Figure 6-49). AUDIO PANEL & CNS EIS 3) Press the ENT Key. Figure 6-49 Navigation Map Page Options Menu FLIGHT MANAGEMENT Zoom Range on the Navigation Map HAZARD AVOIDANCE 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. ADDITIONAL FEATURES AFCS 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 6-49). INDEX APPENDICES Figure 6-50 Lightning Display Range Annunciation 320 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW Selecting a Stormscope range on the Navigation Map: 1) Press the MENU Key. 2) Select ‘MAP SETUP’. FLIGHT INSTRUMENTS 3) Select the ‘Weather’ group. 4) Press the ENT Key. 5) Turn the large FMS Knob to select ‘STRMSCP SMBL’. 6) Turn the small FMS Knob to select the maximum display range. EIS 7) Press the ENT Key. 8) Press the FMS Knob to return to the Navigation Map Page. AUDIO PANEL & CNS To change the display range on the Navigation Map Page, turn the RANGE Knob clockwise to zoom out or counter-clockwise to zoom in. Selecting the Stormscope Page Stormscope lightning data can be displayed at the ranges of 25 nm, 50 nm, 100 nm, and 200 nm. FLIGHT MANAGEMENT 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 3) To change the map range, turn the RANGE Knob clockwise to zoom out or counter-clockwise to zoom in. AFCS ADDITIONAL FEATURES APPENDICES 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T INDEX Figure 6-51 Stormscope Page 321 SYSTEM OVERVIEW Hazard Avoidance Changing between ‘cell’ and ‘strike’ mode on the Stormscope Page: 1) Select the Stormscope Page. FLIGHT INSTRUMENTS 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. 4) Press the BACK Softkey to return to the main Stormscope page. Changing the viewing mode between 360˚ and 120˚ on the Stormscope Page: EIS 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. INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS 3) Press the BACK Softkey to return to the main Stormscope page. 322 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 Perspective™ 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 Perspective™ 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. GPSMSL altitude does not require local altimeter settings to determine MSL altitude. It is a widely-used MSL altitude source. ADDITIONAL FEATURES APPENDICES 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. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 323 SYSTEM OVERVIEW Hazard Avoidance Displaying Terrain Proximity Data FLIGHT INSTRUMENTS The symbols and colors in Figure 6-52 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 6-52 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 • AUX - Video 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 6-55). 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 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. 324 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS 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. Customizing terrain and obstacle display on the Navigation Map Page: EIS 1) Select the Navigation Map Page. 2) Press the MENU Key. 3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-53). AUDIO PANEL & CNS 4) Turn the small FMS Knob to select the ‘Map’ Group and press the ENT Key (Figure 6-54). 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 FLIGHT MANAGEMENT • 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). 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. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Figure 6-53 Navigation Map Page Menu APPENDICES 190-00820-06 Rev. A INDEX Figure 6-54 Navigation Map Page Setup Menu Figure 6-55 Navigation Map Page Setup Menu, Map Group Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 325 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. FLIGHT INSTRUMENTS Additional Information on Obstacle Selected with Map Pointer Red Terrain Area (Above or Within 100’ Below Aircraft Altitude) Yellow Terrain Area (Between 100’ and 1000’ Below Aircraft Altitude) EIS Red Lighted Obstacles (Above or Within 100’ Below Aircraft Altitude) AUDIO PANEL & CNS Lighted Obstacle Selected with Map Pointer FLIGHT MANAGEMENT Terrain Display Enabled Icon Terrain Legend HAZARD AVOIDANCE Figure 6-56 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 Arc’ or ‘View 360º’ (choice dependent on current state) and press the ENT Key to change the view. 326 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 Yellow Terrain (Between 100’ and 1000’ Below the Aircraft Altitude) Current Aircraft GPSderived MSL Altitude EIS Black Terrain (More than 1000’ Below the Aircraft Altitude) Map Range Rings AUDIO PANEL & CNS FLIGHT MANAGEMENT Red Terrain (Above or Within 100’ Below the Aircraft Altitude) Terrain Legend Figure 6-57 Terrain Proximity Page (360 View) HAZARD AVOIDANCE AFCS Yellow Terrain (Between 100’ and 1000’ Below the Aircraft Altitude) Map Range Arc Black Terrain (Terrain More than 1000’ Below the Aircraft Altitude) ADDITIONAL FEATURES Red Terrain (Above or Within 100’ Below the Aircraft Altitude) APPENDICES Terrain Legend Figure 6-58 Terrain Proximity Page (ARC View) INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 327 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. The TAWS-B option will take precedence over TERRAIN-SVS. AUDIO PANEL & CNS Perspective™ Terrain-SVS is a terrain awareness system integrated with the optional Synthetic Vision System (SVS). Terrain-SVS provides visual and auditory alerting to indicate the presence of threatening terrain or obstacles relevant to the projected flight path. For detailed information regarding SVS, refer to the Synthetic Vision System (SVS) section of the Perspective™ 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 and provides additional alerting capabilities. 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 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 • Valid terrain/obstacle database 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 Perspective™ 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- 328 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW MSL altitude does not require local altimeter settings to determine MSL altitude. It is a widely-used MSL altitude source. 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 6-59 and Table 6-5 are used to represent terrain, obstacles, and potential impact points. AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 6-59 Terrain Altitude/Color Correlation for TERRAIN-SVS Unlighted Obstacle Lighted Obstacle Potential < 1000’ AGL > 1000’ AGL < 1000’ AGL > 1000’ AGL Impact Points Obstacle Location AFCS WARNING: Red obstacle is above or within 100’ below current aircraft altitude ADDITIONAL FEATURES CAUTION: Yellow obstacle is between 100’ and 1000’ below current aircraft altitude Table 6-5 Terrain-SVS Obstacle Colors and Symbology APPENDICES Terrain-SVS information can be displayed on the following maps: • PFD Inset Map • Trip Planning Page • Navigation Map Page • Flight Plan Pages • TERRAIN-SVS Page • AUX - Video Page INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 329 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, press the INSET Softkey). FLIGHT INSTRUMENTS 2) Press the TERRAIN Softkey to display terrain and obstacle data. 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 6-65). EIS The Navigation Map Page Setup Menu provides a means in addition to the softkeys for enabling/disabling the 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. For terrain data, the enable/disable function applies only to the MFD, while the range setting also affects the PFD Inset Map. AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE 2) Press the MENU Key. 3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-60). 4) Turn the small FMS Knob to select the ‘Map’ Group and press the ENT Key (Figure 6-61). 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-62). AFCS • TERRAIN DATA – Turns the display of terrain data on or off and sets maximum range at which terrain is shown ADDITIONAL FEATURES • 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). 7) Press the ENT Key to select an option. INDEX APPENDICES 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. 330 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW FLIGHT INSTRUMENTS Figure 6-60 Navigation Map Page Menu EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 6-61 Navigation Map Page Setup Menu Figure 6-62 Navigation Map Page Setup Menu, Map Group HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 331 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 Arc’ 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. 332 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 Annunciation Window FLIGHT MANAGEMENT Figure 6-63 TERRAIN-SVS Page HAZARD AVOIDANCE Red Terrain (Warning - Terrain Above or Within 100’ Below the Aircraft Altitude) AFCS Map Range Arc Yellow Terrain (Caution - Terrain Between 100’ and 1000’ Below the Aircraft Altitude) ADDITIONAL FEATURES Black Terrain (Terrain More than 1000’ Below the Aircraft Altitude) Terrain Legend Figure 6-64 TERRAIN-SVS Page (ARC View) APPENDICES Annunciation Window INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 333 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 TerrainSVS 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 pop-up 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 6-65 TERRAIN-SVS Alert Annunciations Terrain Display Enabled Terrain Legend INDEX Alert Annunciation Figure 6-66 Navigation Map Page (After TERRAIN-SVS Pop-up Alert Acknowledgment) 334 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance PFD/MFD Alert Annunciation MFD Pop-Up Alert SYSTEM OVERVIEW 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 Figure 6-67. 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 Figure 6-67. ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 335 SYSTEM OVERVIEW Hazard Avoidance Required Terrain Clearance RTC Level (FT) RTC Descending (FT) 800 EIS Required Terrain Clearance (FT) Required Terrain Clearance (FT) FLIGHT INSTRUMENTS 700 600 500 400 300 200 AUDIO PANEL & CNS 100 0 0 5 10 15 20 Distance From Runway (NM) Distance From Runway (NM) 25 30 FLIGHT MANAGEMENT Figure 6-67 FLTA Alert Minimum Terrain and Obstacle Clearance Values HAZARD AVOIDANCE FLTA alerts are automatically inhibited when the aircraft is less than 200 feet above the destination runway elevation while within 0.5 nm of the approach runway or the aircraft is between runway ends. Figure 6-68 TERRAIN-SVS Alerting Disabled (TERRAIN-SVS Inhibited) Annunciation Inhibiting/enabling TERRAIN-SVS alerting: AFCS 1) Select the TERRAIN-SVS Page. 2) Press the INHIBIT Softkey to inhibit or enable TERRAIN-SVS (choice dependent on current state). Or: ADDITIONAL FEATURES a) Press the MENU Key. b) Select ‘Inhibit TERRAIN-SVS’ or ‘Enable TERRAIN-SVS’ (choice dependent on current state) and press the ENT Key. INDEX APPENDICES 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. 336 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW System Status During power-up, TERRAIN-SVS conducts a test of its aural and visual annunciations. An aural alert is issued at test completion. PFD/MFD Alert Annunciation Aural Message System Test in Progress System Test Pass FLIGHT INSTRUMENTS Alert Type None None “Terrain System Failure” EIS Terrain System Test Fail Single Chime Table 6-7 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. TERRAIN-SVS Page Annunciation Aural Message TERRAIN DATABASE FAILURE None TERRAIN FAIL “Terrain System Failure” NO GPS POSITION “Terrain System Not Available” “Terrain System Available” when GPS position is available “Terrain System Not Available” “Terrain System Available” when sufficient GPS signal is received “Terrain System Not Available” “Terrain System Available” when aircraft re-enters database coverage area. AFCS Out of database coverage area None INDEX None APPENDICES Excessively degraded GPS signal ADDITIONAL FEATURES MFD Terrain or Obstacle database unavailable or invalid. TERRAIN-SVS operating with PFD Terrain or Obstacle databases Terrain or Obstacle database unavailable or invalid, invalid software configuration, audio fault No GPS position PFD/ MFD Alert Annunciation None HAZARD AVOIDANCE Alert Cause 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 integrity returns and the and the aircraft is within the database coverage area, the aural message “Terrain System Available” is generated. Table 6-8 TERRAIN-SVS Abnormal Annunciations 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 337 SYSTEM OVERVIEW Hazard Avoidance 6.5 TAWS-B FLIGHT INSTRUMENTS Warning: Do not use TAWS information for primary terrain avoidance. TAWS 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: The data contained in the TAWS databases comes from government agencies. Garmin accurately processes and cross-validates the data but cannot guarantee the accuracy and completeness of the data. AUDIO PANEL & CNS TAWS-B (Terrain Awareness and Warning System - Class B) is an optional feature to increase situational awareness and aid in reducing controlled flight into terrain (CFIT). TAWS-B provides visual and aural annunciations when terrain and obstacles are within the given altitude threshold from the aircraft. The displayed alerts and warnings are advisory in nature only. FLIGHT MANAGEMENT TAWS-B satisfies TSO-C151b Class A requirements for certification. TAWS-B requires the following to operate properly: • A valid terrain/obstacle/airport terrain database • A valid 3-D GPS position solution HAZARD AVOIDANCE TAWS-B uses terrain and obstacle information supplied by government sources. Terrain information is based on terrain elevation information in a database that may contain inaccuracies. Individual obstructions may be shown if available in the database. The data undergoes verification by Garmin to confirm accuracy of the content, per TSO-C151b. However, the displayed information should never be understood as being all-inclusive and data may be inaccurate. ADDITIONAL FEATURES AFCS TAWS-B uses information provided from the GPS receiver to provide a horizontal position and altitude. GPS altitude is derived from satellite measurements. GPS altitude is converted to a mean sea level (MSL)-based altitude (GPS-MSL altitude) and is used to determine TAWS-B alerts. GPS-MSL altitude accuracy is affected by factors such as satellite geometry, but it is not subject to variations in pressure and temperature that normally affect pressure altitude devices. GPS-MSL altitude does not require local altimeter settings to determine MSL altitude. Therefore, GPS altitude provides a highly accurate and reliable MSL altitude source to calculate terrain and obstacle alerts. APPENDICES The terrain and obstacle databases used by TAWS-B are referenced to mean sea level (MSL). Using the GPS position and GPS-MSL altitude, TAWS-B displays a 2-D picture of the surrounding terrain and obstacles relative to the position and altitude of the aircraft. Furthermore, the 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 manner, TAWS-B can provide advanced alerts of predicted dangerous terrain conditions. INDEX Baro-corrected altitude (or indicated altitude) is derived by adjusting the altimeter setting for local atmospheric conditions. The most accurate baro-corrected altitude can be achieved by frequently updating the altimeter setting to the nearest reporting station along the flight path. However, because actual atmospheric conditions seldom match the standard conditions defined by the International Standard Atmosphere (ISA) model (where pressure, temperature, and lapse rates have fixed values), it is common for the baro-corrected altitude (as read 338 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW from the altimeter) to differ from the GPS-MSL altitude. This variation results in the aircraft’s true altitude differing from the baro-corrected altitude. Displaying TAWS-B Data FLIGHT INSTRUMENTS TAWS-B uses yellow (caution) and red (warning) to depict terrain and obstacles (with heights greater than 200 feet above ground level, AGL) alerts relative to aircraft altitude. Colors are adjusted automatically as the aircraft altitude changes. The colors and symbols in Figure 6-69 and Table 6-9 are used to represent terrain, obstacles, and potential impact points. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 6-69 Terrain Altitude/Color Correlation for TAWS-B Unlighted Obstacle Lighted Obstacle Potential Impact Points < 1000’ AGL > 1000’ AGL < 1000’ AGL > 1000’ AGL HAZARD AVOIDANCE 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 Table 6-9 TAWS-B Obstacle Colors and Symbology ADDITIONAL FEATURES TAWS-B information can be displayed on the following maps: • Trip Planning Page • Navigation Map Page • Flight Plan Page • TAWS-B Page • AUX - Video Page APPENDICES • PFD Inset Map Displaying terrain and obstacle information (maps other than the TAWS-B Page): 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. INDEX When TAWS-B is selected on maps other than the TAWS-B Page, an icon to indicate the feature is enabled for display and a legend for TAWS-B terrain colors are shown (Figure 6-75). 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 339 SYSTEM OVERVIEW Hazard Avoidance FLIGHT INSTRUMENTS 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. For terrain data, the enable/disable function applies only to the MFD, while the range setting also affects the PFD Inset Map. Terrain data can be selected for display independently of obstacle data; however, obstacles for which warnings and cautions are issued are shown when terrain is selected for display and the map range is within the setting limit. EIS Maps besides the TAWS-B Page use settings based on those selected for the Navigation Map Page. The maximum display ranges for obstacles on each map are dependent on the range setting made for the Navigation Map. If the maximum range for obstacle display on the Navigation Map is adjusted to below 20 nm, the highest obstacle display range settings on the other applicable maps are also adjusted proportionally. AUDIO PANEL & CNS Customizing terrain and obstacle display on the Navigation Map Page: 1) Select the Navigation Map Page. 2) Press the MENU Key. FLIGHT MANAGEMENT 3) With ‘Map Setup’ highlighted, press the ENT Key (Figure 6-69). 4) Turn the small FMS Knob to select the ‘Map’ Group and press the ENT Key (Figure 6-70). 5) Turn the large FMS Knob or press the ENT Key to scroll through product selections (Figure 6-71). HAZARD AVOIDANCE • 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). AFCS 7) Press the ENT Key to select an option. INDEX APPENDICES ADDITIONAL FEATURES 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings. 340 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW FLIGHT INSTRUMENTS Figure 6-70 Navigation Map Page Menu EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 6-71 Navigation Map Page Setup Menu Figure 6-72 Navigation Map Page Setup Menu, Map Group HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 341 SYSTEM OVERVIEW Hazard Avoidance TAWS-B Page FLIGHT INSTRUMENTS The TAWS-B Page is specialized to show terrain, obstacle, and potential impact point data in relation to the aircraft’s current altitude, without clutter from the basemap. Aviation data (airports, VORs, and other NAVAIDs) can be displayed for reference. If an obstacle and the projected flight path of the aircraft intersect, the display automatically zooms in to the closest potential point of impact on the TAWS-B Page. Aircraft orientation on this map is always heading up unless there is no valid heading. Two views are available relative to the position of the aircraft: the 360° default display and the radar-like ARC (120°) display. Map range is adjustable with the RANGE Knob from 1 to 200 nm, as indicated by the map range rings (or arcs). EIS Displaying the TAWS-B 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 TAWS-B Page. Changing the TAWS-B 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 Arc’ 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 TAWS-B 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. 342 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 FLIGHT MANAGEMENT Figure 6-73 TAWS-B Page (360 View) HAZARD AVOIDANCE Red Terrain (Warning - Terrain Above or Within 100’ Below the Aircraft Altitude) AFCS Map Range Arc Black Terrain (Terrain More than 1000’ Below the Aircraft Altitude) ADDITIONAL FEATURES Yellow Terrain (Caution - Terrain Between 100’ and 1000’ Below the Aircraft Altitude) Terrain Legend APPENDICES Figure 6-74 TAWS-B Page (ARC View) INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 343 SYSTEM OVERVIEW Hazard Avoidance TAWS-B Alerts FLIGHT INSTRUMENTS Alerts are issued when flight conditions meet parameters that are set within TAWS-B software algorithms. TAWS-B alerts typically employ a CAUTION or a WARNING alert severity level, or both. When an alert is issued, visual annunciations are displayed and aural alerts are simultaneously issued. Table 6-10 shows TAWS-B alert types with corresponding annunciations and aural messages. When an alert is issued, annunciations appear on the PFD and MFD. The TAWS-B Alert Annunciation is shown to the upper left of the Altimeter on the PFD and below the Terrain Legend on the MFD. If the TAWS-B Page is not displayed at the time, a pop-up alert appears on the MFD. To acknowledge the pop-up alert: EIS • Press the CLR Key (returns to the currently viewed page), or • Press the ENT Key (accesses the TAWS-B Page) HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS Alert Annunciation Figure 6-75 TAWS-B Alert Annunciations ADDITIONAL FEATURES AFCS Pop-up Alert APPENDICES Terrain Display Enabled Icon Terrain Legend Alert Annunciation INDEX Figure 6-76 Navigation Map Page (After TAWS-B Pop-up Alert Acknowledgment) 344 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance PFD/MFD Alert Annunciation MFD Pop-Up Alert Aural Message Excessive Descent Rate Warning (EDR) “Pull Up” or * or Imminent Obstacle Impact Warning (IOI) or * “Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”* or “Obstacle, Obstacle; Pull Up, Pull Up” * “Terrain Ahead; Terrain Ahead”* or “Caution, Terrain; Caution, Terrain” * “Obstacle Ahead; Obstacle Ahead”* or “Caution, Obstacle; Caution, Obstacle” * “Obstacle Ahead; Obstacle Ahead”* or “Caution, Obstacle; Caution, Obstacle” or Imminent Terrain Impact Caution (ITI) or Reduced Required Obstacle Clearance Caution (ROC) or Imminent Obstacle Impact Caution (IOI) or AFCS “Terrain Ahead; Terrain Ahead”* or “Caution, Terrain; Caution, Terrain” HAZARD AVOIDANCE * FLIGHT MANAGEMENT Reduced Required Terrain Clearance Caution (RTC) or * “Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”* or “Obstacle, Obstacle; Pull Up, Pull Up” None ADDITIONAL FEATURES “Too Low, Terrain” None “Five-Hundred” “Sink Rate” or “Don’t Sink”* or “Too Low, Terrain” APPENDICES * * Alerts with multiple messages are configurable at installation and are installation-dependent. Alerts for the default configuration are indicated with asterisks. Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T INDEX Table 6-10 TAWS-B Alerts Summary 190-00820-06 Rev. A AUDIO PANEL & CNS Reduced Required Obstacle Clearance Warning (ROC) Terrain Ahead, Pull Up; Terrain Ahead, Pull Up’* or “Terrain, Terrain; Pull Up, Pull Up” EIS Imminent Terrain Impact Warning (ITI) Negative Climb Rate Caution (NCR) * “Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”* or “Terrain, Terrain; Pull Up, Pull Up” FLIGHT INSTRUMENTS Reduced Required Terrain Clearance Warning (RTC) Premature Descent Alert Caution (PDA) Altitude Callout “500” Excessive Descent Rate Caution (EDR) SYSTEM OVERVIEW Alert Type 345 SYSTEM OVERVIEW Hazard Avoidance Excessive Descent Rate Alert FLIGHT INSTRUMENTS The purpose of the Excessive Descent Rate (EDR) alert is to provide suitable notification when the aircraft is determined to be closing (descending) upon terrain at an excessive speed. Figure 6-76 shows the parameters for the alert as defined by TSO-C151b. 6000 5500 5000 Height Above Terrain (Feet) 4500 EIS 4000 NK : “SI ion Caut 3500 ” RATE 3000 AUDIO PANEL & CNS 2500 2000 Warning: “PULL UP” 1500 1000 12000 11000 Descent Rate (FPM) 10000 9000 8000 7000 6000 5000 4000 3000 2000 1000 0 0 FLIGHT MANAGEMENT 500 HAZARD AVOIDANCE Figure 6-77 Excessive Descent Rate Alert Criteria Forward Looking Terrain Avoidance AFCS Reduced Required Terrain Clearance (RTC) and Reduced Required Obstacle Clearance (ROC) alerts are issued when the aircraft flight path is above terrain, yet is projected to come within the minimum clearance values in Figure 6-77. When an RTC alert is issued, a potential impact point is displayed on the TAWS-B Page. INDEX APPENDICES ADDITIONAL FEATURES Imminent Terrain Impact (ITI) and Imminent Obstacle Impact (IOI) alerts are issued when the aircraft is below the elevation of a terrain or obstacle cell in the aircraft’s projected path. ITI and IOI alerts are accompanied by a potential impact point displayed on the TAWS-B Page. The alert is annunciated when the projected vertical flight path is calculated to come within minimum clearance altitudes in Figure 6-78. 346 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW Required Terrain Clearance RTC Level (FT) RTC Descending (FT) 800 600 FLIGHT INSTRUMENTS 500 400 300 200 EIS Required Terrain Clearance Required Terrain Clearance (FT) (FT) 700 100 0 5 10 15 20 25 AUDIO PANEL & CNS 0 30 Distance From Runway (NM) Distance From Runway (NM) Figure 6-78 FLTA Alert Minimum Terrain and Obstacle Clearance Values FLIGHT MANAGEMENT FLTA alerts are automatically inhibited when the aircraft is less than 200 feet above the destination runway elevation while within 0.5 nm of the approach runway or the aircraft is between runway ends. HAZARD AVOIDANCE Figure 6-79 TERRAIN-SVS Alerting Disabled (TERRAIN-SVS Inhibited) Annunciation Premature Descent Alerting AFCS A Premature Descent Alert (PDA) is issued when the system detects that the aircraft is significantly below the normal approach path to a runway (Figure 6-80). ADDITIONAL FEATURES PDA alerting begins when the aircraft is within 15 nm of the destination airport and ends when the aircraft is either 0.5 nm from the runway threshold or is at an altitude of 125 feet AGL while within 1.0 nm of the threshold. APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 347 SYSTEM OVERVIEW Hazard Avoidance 800 EIS FLIGHT INSTRUMENTS Height Above Destination (Feet) 700 600 500 400 300 PDA Alerting Area 200 100 15 14 13 12 11 10 9 8 7 6 5 4 3 2 1 0 0 AUDIO PANEL & CNS Distance to Destination (NM) Figure 6-80 PDA Alerting Threshold FLIGHT MANAGEMENT PDA and FLTA aural and visual alerts can be manually inhibited. Discretion should be used when inhibiting TAWS-B and the system should be enabled when appropriate. When TAWS-B is inhibited, the alert annunciation ‘TAWS INH’ is shown on the PFD and MFD (Figure 6-80). HAZARD AVOIDANCE Figure 6-81 TAWS-B Alerting Disabled (TAWS-B Inhibited) Annunciation Inhibiting/enabling TAWS-B alerting: 1) Select the TAWS-B Page. AFCS 2) Press the INHIBIT Softkey to inhibit or enable TAWS-B (choice dependent on current state). Or: a) Press the MENU Key. ADDITIONAL FEATURES b) Select ‘Inhibit TAWS’ or ‘Enable TAWS’ (choice dependent on current state) and press the ENT Key. APPENDICES If TAWS-B 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. Five-Hundred Aural Alert INDEX The purpose of the aural alert message “Five-hundred” is to provide an advisory alert of when the aircraft descends to within 500 feet above the terrain or runway threshold. When the aircraft is within 5 nm of an airport, the “Five Hundred” aural alert is based on the nearest runway threshold elevation. When the aircraft is more than 5 nm of the nearest airport, the “Five Hundred” aural alert is based on the height above terrain as determined by the GPS altitude and terrain database. 348 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW Negative Climb Rate After Takeoff Alert (NCR) FLIGHT INSTRUMENTS The Negative Climb Rate (NCR) After Takeoff alert (also referred to as “Altitude Loss After Takeoff”) provides alerts when the system determines the aircraft is losing altitude (closing upon terrain) after takeoff. The aural message “Don’t Sink” is given for NCR alerts, accompanied by an annunciation and a pop-up terrain alert on the display. NCR alerting is only active when departing from an airport and when the following conditions are met: • Height above the terrain is less than 700 feet • Distance from the departure airport is 5 nm or less EIS • Heading change from the departure heading is less than 110 degrees Figures 6-82 and 6-83 shows the NCR alerting parameters as defined by TSO-C151b based on Altitude Loss and Sink Rate respectively. AUDIO PANEL & CNS 1000 900 700 FLIGHT MANAGEMENT 600 “DON’T SINK” or “TOO LOW, TERRAIN” 500 400 300 HAZARD AVOIDANCE Height Above Terrain (Feet) 800 200 100 0 0 20 40 60 80 100 120 140 Altitude Loss (Feet) AFCS Figure 6-82 Negative Climb Rate (NCR) Altitude Loss 1000 ADDITIONAL FEATURES 900 700 600 “DON’T SINK” or “TOO LOW, TERRAIN” 500 400 300 APPENDICES Height Above Terrain (Feet) 800 200 100 INDEX 0 0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000 5500 6000 6500 7000 Sink Rate (FPM) Figure 6-83 Negative Climb Rate (NCR) Sink Rate 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 349 SYSTEM OVERVIEW Hazard Avoidance System Status FLIGHT INSTRUMENTS During power-up, TAWS-B conducts a self-test of its aural and visual annunciations. The system test can also be manually initiated. A single chime is issued at test completion. TAWS-B System Testing is disabled when ground speed exceeds 30 knots. PFD/MFD Alert TAWS-B Page Annunciation Annunciation Alert Type System Test in Progress System Test Pass None EIS TAWS System Test Fail Aural Message TAWS TEST None None Single Chime TAWS FAIL “TAWS System Failure” AUDIO PANEL & CNS Manually testing the TAWS-B System: FLIGHT MANAGEMENT Table 6-11 TAWS-B System Test Status Annunciations 3) Select ‘Test TAWS System’ and press the ENT Key to confirm the selection. 1) Select the TAWS-B Page. HAZARD AVOIDANCE 2) Press the MENU Key (Figure 6-84). AFCS Figure 6-84 TAWS-B Page Menu INDEX APPENDICES ADDITIONAL FEATURES TAWS-B continually monitors several system-critical items such as database validity, hardware status, and GPS status. If the terrain/obstacle database is not available, the aural message “TAWS System Failure” is generated along with the ‘TAWS FAIL’ alert annunciation. TAWS-B requires a 3-D GPS navigation solution along with specific vertical accuracy minimums. Should the navigation solution become degraded or if the aircraft is out of the database coverage area, the annunciation ‘TAWS N/A’ is generated in the annunciation window and on the TAWS-B Page. The aural message “TAWS Not Available” is generated. When the GPS signal integrity is restored and the aircraft is within the database coverage area, the aural message “TAWS Available” is generated. 350 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW None TAWS FAIL “TAWS System Failure” NO GPS POSITION “TAWS Not Available” “TAWS Available” when GPS position returns. “TAWS Not Available” “TAWS Available” when sufficient GPS signal is received. “TAWS Not Available” “TAWS Available” when aircraft enters database coverage area. Excessively degraded GPS signal None Out of database coverage area None HAZARD AVOIDANCE TERRAIN DATABASE FAILURE FLIGHT MANAGEMENT Aural Message AUDIO PANEL & CNS TAWS-B Page Annunciation EIS MFD Terrain or Obstacle database unavailable or invalid. TAWS operating with PFD Terrain or Obstacle databases Terrain or Obstacle database unavailable or invalid on all displays, invalid software configuration, TAWS audio fault No GPS position PFD/MFD Annunciation None FLIGHT INSTRUMENTS Alert Cause Table 6-12 TAWS-B Abnormal Conditions AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 351 SYSTEM OVERVIEW Hazard Avoidance 6.6 Profile View Terrain FLIGHT INSTRUMENTS The Perspective™ offers a Profile View of terrain and obstacles relative to the aircraft’s current flight path and altitude on the Navigation Map Page of the MFD. Profile View does not provide caution or warning annunciations or voice alerts such as Terrain-SVS or TAWS-B systems, nor does it display potential impact points along the Profile View. It only provides color indications when terrain and obstacles are within a certain altitude threshold from the aircraft. Refer to Figure 6-52 in Table 6-4 in the Terrain Proximity discussion for a list of colors and symbols used in the Profile View. EIS Accessing Profile View: 1) Select the Navigation Map Page. 2) Press the MAP Softkey. AUDIO PANEL & CNS 3) Press the PROFILE Softkey. Or: a) Press the MENU Key. FLIGHT MANAGEMENT b) Select ‘Show Profile View’ or ‘Hide Profile View’ (choice dependent on current state) and press the ENT Key. Enabling/Disabling Profile View Terrain on the Navigation Map (when Profile View is enabled): 1) Select the Navigation Map Page. 2) Press the MAP Softkey. HAZARD AVOIDANCE 3) Press the TERRAIN Softkey. Profile View Display INDEX APPENDICES ADDITIONAL FEATURES AFCS When the Profile View is enabled, it is displayed below the Navigation Map. Altitude is shown along with a vertical scale, next to an aircraft symbol at the current altitude. Distance is represented horizontally along the bottom of the Profile View, and increases from left (present position) to right. 352 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW FLIGHT INSTRUMENTS Profile View Corridor Navigation Map Range EIS Terrain Legend AUDIO PANEL & CNS Terrain Enabled Icons Altitude Scale Profile View Total Distance Distance Scale FLIGHT MANAGEMENT Figure 6-85 Navigation Map Page with Profile View Terrain and Topographic Data Enabled HAZARD AVOIDANCE When the Navigation Map range is adjusted with the RANGE Knob, the horizontal distance of the Profile View is adjusted proportionately to be 1/2 of the Navigation Map range distance down to 1 nm, at which point Profile View is no longer available (‘PROFILE NOT AVAILABLE’ is displayed). Terrain and obstacles in the Profile View correspond to those shown on the Navigation Map. When range is adjusted to remove terrain or obstacles from the Navigation Map, these items are also removed from the Profile View. Approach 0.6 nm Departure 0.6 nm Terminal 2.0 nm Enroute 4.0 nm Oceanic 4.0 nm APPENDICES Profile View Width ADDITIONAL FEATURES Flight Phase AFCS If the Navigation Map range is at or below 75 miles, a white Profile View Corridor is shown on the Navigation Map representing the width of the Profile View based on the current aircraft track (or heading if track is unavailable). The Profile View width is automatically adjusted based on the current phase of flight (Table 6-13). Profile View displays the highest terrain or obstacle on either side of the Profile View width from the aircraft center. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T INDEX Table 6-13 Profile View Width Scale 353 SYSTEM OVERVIEW Hazard Avoidance 6.7 Garmin GTS 800 Traffic FLIGHT INSTRUMENTS WARNING: The GTS 800 Traffic Advisory System (TAS) is intended for advisory use only to aid the pilot in visually acquiring traffic. No avoidance maneuvers should be based solely upon TAS traffic information. It is the responsibility of the pilot in command to see and maneuver to avoid traffic. NOTE: Pilots should be aware of TAS system limitations. TAS systems require transponders of other aircraft AUDIO PANEL & CNS EIS to respond to system interrogations. If the transponders do not respond to interrogations due to phenomena such as antenna shading or marginal transponder performance, traffic may be displayed intermittently, or not at all. Aircraft without altitude reporting capability are shown without altitude separation data or climb descent indication. Pilots should remain vigilant for traffic at all times. NOTE: Aircraft without operating transponders are invisible to TAS. FLIGHT MANAGEMENT The optional Garmin GTS 800 is a Traffic Advisory System (TAS). The system enhances flight crew situational awareness by displaying traffic information for transponder-equipped aircraft. The system also provides visual and aural traffic alerts including voice announcements to assist the pilot in visually acquiring traffic. The GTS 800 is capable of tracking a total of 45 intruding aircraft equipped with Mode A, C, or S transponders. The Perspective™ can display a maximum of 30 aircraft with the highest threat potential simultaneously. HAZARD AVOIDANCE When the system is in Operating Mode, the TAS unit interrogates the transponders of intruding aircraft while monitoring transponder replies. The system uses this information to derive the distance, relative bearing, and if reported, the altitude and vertical trend for each aircraft within its surveillance range. AFCS Theory of operation The system then calculates a closure rate to each intruder based on the projected Closest Point of Approach (CPA). If the closure rate meets the threat criteria for a Traffic Advisory (TA), visual and aural alerting is provided. TAS surveillance VOLUME and Symbology ADDITIONAL FEATURES The GTS 800 surveillance system monitors the airspace within ±10,000 feet of own altitude, and up to 12 nm in the forward direction. Range is somewhat reduced to the sides and aft of own aircraft due to the directional interrogation signal patterns. INDEX APPENDICES When paired with an optional 1090 MHz extended squitter transponder, the GTS 800 uses Automatic Dependent Surveillance - Broadcast (ADS-B) data from participating airborne aircraft transponders to enhance the positional accuracy and display of traffic within the TAS surveillance range. Traffic data supplied only by ADS-B Ground Based Transceivers (GBTs) is not displayed. 354 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW TAS Symbol Description FLIGHT INSTRUMENTS Non-Threat Traffic Proximity Advisory (PA) Traffic Advisory (TA) EIS Traffic Advisory Off Scale AUDIO PANEL & CNS Table 6-14 TAS Symbol Description NOTE: A 1090 MHz extended squitter transponder is required to display ADS-B symbology for aircraft Symbol FLIGHT MANAGEMENT providing ADS-B data. Description Traffic Advisory with ADS-B directional information. Points in the direction of the intruder aircraft track. HAZARD AVOIDANCE Proximity Advisory with ADS-B directional information. Points in the direction of the aircraft track. Non-threat traffic with ADS-B directional information. Points in the direction of the intruder aircraft track. Traffic with ADS-B directional information, but positional accuracy is degraded. Points in the direction of the aircraft track. AFCS Table 6-15 TAS Traffic with ADS-B Symbology ADDITIONAL FEATURES A Traffic Advisory (TA), displayed as a yellow circle or triangle, alerts the crew to a potentially hazardous intruding aircraft, if the closing rate, distance, and vertical separation meet TA criteria. A Traffic Advisory that is beyond the selected display range (off scale) is indicated by a half TA symbol at the edge of the screen at the relative bearing of the intruder. APPENDICES A Proximity Advisory (PA), displayed as a solid white diamond or triangle, indicates the intruding aircraft is within ±1200 feet and is within a 6 nm range, but is still not considered a TA threat. A Non-threat Advisory, shown as an open white diamond or triangle, is displayed for all other traffic beyond 6 nm that is neither a TA or PA. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 355 SYSTEM OVERVIEW Hazard Avoidance Relative altitude, when available, is displayed above or below the corresponding intruder symbol in hundreds of feet. When this altitude is above own aircraft, it is preceded by a ‘+’ symbol; a minus sign ‘-’ indicates traffic is below own aircraft. FLIGHT INSTRUMENTS A vertical trend arrow to the right of the intruder symbol indicates climbing or descending traffic with an upward or downward-pointing arrow respectively . Relative Altitude EIS Vertical trend arrow AUDIO PANEL & CNS Figure 6-86 Intruder Altitude and Vertical Trend Arrow If the intruding aircraft is providing ADS-B track information, this is displayed as a vector line extending beyond the traffic symbol in the direction of the track. FLIGHT MANAGEMENT Vector Line indicates intruder aircraft track HAZARD AVOIDANCE Figure 6-87 Intruder Traffic with ADS-B Directional Information and Track INDEX APPENDICES ADDITIONAL FEATURES AFCS The traffic system automatically suppresses the display of on-ground aircraft equipped with Mode S transponders. 356 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW TA Alerting Conditions Sensitivity Intruder Altitude Level Available B Yes B No HAZARD AVOIDANCE No FLIGHT MANAGEMENT A Intruder closing rate provides less than 20 seconds of vertical and horizontal separation. Or: Intruder closing rate provides less than 20 seconds of horizontal separation and vertical separation is within 600 feet. Or: Intruder range is within 0.2 nm and vertical separation is within 600 feet. Intruder closing rate provides less than 15 seconds of separation. Intruder closing rate provides less than 30 seconds of vertical and horizontal separation. Or: Intruder closing rate provides less than 30 seconds of horizontal separation and vertical separation is within 800 feet. Or: Intruder range is within 0.55 nm and vertical separation is within 800 feet. Intruder range is less than 20 seconds. AUDIO PANEL & CNS Yes TA Alerting Conditions EIS A FLIGHT INSTRUMENTS The traffic system automatically adjusts its TA sensitivity level to reduce the likelihood of nuisance TA alerting during flight phases likely to be near airports. Level A (less) TA sensitivity is used when the aircraft’s groundspeed is below 120 knots or when the flaps are down. In all other conditions while the traffic system is providing surveillance, Level B (greater) TA sensitivity is used to assess TA threats. AFCS Table 6-16 TA Sensitivity Level and TA Alerting Criteria ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 357 SYSTEM OVERVIEW Hazard Avoidance TAS Alerts NOTE: Aural traffic alerts do not occur when the flaps are down. Only visual traffic annunciations are issued FLIGHT INSTRUMENTS under this condition. When the traffic system detects a new TA, the following occur: EIS • A single “Traffic!” voice alert is generated, followed by additional voice information about the bearing, relative altitude, and approximate distance from the intruder that triggered the TA (Table 6-17). The announcement “Traffic! 12 o’clock, high, four miles,” would indicate the traffic is in front of own aircraft, above own altitude, and approximately four nautical miles away. • A TRAFFIC Annunciation appears at the top right of the airspeed on the PFD, flashing for five seconds and remains displayed until no TAs are detected in the area (Figure 6-88). AUDIO PANEL & CNS • The PFD Inset Map is automatically displayed with TA traffic. FLIGHT MANAGEMENT If the bearing of TA traffic cannot be determined (Figures 6-90 and 6-93), a yellow text banner will be displayed in the center of the Traffic Map Page and in the lower-left of the PFD inset map instead of a TA symbol. The text will indicate “TA” followed by the distance, relative altitude, and vertical trend arrow for the TA traffic, if known. AFCS HAZARD AVOIDANCE A TA will be displayed for at least eight seconds, even if the condition(s) that initially triggered the TA are no longer present. ADDITIONAL FEATURES Inset Map Displays When TA is Detected INDEX APPENDICES Figure 6-88 Traffic Annunciation (PFD) Bearing Relative Altitude Distance (nm) “One o’clock” through “Twelve o’clock” or “No Bearing” “High”, “Low”, “Same Altitude” (if within 200 feet of own altitude), or “Altitude not available” “Less than one mile”, “One Mile” through “Ten Miles”, or “More than ten miles” Table 6-17 TA Descriptive Voice Announcements 358 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW System Test NOTE: Traffic surveillance is not provided during the system test. Use caution when performing a system FLIGHT INSTRUMENTS test during flight. The traffic system provides a system test mode to verify the TAS system is operating normally. The test takes ten seconds to complete. When the system test is initiated, a test pattern of traffic symbols is displayed on the Traffic Map Page (Figure 6-89). If the system test passes, the aural announcement “TAS System Test Passed” is heard, otherwise the system announces “TAS System Test Failed.” When the system test is complete, the unit enters Standby Mode. EIS Testing the Traffic System: 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) Turn the Range knob to set the range to 2/6 nm to allow for proper test pattern display. 4) Press the TEST Softkey. FLIGHT MANAGEMENT Or: 1) Press the MENU Key and turn the small FMS knob to select ‘Test Mode’. 2) Press the ENT Key. Operating Mode Non-Threat Traffic at 11 o’clock, Distance 3.6 nm, 1000’ Above, Level HAZARD AVOIDANCE Test Mode Annunciation AFCS Proximity Traffic at 1 o’clock, Distance 3.6 nm, 1000’ Below, Descending ADDITIONAL FEATURES TA at 9 o’clock, Distance 2.0 nm, 200’ Below, Climbing APPENDICES INDEX Figure 6-89 System Test in Progress with Test Pattern 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 359 SYSTEM OVERVIEW Hazard Avoidance Operation NOTE: The traffic unit automatically transitions from STANDBY to OPERATE mode eight seconds after FLIGHT INSTRUMENTS takeoff. The unit also automatically transitions from OPERATE to STANDBY mode 24 seconds after landing. After power-up, the traffic system is in Standby Mode. The traffic unit must be in Operating Mode for traffic to be displayed and for TAs to be issued. EIS Pressing the OPERATE Softkey allows the system to switch from Standby Mode to Operating Mode as necessary. Pressing the STANDBY Softkey forces the unit into Standby Mode. Switching from operating mode to standby mode: AUDIO PANEL & CNS On the Traffic Page, press the STANDBY Softkey Or: 1) Press the MENU Key and turn the small FMS knob to select ‘Standby Mode’. FLIGHT MANAGEMENT 2) Press the ENT Key. Switching from standby mode to operating mode: On the Traffic Page, press the OPERATE Softkey Or: HAZARD AVOIDANCE 1) Press the MENU Key and turn the small FMS knob to select ‘Operate Mode’. INDEX APPENDICES ADDITIONAL FEATURES AFCS 2) Press the ENT Key. The traffic system switches from Standby Mode to Operating Mode as necessary. 360 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW Traffic MAP Page FLIGHT INSTRUMENTS The Traffic Map Page (Figure 6-90) 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 up to 12 mn, as indicated by the map range rings. The traffic mode and altitude display mode are annunciated in the upper left corner of the page. Traffic Mode Altitude Mode EIS Traffic Display Range Traffic Advisory, 500’ Below, Climbing AUDIO PANEL & CNS Non-Threat Traffic, 2500’ Above, Descending “No Bearing” Traffic (Bearing Undetermined), Distance 4.0 nm, 500’ Above, Descending FLIGHT MANAGEMENT Non-Threat ADS-B Traffic with Track, 1000’ Above, Level Traffic Advisory OffScale, 400’ Below, Level Proximity Traffic, 900’ Above, Level, Flight ID Displayed HAZARD AVOIDANCE Non-Threat Traffic, Altitude Not Reported Figure 6-90 Traffic Map Page AFCS Displaying traffic on the Traffic Map Page: 1) Turn the large FMS Knob to select the Map Page Group. ADDITIONAL FEATURES 2) Turn the small FMS Knob to select the Traffic Map Page. 3) Press the OPERATE Softkey to begin displaying traffic. OPERATING is displayed in the Traffic mode field. 4) Press the STANDBY Softkey to place the system in the Standby mode. STANDBY is displayed in the Traffic Mode field. APPENDICES 5) Turn the RANGE Knob clockwise to display a larger area or counter-clockwise to display a smaller area. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 361 SYSTEM OVERVIEW Hazard Avoidance Altitude Display FLIGHT INSTRUMENTS The pilot can select the volume of airspace in which non-threat and proximity traffic is displayed. TAs occurring outside of these limits will always be shown. Changing the altitude range: 1) On the Traffic Map Page, press the ALT MODE Softkey. AUDIO PANEL & CNS EIS 2) Press one of the following Softkeys: • ABOVE: Displays non-threat and proximity traffic from 9000 feet above the aircraft to 2700 feet below the aircraft. Typically used during climb phase of flight. • NORMAL: Displays non-threat and proximity traffic from 2700 feet above the aircraft to 2700 feet below the aircraft. Typically used during enroute phase of flight. • BELOW: Displays non-threat and proximity traffic from 2700 feet above the aircraft to 9000 feet below the aircraft. Typically used during descent phase of flight. • UNREST (unrestricted): All traffic is displayed from 9900 feet above and 9900 feet below the aircraft. FLIGHT MANAGEMENT 3) To return to the Traffic Map Page, press the BACK Softkey. Or: 1) Press the MENU Key. HAZARD AVOIDANCE 2) Turn the small FMS Knob to select one of the following (see Softkey description in previous step 2): • ABOVE • NORMAL • BELOW • UNRESTRICTED AFCS 3) Press the ENT Key. Flight ID Display INDEX APPENDICES ADDITIONAL FEATURES The Flight IDs of other aircraft (when available) can be enabled for display on the Traffic Map Page (Figure 6-91). When a flight ID is received, it will appear above or below the corresponding traffic symbol on the Traffic Map Page when this option is enabled. 362 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW FLIGHT INSTRUMENTS Flight ID EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 6-91 Traffic Map Page with Flight IDs Enabled Enabling/Disabling Flight ID Display: On the Traffic Map Page, press the FLT ID Softkey. Or: HAZARD AVOIDANCE 1) Press the MENU Key. AFCS 2) Turn the small FMS Knob to select ‘Show Flight IDs’ or ‘Hide Flight IDs’ (choice dependent on current state) (Figure 6-92). 3) Press the ENT Key. ADDITIONAL FEATURES APPENDICES Figure 6-92 Traffic Map Page Menu INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 363 SYSTEM OVERVIEW Hazard Avoidance Traffic Map Page Display Range FLIGHT INSTRUMENTS The display range on the Traffic Map Page can be changed at any time. Map range is adjustable with the RANGE Knob, as indicated by the map range rings. Changing the display range on the Traffic Map Page: 1) Turn the RANGE Knob. EIS 2) The following range options are available: • 2 nm • 2 and 6 nm • 6 and 12 nm AUDIO PANEL & CNS Additional Traffic Displays FLIGHT MANAGEMENT Traffic information can be displayed on the following maps on the MFD when the unit is operating: • Navigation Map Page • Nearest Pages • Traffic Map Page • Active Flight Plan Page • Trip Planning Page • System Pages • Video Page HAZARD AVOIDANCE Traffic information can also be displayed on the PFD when the Synthetic Vision System (SVS) option is installed and enabled. See the Additional Features Section for details. Displaying traffic information (MFD maps other than the Traffic Map Page): 1) Press the MAP Softkey. AFCS 2) Press the TRAFFIC Softkey. Traffic is now displayed on the map. When traffic is selected on maps other than the Traffic Map Page, a traffic icon is shown to indicate traffic is enabled for display (Table 6-18). ADDITIONAL FEATURES Displaying traffic on the Navigation Map: NOTE: The Navigation Map Page must be oriented with the desired track up or heading up to display traffic APPENDICES on the Navigation Map Page. Refer to Section 5.2 of Flight Management for details about changing map page orientation. 1) Ensure the TAS system is operating. With the Navigation Map displayed, press the MAP Softkey. INDEX 2) Press the TRAFFIC Softkey. Traffic is now displayed on the map as shown in Figure 6-93. 364 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW FLIGHT INSTRUMENTS Non-Threat Traffic EIS Traffic Advisory AUDIO PANEL & CNS Proximity Traffic TA Off Scale Banner FLIGHT MANAGEMENT Non-Bearing Traffic Advisory Figure 6-93 TAS Traffic on Navigation Map HAZARD AVOIDANCE Customizing the traffic display on the Navigation Map Page: 1) Select the Navigation Map Page. 2) Press the MENU Key. 3) With Map Setup highlighted, press the ENT Key (Figure 6-94). AFCS 4) Turn the small FMS Knob to select the Traffic Group and press the ENT Key (Figure 6-95). 5) Turn the large FMS Knob or press the ENT Key to scroll through the selections (Figure 6-96). • TRAFFIC – Turns the display of traffic data on or off - All Traffic - Displays all traffic - TA/PA - Displays Traffic Advisories and Proximity Advisories - TA ONLY - Displays Traffic Advisories only APPENDICES ADDITIONAL FEATURES • 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 6) Turn the small FMS Knob to scroll through options (ON/OFF, range settings, etc.). 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. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 365 FLIGHT INSTRUMENTS SYSTEM OVERVIEW Hazard Avoidance FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS Figure 6-94 Navigation Map Page Menu Figure 6-95 Navigation Map Page Setup Menu Figure 6-96 Navigation Map Page Setup Menu, Traffic Group HAZARD AVOIDANCE 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. AFCS Traffic information can also be displayed on the PFD Inset Map by pressing the INSET Softkey. A traffic map will appear in heading up orientation. Traffic information can also be overlaid with navigation, topographic and optional XM Weather data. Displaying traffic information (PFD Inset Map): 1) Press the INSET Softkey. ADDITIONAL FEATURES 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). INDEX APPENDICES 4) Press the softkey again to remove traffic data. 366 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW System Status The traffic mode is annunciated in the upper left corner of the Traffic Map Page. TAS System Test Initiated TEST (also shown in white in center of page) TAS Operating OPERATING STANDBY (also shown in white in center of page) TAS Failed* FAIL EIS TAS Standby Traffic Display Status Icon (Other Maps) FLIGHT INSTRUMENTS Traffic Mode Annunciation (Traffic Map Page) Traffic Mode AUDIO PANEL & CNS * See Table 6-19 for additional failure annunciations Table 6-18 TAS Modes Traffic Map Page Annunciation NO DATA 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 If the traffic unit fails, an annunciation as to the cause of the failure is shown in the center of the Traffic Map Page. During a failure condition, the Operating Mode cannot be selected. Table 6-19 TAS Failure Annunciations AFCS The annunciations to indicate the status of traffic information appear in a banner at the lower left corner of maps on which traffic can be displayed. Traffic Status Banner Annunciation TRFC FAIL INDEX NO TRFC DATA 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 APPENDICES TA X.X ± XX ↕ ADDITIONAL FEATURES TA OFF SCALE Description *Shown as symbol on Traffic Map Page **Shown in center of Traffic Map Page Table 6-20 TAS Traffic Status Annunciations 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 367 SYSTEM OVERVIEW Hazard Avoidance 6.8 Avidyne TAS610 Traffic FLIGHT INSTRUMENTS NOTE: Refer to the Avidyne TAS600 Series Pilot’s Operating Handbook for a detailed discussion of the Avidyne TAS610. The TAS610 Traffic Advisory System (TAS) is designed to help in detection and avoidance of other aircraft. TAS uses an on-board interrogator-processor and an altitude reporting transponder for the air-to-air traffic data link. EIS TAS Symbology Traffic is displayed according to TCAS symbology using four different symbols. AUDIO PANEL & CNS TAS Symbol Description Non-Threat Traffic FLIGHT MANAGEMENT Proximity Advisory (PA) Traffic Advisory (TA) HAZARD AVOIDANCE Traffic Advisory Off Scale Table 6-21 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. AFCS 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. ADDITIONAL FEATURES 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. Displaying Traffic Data APPENDICES Traffic information is displayed on the following maps: • PFD Inset Map • Nearest Pages • Navigation Map Page (DTK up or HDG up) • Active Flight Plan Page • Traffic Map Page • AUX - Video Page • Trip Planning Page INDEX Traffic information can also be displayed on the PFD when the Synthetic Vision System (SVS) option is installed and enabled. See the Additional Features Section for details. 368 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW Displaying traffic on the Traffic Map Page: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. FLIGHT INSTRUMENTS 3) Turn the RANGE Knob clockwise to display a larger area or counter-clockwise to display a smaller area. Traffic Mode Altitude Mode Traffic Display Range AUDIO PANEL & CNS Traffic Advisory, 500’ Below, Climbing EIS Non-Threat Traffic, 2500’ Above, Descending “No Bearing” Traffic (Bearing Undetermined), Distance 4.0 nm, 500’ Above, Descending Proximity Traffic, 900’ Above, Level FLIGHT MANAGEMENT Traffic Advisory OffScale, 400’ Below, Level HAZARD AVOIDANCE Non-Threat Traffic, Altitude Not Reported Figure 6-97 Traffic Map Page AFCS 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. ADDITIONAL FEATURES Displaying traffic information (maps other than the Traffic Map Page): 1) Press the MAP Softkey. 2) Press the TRAFFIC Softkey to display traffic data. APPENDICES When traffic is selected on maps other than the Traffic Map Page, a traffic icon is shown to indicate TAS is enabled for display. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 369 SYSTEM OVERVIEW Hazard Avoidance NOTE: The Navigation Map Page must be oriented with desired track up or heading up to display traffic on AUDIO PANEL & CNS Non-Threat Traffic FLIGHT MANAGEMENT EIS FLIGHT INSTRUMENTS the Navigation Map Page. Refer to Section 5.2 of Flight Management for details about changing map page orientation. Proximity Traffic Traffic Advisory TA Off Scale Banner HAZARD AVOIDANCE Non-Bearing Traffic Advisory Figure 6-98 TAS Traffic on Navigation Map AFCS Displaying traffic information (PFD Inset Map): 1) Press the INSET Softkey. 2) Press the TRAFFIC Softkey to display traffic data on the inset map (TRFC-1). ADDITIONAL FEATURES 3) Press the softkey again to display the traffic-only inset (TRFC-2). INDEX APPENDICES 4) Press the softkey again to remove traffic data. 370 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW Altitude Display Changing the altitude display mode: FLIGHT INSTRUMENTS 1) On the Traffic Page, press the ALT MODE Softkey. 2) Press one of the following Softkeys: • BELOW • NORMAL • ABOVE • UNREST (unrestricted) EIS 3) To return to the Traffic Page, press the BACK Softkey. Or: AUDIO PANEL & CNS 1) Press the MENU Key. 2) Turn the small FMS Knob to select one of the following: • BELOW • NORMAL • ABOVE • UNREST (unrestricted) FLIGHT MANAGEMENT HAZARD AVOIDANCE 3) Press the ENT Softkey. Traffic Map Page Display Range The display range on the Traffic Map Page can be changed at any time. Map range is adjustable with the RANGE Knob from 2 to 24 nm, as indicated by the map range rings. AFCS Changing the display range on the Traffic Page: 1) Turn the RANGE Knob. 2) The following range options are available: • 2 and 6 nm • 6 and 12 nm • 12 and 24 nm APPENDICES • 2 nm ADDITIONAL FEATURES 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. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 371 SYSTEM OVERVIEW Hazard Avoidance Customizing the traffic display on the Navigation Map Page: 1) Select the Navigation Map Page. FLIGHT INSTRUMENTS 2) Press the MENU Key. 3) With Map Setup highlighted, press the ENT Key (Figure 6-99). 4) Turn the small FMS Knob to select the Traffic Group and press the ENT Key (Figure 6-100). 5) Turn the large FMS Knob or press the ENT Key to scroll through the selections (Figure 6-101). • TRAFFIC – Turns the display of traffic data on or off AUDIO PANEL & CNS EIS • 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 • 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. AFCS HAZARD AVOIDANCE 8) Press the FMS Knob or CLR Key to return to the Navigation Map Page. APPENDICES ADDITIONAL FEATURES Figure 6-99 Navigation Map Page Menu Figure 6-101 Navigation Map Page Setup Menu, Traffic Group INDEX Figure 6-100 Navigation Map Page Setup Menu 372 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW TAS Alerts NOTE: Refer to the Avidyne TAS600 Series Pilot’s Operating Handbook for information on alerts generated FLIGHT INSTRUMENTS 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. EIS • The PFD Inset Map is automatically displayed with TA traffic. AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Inset Map Displays When TA is Detected Figure 6-102 Traffic Annunciation (PFD) AFCS TAS Voice Alerts To listen to an update of Traffic Advisories press the MUTE Softkey twice. Muting the TAS voice alert in progress: ADDITIONAL FEATURES 1) Select the Traffic Map Page. 2) Press the MUTE Softkey while the voice alert is playing. Subsequent voice alerts will be heard. APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 373 SYSTEM OVERVIEW Hazard Avoidance System Status NOTE: Refer to the Avidyne TAS600 Series Pilot’s Operating Handbook for information on the operating FLIGHT INSTRUMENTS mode. The traffic mode is annunciated in the upper left corner of the Traffic Map Page. Traffic Mode Annunciation (Traffic Map Page) Traffic Mode OPERATING TAS Operating EIS Traffic Display Status Icon (Other Maps) FAIL TAS Failed* AUDIO PANEL & CNS * See Table 6-23 for additional failure annunciations Table 6-22 TAS Modes FLIGHT MANAGEMENT If the unit fails, an annunciation as to the cause of the failure is shown in the center of the Traffic Map Page. Traffic Map Page Annunciation NO DATA HAZARD AVOIDANCE DATA FAILED 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 Table 6-23 TAS Failure Annunciations AFCS 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. ADDITIONAL FEATURES TA OFF SCALE APPENDICES Traffic Status Banner Annunciation TA X.X ± XX ↕ INDEX 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 *Shown as symbol on Traffic Map Page **Shown in center of Traffic Map Page Table 6-24 TAS Traffic Status Annunciations 374 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW 6.9 L-3 Skywatch Traffic FLIGHT INSTRUMENTS NOTE: Refer to the SKYWATCH® (SKY497) Pilot’s Guide for a detailed discussion of the SKY497 TAS. The SKYWATCH Traffic Advisory System (TAS) is designed to help in detection and avoidance of other aircraft. TAS uses an on-board interrogator-processor and an altitude reporting transponder for the air-to-air traffic data link. TAS Symbology EIS Traffic is displayed using four different symbols. TAS Symbol Description AUDIO PANEL & CNS Non-Threat Traffic Proximity Advisory (PA) FLIGHT MANAGEMENT Traffic Advisory (TA) Traffic Advisory Off Scale HAZARD AVOIDANCE Table 6-25 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. AFCS 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. ADDITIONAL FEATURES 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. APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 375 SYSTEM OVERVIEW Hazard Avoidance Operation FLIGHT INSTRUMENTS The unit must be in operating mode for traffic to be displayed. The ability to switch from standby to operating mode on the ground is especially useful for scanning the airspace around the airport before takeoff. Switching from standby mode to operating mode: 1) On the Traffic Page, press the OPERATE Softkey or press the MENU Key and turn the small FMS knob to select Operating Mode. 2) If using the FMS menu, press the ENT Key to place the SKY497 in the operating mode. EIS 3) To switch to Standby Mode from the Traffic Page, press the STANDBY Softkey. Testing the Traffic Advisory System: AUDIO PANEL & CNS 1) Set the range to 2/6 nm to allow for full traffic test pattern display. 2) Press the STANDBY Softkey. 3) Press the TEST Softkey. FLIGHT MANAGEMENT 4) System test takes approximately eight seconds to complete. When completed successfully, traffic symbols display and a voice alert “Traffic Advisory System Test Passed” is heard. If the system test fails, the system reverts to Standby Mode and a voice alert “Traffic Advisory System Test Failed” is heard. Displaying Traffic Data HAZARD AVOIDANCE Traffic information can be displayed on the following maps when the SKY497 unit is operating: • PFD Inset Map • Nearest Pages • Navigation Map Page • Active Flight Plan Page • Traffic Map Page • AUX - Video Page AFCS • Trip Planning Page Traffic information can also be displayed on the PFD when the Synthetic Vision System (SVS) option is installed and enabled. See the Additional Features Section for details. ADDITIONAL FEATURES Displaying traffic on the Traffic Map Page: 1) Turn the large FMS Knob to select the Map Page Group. 2) Turn the small FMS Knob to select the Traffic Map Page. 3) Press the OPERATE Softkey to begin displaying traffic. OPERATING is displayed in the Traffic mode field. APPENDICES 4) Press the ALT MODE Softkey to change the altitude volume. 5) Press the STANDBY Softkey to place the system in the Standby mode. STANDBY is displayed in the Traffic mode field. INDEX 6) Turn the RANGE Knob clockwise to display a larger area or counter-clockwise to display a smaller area. 376 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW Traffic Mode Altitude Mode Traffic Display Range Traffic Advisory, 500’ Below, Climbing EIS “No Bearing” Traffic (Bearing Undetermined), Distance 4.0 nm, 500’ Above, Descending FLIGHT INSTRUMENTS Non-Threat Traffic, 2500’ Above, Descending Proximity Traffic, 900’ Above, Level AUDIO PANEL & CNS Traffic Advisory OffScale, 400’ Below, Level Non-Threat Traffic, Altitude Not Reported FLIGHT MANAGEMENT Figure 6-103 Traffic Map Page HAZARD AVOIDANCE 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 12 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) Press the MAP Softkey. AFCS 2) Press the TRAFFIC Softkey. Traffic is now displayed on the map. When traffic is selected on maps other than the Traffic Map Page, a traffic icon is shown to indicate TAS is enabled for display. ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 377 SYSTEM OVERVIEW Hazard Avoidance NOTE: The Navigation Map Page must be oriented with the desired track up or heading up to display traffic AUDIO PANEL & CNS Non-Threat Traffic FLIGHT MANAGEMENT EIS FLIGHT INSTRUMENTS on the Navigation Map Page. Refer to Section 5.2 of Flight Management for details about changing map page orientation. Proximity Traffic Traffic Advisory TA Off Scale Banner HAZARD AVOIDANCE Non-Bearing Traffic Advisory AFCS Figure 6-104 TAS Traffic on Navigation Map Displaying traffic information (PFD Inset Map): 1) Press the INSET Softkey. ADDITIONAL FEATURES 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. INDEX APPENDICES 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. 378 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW Altitude Display Changing the altitude display mode: FLIGHT INSTRUMENTS 1) On the Traffic Page, press the ALT MODE Softkey. 2) Press one of the following Softkeys: • BELOW • NORMAL • ABOVE • UNREST (unrestricted) EIS 3) To return to the Traffic Page, press the BACK Softkey. Or: AUDIO PANEL & CNS 1) Press the MENU Key. 2) Turn the small FMS Knob to select one of the following: • BELOW • NORMAL • ABOVE • UNREST (unrestricted) FLIGHT MANAGEMENT HAZARD AVOIDANCE 3) Press the ENT Softkey. Traffic Map Page Display Range The display range on the Traffic Map Page can be changed at any time. Map range is adjustable with the RANGE Knob from 2 to 12 nm, as indicated by the map range rings. AFCS Changing the display range on the Traffic Page: 1) Turn the RANGE Knob. 2) The following range options are available: • 2 nm • 2 and 6 nm • 6 and 12 nm ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 379 SYSTEM OVERVIEW Hazard Avoidance Customizing the traffic display on the Navigation Map Page: 1) Select the Navigation Map Page. FLIGHT INSTRUMENTS 2) Press the MENU Key. 3) With Map Setup highlighted, press the ENT Key (Figure 6-105). 4) Turn the small FMS Knob to select the Traffic Group and press the ENT Key (Figure 6-106). 5) Turn the large FMS Knob or press the ENT Key to scroll through the selections (Figure 6-107). • TRAFFIC – Turns the display of traffic data on or off AUDIO PANEL & CNS EIS • 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 • 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. AFCS HAZARD AVOIDANCE 8) Press the FMS Knob or the CLR Key to return to the Navigation Map Page. APPENDICES ADDITIONAL FEATURES Figure 6-105 Navigation Map Page Menu INDEX Figure 6-106 Navigation Map Page Setup Menu 380 Figure 6-107 Navigation Map Page Setup Menu, Traffic Group Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Hazard Avoidance SYSTEM OVERVIEW TAS Alerts NOTE: Refer to the SKY497 documentation for information on alerts generated by the TAS equipment. FLIGHT INSTRUMENTS When the number of TAs on the Traffic Map Page increases from one scan to the next, the following occur: • A “Traffic, Traffic” voice alert is generated. • 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. EIS • The PFD Inset Map is automatically displayed with TA traffic AUDIO PANEL & CNS FLIGHT MANAGEMENT Inset Map Displays When TA is Detected HAZARD AVOIDANCE Figure 6-108 Traffic Annunciation (PFD) System Status Mode Traffic Mode Annunciation (Traffic Map Page) TEST (also shown in white in center of page) TAS Operating OPERATING STANDBY (also shown in white in center of page) TAS Failed* FAIL APPENDICES TAS Standby Traffic Display Status Icon (Other Maps) ADDITIONAL FEATURES TAS System Test Initiated AFCS The traffic mode is annunciated in the upper left corner of the Traffic Map Page. * See Table 6-27 for additional failure annunciations INDEX Table 6-26 TAS Modes 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 381 SYSTEM OVERVIEW Hazard Avoidance If the unit fails, an annunciation as to the cause of the failure is shown in the center of the Traffic Map Page. FLIGHT INSTRUMENTS Traffic Map Page Annunciation NO DATA DATA FAILED 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 EIS Table 6-27 TAS Failure Annunciations AUDIO PANEL & CNS The annunciations to indicate the status of traffic information appear in a banner at the lower left corner of maps on which traffic can be displayed. Traffic Status Banner Annunciation FLIGHT MANAGEMENT TA OFF SCALE HAZARD AVOIDANCE 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 AFCS *Shown as symbol on Traffic Map Page **Shown in center of Traffic Map Page INDEX APPENDICES ADDITIONAL FEATURES Table 6-28 TAS Traffic Status Annunciations 382 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Automatic Flight Control System SYSTEM OVERVIEW Section 7 Automatic Flight Control System FLIGHT INSTRUMENTS Note: The approved Pilot’s Operating Handbook (POH) always supersedes this Pilot’s Guide. 7.1 GFC 700 (Optional) • GSA 80 AFCS Yaw Servo (optional) • GDU 1240A Multi-Function Display (MFD) • GSA 81 AFCS Servos (2) • GIA 63W Integrated Avionics Units (2 IAUs) • GTA 82 Pitch Trim Adapter • GMC 705 AFCS Control Unit • GSM 85 Servo Gearboxes (3) AUDIO PANEL & CNS • GDU 1240A Primary Flight Display (PFD) EIS The GFC 700 is a digital Automatic Flight Control System (AFCS), fully integrated within the Perspective™ System avionics architecture. The System Overview section provides a block diagram to support this system description. GFC 700 AFCS functionality is distributed across the following Line Replaceable Units (LRUs): The GFC 700 AFCS can be divided into these main operating functions: FLIGHT MANAGEMENT • Flight Director (FD) — Flight director operation takes place within either GIA 63W. Flight director commands are displayed on the PFD. The flight director provides: – Command Bars showing pitch/roll guidance – Vertical/lateral mode selection and processing HAZARD AVOIDANCE – Autopilot communication • Autopilot (AP) — Autopilot operation occurs within the pitch, roll, yaw, and pitch trim servos. It also provides servo monitoring and automatic flight control in response to flight director steering commands, Attitude and Heading Reference System (AHRS) attitude and rate information, and airspeed. AFCS • Yaw Damper (YD) — The yaw servo (optional) is self-monitoring and provides Dutch roll damping and turn coordination in response to yaw rate, roll angle, lateral acceleration, and airspeed. • Manual Electric Trim (MET) — The pitch trim adapter provides manual electric pitch trim capability when the autopilot is not engaged and provides directional trim during climbs and descents. ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 383 SYSTEM OVERVIEW Automatic Flight Control System GFC 700 Controls The GFC 700 AFCS Control Unit is positioned below the GCU 478, and has the following controls: FLIGHT INSTRUMENTS 1 2 3 4 HDG Key NAV Key Selects/deselects Heading Select Mode AP Key LVL Key Engages/disengages the autopilot Engages the autopilot (if the autopilot is disengaged and the aircraft is within the autopilot engagement limitations) in level vertical and lateral modes Adjusts the vertical mode reference in Pitch Hold, Vertical Speed, Indicated Airspeed, and Altitude Hold modes Selects/deselects Indicated Airspeed Mode Selects/deselects Altitude Hold Mode Selects/deselects Vertical Path Tracking Mode for Vertical Navigation flight control Selects/deselects Vertical Speed Mode Engages/disengages the yaw damper Activates/deactivates the flight director only Pressing once turns on the director in the default vertical and lateral modes. Pressing again deactivates the flight director and removes the Command Bars. If the autopilot is engaged, the key is disabled. Selects/deselects Approach Mode NOSE UP/DN Wheel 6 IAS Key 7 ALT Key 8 VNV Key 9 VS Key 10 YD Key 11 FD Key FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 5 HAZARD AVOIDANCE 12 APR Key Selects/deselects Navigation Mode 2 3 4 12 11 10 5 6 7 9 8 ADDITIONAL FEATURES AFCS 1 INDEX APPENDICES Figure 7-1 GMC 705 AFCS Control Unit 384 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Automatic Flight Control System SYSTEM OVERVIEW The following GFC 700 AFCS controls are located separately from the GFC 700 AFCS Control Unit: GA Button (Go Around) Disengages the autopilot, yaw damper, and interrupts pitch trim operation An AP DISC Button is located on the pilot’s control stick. FLIGHT INSTRUMENTS AP DISC Button (Autopilot Disconnect) This button may be used to acknowledge an autopilot disconnect alert and mute the associated aural tone. Selects flight director Takeoff (on ground) or Go Around (in air) Mode EIS 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 power lever. Used to command manual electric pitch trim AUDIO PANEL & CNS MET Switch (Manual Electric An MET Switch is located on the pilot and copilot control stick. Trim) Press DN (forward) and UP (rearward) for manual electric trim. The MET Switch may be used to acknowledge an autopilot disconnect alert and mute the associated aural tone. FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 385 SYSTEM OVERVIEW Automatic Flight Control System 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 active, the aircraft can be hand-flown to follow the path shown by the Command Bars. Maximum commanded pitch (-15°, +20°) and roll (25°) 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 Lateral Roll Hold (default) Roll Hold (default) Takeoff (on ground) Go Around (in air) Roll Hold (default) Roll Hold (default) ROL ROL TO GA ROL ROL VNV Key Roll Hold (default) ROL FD Key AP Key AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT GA Button ADDITIONAL FEATURES Modes Selected NAV Key Navigation** APR Key Approach** HDG Key LVL Key Heading Select Level Hold GPS VOR LOC BC GPS VOR LOC HDG LVL Vertical Pitch Hold (default) Pitch Hold (default) Takeoff (on ground) Go Around (in air) Altitude Hold Vertical Speed Vertical Path Tracking* PIT PIT TO GA ALT VS VPTH Pitch Hold (default) PIT Pitch Hold (default) PIT Pitch Hold (default) Level Hold PIT LVL *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 386 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Automatic Flight Control System SYSTEM OVERVIEW AFCS Status Box Lateral Modes Active Vertical Modes Active Mode Reference EIS Armed Autopilot Yaw Damper Status Status FLIGHT INSTRUMENTS Flight director mode annunciations are displayed on the PFD when the flight director is active. Flight director selection and autopilot and yaw damper statuses are shown in the center of the AFCS Status Box. Lateral flight director modes are displayed on the left and vertical on the right. Armed modes are displayed in white and active in green. Armed AFCS Status Box AUDIO PANEL & CNS Selected Altitude AFCS Status Annunciation FLIGHT MANAGEMENT Command Bars HAZARD AVOIDANCE GPS is Selected Navigation Source AFCS Figure 7-2 PFD AFCS Display ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 387 SYSTEM OVERVIEW Automatic Flight Control System Flight Director Modes FLIGHT INSTRUMENTS Flight director modes are normally selected independently for the pitch and roll axes. Unless otherwise specified, all mode keys are alternate action (i.e., press on, press off). In the absence of specific mode selection, the flight director reverts to the default pitch and/or roll modes. 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. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 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, SBAS) required to compute commands. When such a loss occurs, the system automatically begins to roll the wings level (enters Roll Hold Mode) or maintain the pitch angle (enters Pitch Hold Mode), depending on the affected axis. The flashing annunciation stops when the affected mode key is pressed or another mode for the axis is selected. If after 10 seconds no action is taken, the flashing annunciation stops. Figure 7-3 Loss of VOR Signal The flight director is automatically disabled if the attitude information required to compute the default flight director modes becomes invalid or unavailable. HAZARD AVOIDANCE Command Bars AFCS Upon activation of the flight director, Command Bars are displayed in magenta on the PFD. If the aircraft is being flown by hand, the command bars are displayed hollow (Figure 7-4). The Command Bars do not override the Aircraft Symbol. The Command Bars move together vertically to indicate pitch commands and bank left or right to indicate roll commands. Command Bars (Autopilot Engaged) ADDITIONAL FEATURES Command Bars Command Bars (Pilot Hand Flying Aircraft) Aircraft Symbol APPENDICES Figure 7-4 Command Bars INDEX If the attitude information being sent to the flight director becomes invalid or unavailable, the Command Bars are removed from the display. 388 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Automatic Flight Control System SYSTEM OVERVIEW Vertical Modes Vertical Mode Indicated Airspeed (IAS) Captures and tracks descent legs of an active vertical profile VNV Target Altitude Capture Glideslope Go Around 10 ft VS Key VS nnnn fpm -3000 to +1500 fpm 100 fpm IAS Key IAS nnn kt 80 to 185 kt 1 kt VNV Key Captures the Vertical Navigation ** (VNV) Target Altitude Captures and tracks the SBAS glidepath on approach APR Key Captures and tracks the ILS glideslope on approach Commands a constant pitch angle and wings level on ground in GA preparation for takeoff Button Commands a constant pitch angle and wings level in the air VPTH ALTV GP GS TO 7° GA 7° ADDITIONAL FEATURES Takeoff ± 150 ft * ALTS ALT Key ALT nnnnn ft AFCS Glidepath 0.5° HAZARD AVOIDANCE Vertical Path Tracking (If equipped) -15° to +20° PIT FLIGHT MANAGEMENT Vertical Speed (default) AUDIO PANEL & CNS Selected Altitude Capture Altitude Hold Holds the current aircraft pitch attitude; may be used to climb/ descend to the Selected Altitude Captures the Selected Altitude Holds the current Altitude Reference Maintains the current aircraft vertical speed; may be used to climb/descend to the Selected Altitude Maintains the current aircraft airspeed in IAS while the aircraft is climbing/descending to the Selected Altitude Reference Change Increment EIS Pitch Hold Description Reference Control Annunciation Range 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 Indicated Airspeed modes. The NOSE UP/DN Wheel can be used to change the vertical mode reference while operating under Pitch Hold, Vertical Speed, Indicated Airspeed, or Altitude Hold modes. Increments of change and acceptable ranges of values for each of these references using the NOSE UP/DN Wheel are also listed in the table. APPENDICES * ALTS armed automatically when PIT, VS, IAS, or GA active, and under VPTH when Selected Altitude is to be captured instead of VNV Target Altitude ** ALTV armed automatically under VPTH when VNV Target Altitude is to be captured instead of Selected Altitude Table 7-2 Flight Director Vertical Modes INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 389 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 vertical mode by the green ‘PIT’ annunciation. This mode may be used for climb or descent to the Selected Altitude (shown above the Altimeter), since Selected Altitude Capture Mode is automatically armed when Pitch Hold Mode is activated. In Pitch Hold Mode, the flight director maintains a constant pitch attitude. The pitch reference 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. EIS Changing the Pitch Reference AUDIO PANEL & CNS When operating in Pitch Hold Mode, the pitch reference can be adjusted by using the NOSE UP/DN Wheel. FLIGHT MANAGEMENT Pitch Hold Mode Active Selected Altitude Capture Mode Armed AFCS HAZARD AVOIDANCE Selected Altitude Command Bars Maintain Desired Pitch Reference INDEX APPENDICES ADDITIONAL FEATURES Figure 7-5 Pitch Hold Mode 390 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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) • Indicated Airspeed FLIGHT INSTRUMENTS • Pitch Hold EIS The white ‘ALTS’ annunciation indicates Selected Altitude Capture Mode is armed (see Figure 7-5 for example). The ALT SEL Knob is used to set the Selected Altitude (shown above the Altimeter) until Selected Altitude Capture Mode becomes active. 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 reference altitude. 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. Altitude Reference (in this case, equal to Selected Altitude) HAZARD AVOIDANCE Flash up to 10 sec, Indicating Automatic Transition AFCS Figure 7-6 Automatic Mode Transitions During Altitude Capture Changing the Selected Altitude ADDITIONAL FEATURES Use of the ALT SEL Knob to change the Selected Altitude while Selected Altitude Capture Mode is active causes the flight director to revert to Pitch Hold Mode with Selected Altitude Capture Mode armed for the new Selected Altitude. APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 391 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 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 AUDIO PANEL & CNS When operating in Altitude Hold Mode, the reference altitude can be adjusted by using the NOSE UP/DN Wheel. The reference altitude can only be moved a maximum of 150 ft from the current aircraft altitude; each click changes the reference altitude by 10 ft. NOTE: Turning the ALT SEL Knob while in Altitude Hold Mode changes the Selected Altitude, but not the FLIGHT MANAGEMENT flight director’s Altitude Reference, and does not cancel the mode. HAZARD AVOIDANCE Altitude Hold Mode Active Altitude Reference 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 392 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 Vertical Speed Mode Active Vertical Speed Reference Selected Altitude Capture Mode Armed FLIGHT MANAGEMENT Selected Altitude 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/DN Wheel. Vertical Speed Reference HAZARD AVOIDANCE Vertical Speed Reference Bug AFCS Command Bars Indicate Climb to Attain Vertical Speed Reference ADDITIONAL FEATURES Figure 7-8 Vertical Speed Hold Mode APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 393 SYSTEM OVERVIEW Automatic Flight Control System Indicated Airspeed Mode (IAS) NOTE: The Selected Altitude should be set before selecting Indicated Airspeed Mode (IAS). FLIGHT INSTRUMENTS Indicated Airspeed Mode is selected by pressing the IAS Key. This mode acquires and maintains the Airspeed Reference (IAS) while climbing or descending to the Selected Altitude (shown above the Altimeter). When Indicated Airspeed Mode is active, the flight director continuously monitors Selected Altitude, airspeed and altitude. EIS The Airspeed Reference is set to the current airspeed upon mode activation. Indicated Airspeed Mode is indicated by a green ‘IAS’ 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. 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. Changing the Airspeed Reference FLIGHT MANAGEMENT The Airspeed Reference (shown in both the AFCS Status Box and above the Airspeed Indicator) may be adjusted by using the NOSE UP/DN Wheel. HAZARD AVOIDANCE Indicated Airspeed Mode Active Selected Airspeed Altitude Capture Reference Mode Armed Selected Altitude AFCS Airspeed Reference ADDITIONAL FEATURES Airspeed Reference Bug Command Bars Indicate Climb To Attain Selected Altitude INDEX APPENDICES Figure 7-9 Indicated Airspeed Mode (IAS) 394 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 vertical mode key is pressed while Vertical Path Tracking Mode is selected, Vertical Path AFCS Tracking Mode reverts to armed. ADDITIONAL FEATURES 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. APPENDICES Figure 7-10 Vertical Path Tracking Armed Annunciations INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 395 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 five minutes of descent path interception by: FLIGHT INSTRUMENTS • Pressing the VNV Key • Adjusting the Selected Altitude EIS If acknowledgment is not received within one minute of descent path interception, the white ‘VPTH’ annunciation starts to flash. Flashing continues until acknowledged or the descent path is intercepted. If the descent is not confirmed by the time of interception, Vertical Path Tracking Mode remains armed and the descent is not captured. AUDIO PANEL & CNS In conjunction with the “TOD [top of descent] within 1 minute” annunciation in the PFD Navigation Status Box and the “Vertical track” voice message, VNV indications (VNV Target Altitude, vertical deviation, and vertical speed required) appear on the PFD in magenta (Figure 7-11). FLIGHT MANAGEMENT Altitude Hold Mode Active Vertical Path Tracking Armed, (Flashing Indicates Acknowledgment Required) HAZARD AVOIDANCE Selected Altitude AFCS Vertical Deviation Indicator ADDITIONAL FEATURES GPS is Selected Navigation Source VNV Target Altitude Required Vertical Speed Bug Terminal Phase of Flight INDEX APPENDICES Figure 7-11 Vertical Path Capture 396 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 (Figure 7-12). An altitude capture mode (‘ALTS’ or ‘ALTV’) is armed as appropriate. VNV Target Altitude Capture Armed FLIGHT INSTRUMENTS Vertical Path Tracking Active EIS VNV Target Altitude AUDIO PANEL & CNS Required Vertical Speed Indication Terminal Phase of Flight FLIGHT MANAGEMENT GPS is Selected Navigation Source Command Bars Indicate Descent to Maintain Required Vertical Speed HAZARD AVOIDANCE Vertical Deviation Indicator (VDI) Figure 7-12 Vertical Path Tracking Mode AFCS If the altimeter barometric setting is adjusted while Vertical Path Tracking is active, the flight director increases/decreases the descent rate by up to 500 fpm to re-establish the aircraft on the descent path (without commanding a climb). Adjusting the altimeter barometric setting creates discontinuities in VNV vertical deviation, moving the descent path. For large adjustments, it may take several minutes for the AFCS 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 397 SYSTEM OVERVIEW Automatic Flight Control System Automatic Reversion to Pitch Hold Mode Several situations can occur while Vertical Path Tracking Mode is active which cause the flight director to revert to Pitch Hold Mode: FLIGHT INSTRUMENTS • Vertical deviation exceeds 200 feet during an overspeed condition. • 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 Indicated Airspeed modes can also be used to fly non-path descents while VNV flight control is selected. If the VS or IAS 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 Indicated Airspeed Mode 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. 398 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 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). INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 399 SYSTEM OVERVIEW Automatic Flight Control System Glidepath Mode (GP) FLIGHT INSTRUMENTS Glidepath Mode is used to track the SBAS-based glidepath. When Glidepath Mode is armed, ‘GP’ is annunciated in white in the AFCS Status Box. Selecting Glidepath Mode: 1) Ensure a GPS approach 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). EIS 2) Ensure that GPS is the selected navigation source (use the CDI Softkey to cycle through navigation sources if necessary). 3) Press the APR Key. NOTE: Some RNAV (GPS) approaches provide a vertical descent angle as an aid in flying a stabilized AUDIO PANEL & CNS 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. FLIGHT MANAGEMENT WARNING: When flying an LNAV approach (with vertical descent angle) with the autopilot coupled, the aircraft will not level off at the MDA even if the MDA is set in the altitude preselect. HAZARD AVOIDANCE 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: AFCS • 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 ADDITIONAL FEATURES • Automatic sequencing of waypoints has not been suspended (no ‘SUSP’ annunciation on the HSI) 400 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Automatic Flight Control System LNAV/VNAV Approach Active Command Bars Indicate Descent on Glidepath FLIGHT INSTRUMENTS Glidepath Mode Active SYSTEM OVERVIEW GPS Approach Mode Active EIS Glidepath Indicator FLIGHT MANAGEMENT Figure 7-16 Glidepath Mode AUDIO PANEL & CNS GPS is Selected Navigation Source HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 401 SYSTEM OVERVIEW Automatic Flight Control System Glideslope Mode (GS) FLIGHT INSTRUMENTS 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: 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). EIS 3) Press the APR Key. 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. FLIGHT MANAGEMENT 4) Press the APR Key. Figure 7-17 Glideslope Mode Armed HAZARD AVOIDANCE 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 NAV2 (localizer) is Selected Navigation Source Command Bars Indicate Descent On Localizer/ Glideslope Path Glideslope Indicator INDEX Figure 7-18 Glideslope Mode 402 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Automatic Flight Control System SYSTEM OVERVIEW Go Around (GA) and Takeoff (TO) Modes FLIGHT INSTRUMENTS Go Around and Takeoff modes are coupled pitch and roll modes and are annunciated as both the vertical and lateral modes when active. In these modes, the flight director commands a constant set pitch attitude and keeps the wings level. The GA Switch is used to activate both modes. The mode entered by the flight director depends on whether the aircraft is on the ground or in the air. Takeoff Mode provides an attitude reference during rotation and takeoff. This mode can be selected only while on the ground by pushing the GA Switch. The flight director Command Bars assume a wings-level, pitch-up attitude. EIS Pressing the GA Button while in the air activates the flight director in a wings-level, pitch-up attitude, allowing the execution of a missed approach or a go around. Go Around Mode arms Selected Altitude Capture Mode automatically, and attempts to modify the aircraft attitude (i.e., with the NOSE UP/DN Wheel) result in reversion to Pitch and Roll Hold modes. AUDIO PANEL & CNS Go Around Mode Active FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS Command Bars Indicate Climb ADDITIONAL FEATURES Takeoff Mode Active APPENDICES Figure 7-19 Go Around and Takeoff Modes INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 403 SYSTEM OVERVIEW Automatic Flight Control System Lateral Modes FLIGHT INSTRUMENTS The following table relates each GFC 700 lateral mode to its respective control and annunciation. Refer to the vertical modes section for information regarding Takeoff and Go Around Modes. NOTE: The GFC 700 may generate a lower bank angle than the maximum roll command limit in degrees indicated in Table 7-3 by the amount needed to produce a turn rate equal to or less than standard rate. Lateral Mode Control Annunciation EIS Holds the current aircraft roll attitude or rolls the wings level, (default) depending on the commanded bank angle Captures and tracks the Selected HDG Heading Key Roll Hold AUDIO PANEL & CNS Description Heading Select Navigation, GPS FLIGHT MANAGEMENT Navigation, VOR Enroute Capture/Track Navigation, LOC Capture/Track (No Glideslope) HAZARD AVOIDANCE Navigation, Backcourse Capture/Track Captures and tracks the selected navigation source (GPS, VOR, LOC) Captures and tracks a localizer signal for backcourse approaches AFCS Approach, LOC Capture/Track (Glideslope Mode automatically armed) ADDITIONAL FEATURES HDG 25° GPS 25° 25° Capture 10° Track 25° Capture 10° Track LOC GPS Approach, VOR Capture/Track Go Around 25° BC Approach, GPS Takeoff ROL VOR NAV Key Captures and tracks the selected navigation source (GPS, VOR, APR Key LOC) Commands a constant pitch angle and wings level on ground in preparation for takeoff Commands a constant pitch angle and wings level in the air GA Button Maximum Roll Command Limit VAPP LOC 25° Capture 10° Track 25° 25° Capture 10° Track 25° Capture 10° Track TO Wings Level GA Wings Level The GFC 700 limits turn rate to 3 degrees per second (standard rate turn). INDEX APPENDICES Table 7-3 Flight Director Lateral Modes 404 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 or switched, Roll Hold Mode is selected by default. This mode is annunciated as ‘ROL’ in the AFCS Status Box. The current aircraft bank angle is held, subject to the bank angle condition. EIS Figure 7-20 Roll Hold Mode Annunciation AUDIO PANEL & CNS Flight Director Response Rolls wings level Maintains current aircraft roll attitude Limits bank to 25° FLIGHT MANAGEMENT Bank Angle < 6° 6 to 25° >25° Table 7-4 Roll Hold Mode Responses HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 405 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. AUDIO PANEL & CNS EIS The Selected Heading is adjusted using the HDG Knob. Turns are commanded in the same direction as Selected Heading Bug movement, even if the bug is turned more than 180° from the present heading (e.g., a 270° turn to the right). However, Selected Heading changes of more than 330° at a time result in turn reversals. Pitch Hold Mode Active AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT Heading Select Mode Active ADDITIONAL FEATURES Selected Heading Selected Heading Bug Command Bars Track Selected Heading INDEX APPENDICES Figure 7-21 Heading Select Mode 406 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 vertical guidance 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 (Figure 7-24). 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 ADDITIONAL FEATURES 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. 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 407 SYSTEM OVERVIEW Automatic Flight Control System Changing the Selected Course FLIGHT INSTRUMENTS If the navigation source is VOR or localizer, or OBS Mode has been enabled when using GPS, the Selected Course is controlled using the CRS Knob. Pitch Hold Mode Active FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS GPS Navigation Mode Active HAZARD AVOIDANCE GPS is Selected Navigation Source Selected Course Command Bars Indicate Right Turn to Track GPS Course and Climb to Intercept Selected Altitude Figure 7-23 Navigation Mode Pitch Hold Mode Active APPENDICES ADDITIONAL FEATURES AFCS Backcourse Mode Active LOC2 is Selected Navigation Source Command Bars Hold Pitch Attitude INDEX Figure 7-24 Backcourse Mode 408 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 the 1 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). FLIGHT MANAGEMENT 3) Press the APR Key. 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 409 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 If the navigation source is VOR or localizer, or OBS Mode has been enabled when using GPS, the Selected Course is controlled using the CRS Knob. Level Mode NOTE: Pressing the LVL Key will NOT engage the autopilot while the Stall Warning System is activated. ADDITIONAL FEATURES Likewise, the autopilot will disengage if the Stall Warning System is activated while in LVL mode. INDEX APPENDICES Level Mode is coupled pitch and roll modes and is annunciated as both the vertical and lateral modes when active. Pressing the LVL Key engages the autopilot (if the autopilot is disengaged and the aircraft is within the autopilot engagement limitations) in level vertical and lateral modes. Level Mode does not track altitude or heading. When the LVL Key is pressed all armed and active modes are cancelled and the autopilot and flight director revert to LVL mode for pitch and roll (Figure 7-26). While in level mode, all other modes are available by pressing the corresponding button. 410 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Automatic Flight Control System SYSTEM OVERVIEW Pitch Roll FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS Command Bars Indicate Level with the Horizon Figure 7-26 Level Mode Annunciation FLIGHT MANAGEMENT Intercepting and Flying A DME Arc HAZARD AVOIDANCE 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. AFCS 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. ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 411 SYSTEM OVERVIEW Automatic Flight Control System Autopilot and Yaw Damper Operation FLIGHT INSTRUMENTS The autopilot and optional yaw damper (not available in the SR20) operate the flight control surface servos to provide automatic flight control. The autopilot controls the aircraft pitch and roll attitudes following commands received from the flight director. Pitch autotrim provides trim commands to the pitch trim servo to relieve any sustained effort required by the pitch servo. Autopilot operation is independent of the yaw damper. EIS NOTE: Refer to the POH for specific instructions regarding emergency procedures. The yaw damper reduces Dutch roll tendencies, coordinates turns, and provides a steady force to maintain directional trim. It can operate independently of the autopilot and may be used during normal hand-flight maneuvers. Yaw rate commands are limited to 6 deg/sec by the yaw damper. Flight Control AUDIO PANEL & CNS Pitch and roll commands are provided to the servos based on the active flight director modes. Yaw commands are provided by the yaw servo. 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. FLIGHT MANAGEMENT Pitch Axis and Trim HAZARD AVOIDANCE The autopilot pitch axis uses pitch rate to stabilize the aircraft pitch attitude during 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. When the autopilot is not engaged, the pitch trim adapter may be used to provide manual electric trim (MET). This allows the aircraft to be trimmed using a control stick switch. Manual trim commands are generated only when the MET Switch are pressed. Trim speeds are scheduled with airspeed to provide more consistent response. AFCS NOTE: When the autopilot is engaged, the MET Switch does not respond. Roll Axis ADDITIONAL FEATURES The autopilot roll axis uses roll rate to stabilize aircraft roll attitude during 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. APPENDICES Yaw Axis INDEX 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 and reduce or eliminate the need for the pilot to use rudder pedal force to maintain coordinated flight during climbs and descents. 412 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Automatic Flight Control System SYSTEM OVERVIEW Engagement Autopilot Engaged FLIGHT INSTRUMENTS When the AP Key is pressed, the autopilot, yaw damper, and flight director (if not already active) are activated. The flight director engages in Pitch and Roll Hold Modes when initially activated. When the YD Key is pressed, the system engages the yaw damper independently of the autopilot (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. Yaw Damper Engaged EIS Figure 7-27 Autopilot and Yaw Damper Engaged AUDIO PANEL & CNS Disengagement NOTE: The autopilot does not disengage when the MET Switch is pressed. FLIGHT MANAGEMENT Pushing the AP Key on the AFCS Control Panel disengages the autopilot. Manual autopilot disengagement is indicated by a five-second flashing yellow ‘AP’ annunciation and a three-second autopilot disconnect aural alert. HAZARD AVOIDANCE Figure 7-28 Manual Autopilot Disengagement AFCS Pushing the AP DISC button disengages the autopilot, yaw damper, and flight director. Pushing the YD Key disengages the yaw damper and the autopilot. When the yaw damper and autopilot are manually disengaged, both the ‘AP’ and ‘YD’ annunciation turn yellow and flash for 5 seconds and a three-second autopilot disconnect aural alert is generated. ADDITIONAL FEATURES Figure 7-29 Autopilot and Yaw Damper Disengagement After manual disengagement, the autopilot disconnect aural alert and the flashing ‘AP’ annunciation may be cancelled by pushing the AP DISC Button. • System failure • Invalid sensor data APPENDICES Automatic autopilot disengagement is indicated by a flashing red and white ‘AP’ annunciation and by the autopilot disconnect aural alert, which continue until acknowledged by pushing the AP DISC Button. Automatic autopilot disengagement occurs due to: • Inability to compute default flight director modes (FD also disengages automatically) INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 413 SYSTEM OVERVIEW Automatic Flight Control System FLIGHT INSTRUMENTS Yaw damper disengagement is indicated by a five-second flashing yellow ‘YD’ annunciation. Automatic yaw damper disengagement occurs when autopilot disengagement is caused by failure in a parameter also affecting the yaw damper. This means the yaw damper can remain operational in some cases where the autopilot automatically disengages. A localized failure in the yaw damper system or invalid sensor data also cause yaw damper disengagement. Figure 7-30 Automatic Autopilot and Yaw Damper Disengagement EIS Reversionary Mode AUDIO PANEL & CNS In the event of a PFD failure, the MFD goes into reversionary mode. The autopilot remains engaged but reverts to pitch hold and roll hold modes; all other modes are available for selection. If the MFD fails, the PFD goes into reversionary mode and the autopilot continues to function. Miscompare HAZARD AVOIDANCE FLIGHT MANAGEMENT Critical values generated by redundant sensors are monitored by comparators. If differences in the sensors exceed a specified amount, the Comparator Window appears in the upper right corner of the PFD and the discrepancy is annunciated in the Comparator Window as a ‘MISCOMP’ (miscompare). If one or both of the sensed values are unavailable, it will be annunciated as a ‘NO COMP’ (no compare). Figure 7-31 Comparator Window ADDITIONAL FEATURES AFCS Reversionary sensor selection is annunciated in a window on the right side of the PFD (SR22 only). These annunciations reflect reversionary sensors selected on the PFD. Pressing the SENSOR Softkey accesses the ADC1, ADC2, AHRS1, and AHRS2 softkeys. These softkeys allow switching of the sensors being viewed on the PFD. The GPS sensor cannot be switched manually. Figure 7-32 Reversionary Sensor Window APPENDICES If an ‘AP MISCOMP’ annunciation is displayed in the comparator window the IAU will select the operating AHRS and the following message (e.g., ‘USING AHRS2’) appears in the reversionary sensor window. When the ‘AP MISCOMP’ annunciation disappears, the pilot must then select the AHRS being used by the IAU (in this case AHRS2) and re-engage the autopilot. If AHRS1 is selected as the operating AHRS no annunciation will appear in the reversionary sensor window and the pilot can re-engage the autopilot. INDEX If a miscompare occurs between ADC1 and ADC2 the autopilot does not disengage and the IAU automatically switches to the operating ADC. 414 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Automatic Flight Control System SYSTEM OVERVIEW Example Flight Plan Note: The following example flight plan and diagrams (not to be used for navigation) in this section are FLIGHT INSTRUMENTS for instructional purposes only and should be considered not current. Numbered portions of accompanying diagrams correspond to numbered procedure steps. This scenario-based set of procedures (based on the example flight plan found in the Flight Management Section) shows various 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. EIS 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. 30 3 30 27 HAZARD AVOIDANCE 27 30 24 24 21 27 24 27 15 12 21 18 15 18 9 24 21 12 6 Lamar VOR (LAA) Topeka VOR (TOP) 12 Hays VOR (HYS) 9 V 244 Salina VOR (SLN) 9 3 V4 18 V 244 9 6 0 33 15 6 KCOS KMKC 30 3 6 0 33 3 FLIGHT MANAGEMENT 33 AUDIO PANEL & CNS 0 33 0 12 21 15 18 Figure 7-33 Flight Plan Overview AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 415 SYSTEM OVERVIEW Automatic Flight Control System Departure Climbing to the Selected Altitude and flying an assigned heading: FLIGHT INSTRUMENTS 1) Before takeoff: a) Use the ALT SEL Knob to set the Selected Altitude to 12,000 feet. EIS b) Push the GA Switch to activate Takeoff Mode. The flight director Command Bars establish a pitch up attitude to follow. AUDIO PANEL & CNS c) Press the AP Key to engage the autopilot in a climb, holding the pitch angle commanded in Takeoff Mode and wings level. FLIGHT MANAGEMENT 2) In this example, Vertical Speed Mode is used to capture the Selected Altitude (Pitch Hold, Vertical Speed, or Indicated Airspeed Mode may be used). a) Press the VS Key to activate Vertical Speed Mode. HAZARD AVOIDANCE The Vertical Speed Reference may be adjusted after Vertical Speed Mode is selected using the NOSE UP/DN Wheel. 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. AFCS ADDITIONAL FEATURES 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. 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. INDEX APPENDICES 416 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Automatic Flight Control System SYSTEM OVERVIEW FLIGHT INSTRUMENTS HD GM od e EIS AUDIO PANEL & CNS TO M ode 3 Selected Altitude of 12,000 MSL ALT Mode 4 1 2 VS FLIGHT MANAGEMENT KMKC e Mod ode M TO HAZARD AVOIDANCE Figure 7-34 Departure AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 417 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 the desired value, 255°. Note that at this point, the flight director is still in Heading Select Mode and the autopilot continues to fly the Selected Heading, 290°. FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE d) Press the NAV Key. This arms VOR Navigation Mode and the white ‘VOR’ annunciation appears to the left of the active lateral mode. 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 7-35 Intercepting a VOR Radial 418 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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: 1) Transition from VOR to GPS Navigation Mode: EIS 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 2 12 15 21 18 12 AFCS 24 9 Hays VOR (HYS) Salina VOR (SLN) V 244 1 24 27 076 e 9 o 260 o d AV Mo VOR N 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 7-36 Transition to GPS Flight Plan APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 419 SYSTEM OVERVIEW Automatic Flight Control System Descent While flying the arrival procedure, the aircraft is cleared for descent in preparation for the approach to KCOS. Three methods are presented for descent: FLIGHT INSTRUMENTS • Indicated Airspeed descent – Indicated Airspeed Mode can be used to descend to the Selected Altitude at a constant airspeed. This descent method does not account for flight plan waypoint altitude constraints. • Vertical Path Tracking descent – Vertical Path Tracking Mode is used to follow the vertical descent path defined in the GPS flight plan. Altitude constraints correspond to waypoints in the flight plan. Before VNV flight control can provide vertical profile guidance, a VNV flight plan must be entered and enabled. EIS • Non-path descent in a VNV scenario – A VNV flight plan is entered and enabled, however Pitch Hold, Vertical Speed, or Indicated Airspeed Mode can be used to descend to the VNV Target Altitude prior to reaching the planned TOD. Indicated Airspeed Mode is used in the example. AUDIO PANEL & CNS Indicated Airspeed descent: 1) Select Indicated Airspeed Mode: a) Using the ALT SEL Knob, set the Selected Altitude to 10,000 feet. HAZARD AVOIDANCE FLIGHT MANAGEMENT b) Press the IAS Key to activate Indicated Airspeed Mode. The annunciation ‘IAS’ 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/DN Wheel to adjust the commanded airspeed while maintaining the same power, or reduce power to allow descent in Indicated Airspeed 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. 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. APPENDICES 1 Cruise Altitude of 12,000 MSL ALT Mode 2 IAS Mod e 3 Selected Altitude of 10,000 MSL ALT Mode INDEX Figure 7-37 IAS Descent 420 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A 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 SEL 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 SEL 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 VNAV Target Altitude of 10,000 MSL BOD ALT Mode Selected Altitude (set below VNAV Target Altitude) INDEX Along-track Offset, 3 nm before OPSHN 3 nm Figure 7-38 VPTH Descent 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 421 SYSTEM OVERVIEW Automatic Flight Control System Non-path descent using Indicated Airspeed Mode: 1) Using Indicated Airspeed Mode, command a non-path descent to an intermediate altitude above the next VNV flight plan altitude. FLIGHT INSTRUMENTS a) Using the ALT SEL Knob, set the Selected Altitude below the current aircraft altitude to an altitude (in this case, 9,400 feet) at which to level off between VNV flight plan altitudes. EIS b) Press the IAS 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 Indicated Airspeed 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 422 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Automatic Flight Control System SYSTEM OVERVIEW FLIGHT INSTRUMENTS VP TH M od e Planned TOD 2 BOD 1 IA S VNAV Target Altitude of 10,000 MSL Pla nn M od e 3 Selected Altitude of 9,400 MSL ed EIS ALT Mode De sce nt ALT Mode Pa th TOD VP VNAV Target Altitude of 9,000 MSL TH Mo de 5 BOD AUDIO PANEL & CNS 4 ALT Mode Selected Altitude OPSHN FLIGHT MANAGEMENT 3 nm HABUK Figure 7-39 Non-path Descent HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 423 SYSTEM OVERVIEW Automatic Flight Control System Approach Note: If an approach contains a DME arc, the arc must be flown in Navigation Mode with the GFC 700. FLIGHT INSTRUMENTS When receiving vectors from ATC, Navigation Mode must be selected prior to intercepting the ARC. Flying an ILS approach: 1) Transition from GPS Navigation Mode to Heading Select Mode. EIS 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. AUDIO PANEL & CNS d) Use Heading Select Mode to comply with ATC vectors as requested. FLIGHT MANAGEMENT 2) Arm LOC Approach and Glideslope modes. a) Ensure the appropriate localizer frequency is tuned. HAZARD AVOIDANCE b) Press the APR Key when cleared for approach to arm Approach and Glideslope modes. ‘LOC’ and ‘GS’ appear in white as armed mode annunciations. c) The navigation source automatically switches to LOC. After this switch occurs, the localizer signal can be captured and the flight director determines when to begin the turn to intercept the final approach course. The flight director now provides guidance to the missed approach point. AFCS 3) There are two options available at this point, as the autopilot flies the ILS approach: • Push the AP DISC Button at the decision height and land the aircraft. INDEX APPENDICES ADDITIONAL FEATURES • Use the GA Button to execute a missed approach. 424 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Automatic Flight Control System SYSTEM OVERVIEW KCOS FLIGHT INSTRUMENTS LOC APR/ GS Mode 3 PETEY 2 HD G od M e PYNON 1 EIS AUDIO PANEL & CNS GPS NAV Mode FLIGHT MANAGEMENT Figure 7-40 ILS Approach to KCOS HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 425 SYSTEM OVERVIEW Automatic Flight Control System Flying a RNAV GPS approach with vertical guidance (SBAS Only): 1) Arm flight director modes for a RNAV GPS approach with vertical guidance: FLIGHT INSTRUMENTS a) Make sure the navigation source is set to GPS (use CDI Softkey to change navigation source). b) Select the Runway 35R LPV approach for KCOS. Load and activate the approach into the flight plan. EIS 2) Press the APR Key once clearance for approach has been received. GPS Approach Mode is activated and Glidepath Mode is armed. AUDIO PANEL & CNS 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: FLIGHT MANAGEMENT • Push the AP DISC Button at the decision height and land the aircraft. • Use the GA Button to execute a missed approach. KCOS CEGIX AFCS 3 GPS APR/ GP Mode HAZARD AVOIDANCE 4 2 ADDITIONAL FEATURES FALUR HABUK PYNON 1 INDEX APPENDICES GPS NAV Mode Figure 7-41 LPV Approach to KCOS 426 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Automatic Flight Control System SYSTEM OVERVIEW 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. AUDIO PANEL & CNS 2) Start the climb to the prescribed altitude in the published Missed Approach Procedure (in this case, 10,000 ft). Press the NAV Key to have the autopilot fly to the hold. FLIGHT MANAGEMENT 3) Use the ALT SEL Knob to set a Selected Altitude to hold. To hold the current airspeed during the climb, press the IAS Key. HAZARD AVOIDANCE 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. AFCS 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. ADDITIONAL FEATURES 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. APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 427 FLIGHT INSTRUMENTS SYSTEM OVERVIEW Automatic Flight Control System 4 EIS MOGAL AUDIO PANEL & CNS GPS NAV Mode 3 KCOS GA Mode FLIGHT MANAGEMENT 2 HAZARD AVOIDANCE 1 INDEX APPENDICES ADDITIONAL FEATURES AFCS Figure 7-42 Go Around/Missed Approach 428 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Automatic Flight Control System SYSTEM OVERVIEW AFCS Annunciations and Alerts AFCS Status Alerts FLIGHT INSTRUMENTS 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. AFCS Status Annunciation EIS AUDIO PANEL & CNS Figure 7-43 AFCS Status Annunciation Annunciation Rudder Mistrim Right Yaw servo providing sustained force in the indicated direction Rudder Mistrim Left Aileron Mistrim Right Elevator Mistrim Down Yaw Damper Failure Pitch servo providing sustained force in the indicated direction If AP engaged, take control of the aircraft and disengage AP If AP disengaged, move MET switch to unstick YD control failure Roll axis control failure; AP inoperative Pitch Failure Pitch axis control failure 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 Button 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. APPENDICES Preflight Test ADDITIONAL FEATURES Roll Failure System Failure AFCS Pitch Trim Failure HAZARD AVOIDANCE Roll servo providing sustained force in the indicated direction Aileron Mistrim Left Elevator Mistrim Up Description FLIGHT MANAGEMENT Alert Condition Hypoxia Recognition System is activated INDEX Preflight system test failed; aural alert sounds at failure Activated only by the Hypoxia Recognition System Table 7-5 AFCS Status Alerts 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 429 SYSTEM OVERVIEW Overspeed Protection FLIGHT INSTRUMENTS Automatic Flight Control System While Pitch Hold, Vertical Speed, Indicated Airspeed, Vertical Path Tracking, or an altitude capture mode is active, airspeed is monitored by the flight director. Pitch commands are not changed until overspeed protection becomes active. 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. Note: Overspeed protection is not active in ALT, GS or GP Modes. AUDIO PANEL & CNS EIS When an autopilot overspeed condition occurs, the Airspeed Reference appears in a box above the Airspeed Indicator, flashing a yellow ‘MAXSPD’ annunciation. The autopilot, if engaged, will follow the pitch up command for the flight director. Engine power should be reduced and/or the pitch reference adjusted to slow the aircraft. The annunciation disappears when the overspeed condition is resolved. Note: When the autopilot is outside normal operating limits, it uses more aggressive commands to return FLIGHT MANAGEMENT to normal limits. HAZARD AVOIDANCE Airspeed Indicator Figure 7-44 Overspeed Annunciation AFCS Underspeed Protection Underspeed Protection is designed to discourage aircraft operation below minimum established airspeeds and is available when the autopilot is on. ADDITIONAL FEATURES When the aircraft reaches a predetermined airspeed (Table 7-6), a yellow MINSPD annunciation (Figure 7-45) will appear above the airspeed indicator. When the airspeed trend vector reaches a predetermined airspeed (Table 7-6), a single aural “AIRSPEED” will sound, alerting the pilot to the impending underspeed condition. Flaps MINSPD Annunciation Aural AIRSPEED Alert 0% 80 kt 85 kt OFF 50% 76 kt 80 kt 100% 70 kt 80 kt 0% 85 kt 90 kt ON 50% 81 kt 85 kt * The optional TKS Flight Into Known Icing (FIKI) Anti-Ice System is only available on SR22 Models INDEX APPENDICES TKS FIKI * Table 7-6 MINSPD Annunciation and AIRSPEED Alert 430 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Automatic Flight Control System SYSTEM OVERVIEW FLIGHT INSTRUMENTS Airspeed Indicator Figure 7-45 MINSPD Annunciation EIS If the aircraft continues to decelerate, Underspeed Protection functionality depends on which vertical flight director mode is selected. For the purpose of this discussion, the vertical flight director modes can be divided into two categories: Those in which it is important to maintain altitude for as long as possible (altitude-critical modes), and those in which maintaining altitude is less crucial (non-altitude critical modes). AUDIO PANEL & CNS Altitude-Critical Modes (ALT, GS, GP, TO, GA) FLIGHT MANAGEMENT If the aircraft decelerates to stall warning, the lateral and vertical flight director modes will change from active to armed (Figure 7-46). The autopilot will provide input causing the aircraft to pitch down to maintain an airspeed no less than stall warning activation speed plus two knots, and the wings to level. Lateral and Vertical FD Modes Armed Figure 7-46 Lateral and Vertical Flight Director Modes Armed HAZARD AVOIDANCE An aural “AIRSPEED” alert will sound every five seconds and a red “UNDERSPEED PROTECT ACTIVE” annunciation (Figure 7-47) will appear to the right of the vertical speed indicator. AFCS ADDITIONAL FEATURES APPENDICES Figure 7-47 Underspeed Protect Active Annunciation When airspeed increases (as a result of adding power/thrust) to above the IAS at which stall warning turns off, plus two knots, the autopilot will cause the aircraft to pitch up until recapturing the vertical reference. The vertical and lateral flight director modes will change from armed to active. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 431 SYSTEM OVERVIEW Automatic Flight Control System Non-Altitude Critical Modes (VS, VNAV) FLIGHT INSTRUMENTS If the aircraft decelerates to an IAS below the minimum commandable autopilot airspeed, a red “UNDERSPEED PROTECT ACTIVE” annunciation (Figure 7-47) will appear to the right of the vertical speed indicator. The vertical flight director mode will change from active to armed (Figure 7-48), and the autopilot will cause the aircraft to pitch down until reaching a pitch attitude at which IAS equals the minimum commandable autopilot airspeed. EIS Vertical FD Mode Armed Figure 7-48 Vertical Flight Director Mode Armed AUDIO PANEL & CNS When sufficient power/thrust is available, the autopilot will recapture the previously selected vertical reference and the flight director mode will change from armed to active. Note: When the autopilot is outside normal operating limits, it uses more aggressive commands to return FLIGHT MANAGEMENT to normal limits. 7.2 S-TEC Fifty Five X Autopilot (Optional) HAZARD AVOIDANCE Note: This section covers only the additional ‘AP’ (autopilot engaged) status annunciation that may appear in the Perspective™ AFCS Status Box. This status annunciation is not analogous to both the Perspective™ and the S-TEC Fifty Five X. Refer to the approved S-TEC Fifty Five X Pilot’s Operating Handbook (POH) for comprehensive list of annunciations and operating instructions. AFCS In addition to the status and mode annunciations that are simultaneously displayed on both the Perspective™ (AFCS Status Box) and the S-TEC Fifty Five X (Autopilot Display and/or Remote Annunciator Display), the Perspective™ displays an additional status annunciation of ‘AP’ when the autopilot is engaged. ADDITIONAL FEATURES Autopilot Status INDEX APPENDICES Figure 7-49 Autopilot Engaged (Perspective™ AFCS Status Box) 432 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW Section 8 Additional Features NOTE: With the availability of SafeTaxi®, ChartView, or FliteCharts®, it may be necessary to carry another FLIGHT INSTRUMENTS source of charts on-board the aircraft. Additional features of the system include the following: • Synthetic Vision System (SVS) • SafeTaxi® diagrams EIS • ChartView and FliteCharts® electronic charts • AOPA’s Airport Directory • XM Radio entertainment AUDIO PANEL & CNS • Scheduler • Electronic Checklists • Flight Data Logging FLIGHT MANAGEMENT • Hypoxia Prevention System • Electronic Stability and Protection (ESP™) System HAZARD AVOIDANCE 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. AFCS 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. AOPA’s Airport Directory offers detailed information for a selected airport, such as available services, hours of operation, and lodging options. ADDITIONAL FEATURES 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. APPENDICES 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 Messages Window on the PFD. Optional checklists help to quickly find the proper procedure on the ground or during flight. The Flight Data Logging feature automatically stores critical flight and engine data on an SD data card. Approximately 1,000 flight hours can be recorded for each 1GB of available space on the card. INDEX The Hypoxia Prevention System provides protection to aircraft occupants from succumbing to the debilitating affects of hypoxia. The Electronic Stability and Protection (ESP™) system discourages aircraft operation outside a desired flight envelope. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 433 SYSTEM OVERVIEW Additional Features 8.1 Synthetic Vision System (SVS) 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. AUDIO PANEL & CNS EIS The optional Synthetic Vision System (SVS) is a visual enhancement to the Perspective™ Integrated Avionics System. 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 8‑94). 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 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. 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 The optional Terrain Awareness and Warning System (TAWS) or standard 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 or TAWS 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: 434 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 435 SYSTEM OVERVIEW Additional Features FLIGHT INSTRUMENTS PFD BACK SYN VIS Pressing the BACK Softkey returns to the top-level softkeys. BACK SYN TERR HRZN HDG APTSIGNS EIS PATHWAY 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. 436 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW SVS Features Flight Path Marker FLIGHT INSTRUMENTS Selected Altitude Pathways Color Matches CDI Indicating NAV Source Airport Runway EIS Zero Pitch Line (ZPL) with Compass Heading Marks Airplane Symbol 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 selected altitude during climb, cruise, and when the active leg is the final approach course prior to intercepting the glidepath/glideslope. During a descent (except while on the approach glidepath/glideslope), the pathway boxes are displayed at the selected altitude, or the VNAV altitude programmed for the active leg in the flight plan, or the published altitude constraint, whichever is higher (Figure 8-4). Just prior to intercepting the glidepath/glideslope, the pathway boxes are displayed on the glidepath/glideslope, or the selected altitude, whichever is lower. APPENDICES 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 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. 437 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/glideslope information on an active ILS, LPV, LNAV/VNAV, and some LNAV approaches. Pathways are intended as an aid to situational awareness and should not be used independent of the CDI, VDI, glide path indicator, and glide slope indicator. They are removed from the display when the selected navigation information is not available. Pathways are not displayed beyond the active leg when leg sequencing is suspended and are not displayed on any portion of the flight plan leg that would lead to intercepting a leg in the wrong direction. 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 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. 438 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 the selected altitude is lower than the programmed altitude. When an approach providing vertical guidance is activated, Pathways are shown level at the selected altitude up to the point along the final approach course where the altitude intercepts the extended vertical descent path, glidepath, or glideslope. From the vertical path descent, glidepath, or glideslope intercept point, the pathways are shown inbound to the Missed Approach Point (MAP) along the published lateral and vertical descent path, or at the selected altitude, whichever is lower. EIS 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. 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. FLIGHT MANAGEMENT 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 Selected Altitude or Programmed Altitude (whichever is higher) APPENDICES Figure 8-5 SVS Pathways, Enroute and Descent INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 439 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 440 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 TAWS or Terrain-SVS. 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 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. 441 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 250 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 442 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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. NOTE: Not all airports have runways with endpoint data in the database, therefore, these runways are not displayed. 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 HAZARD AVOIDANCE Runway Selected for Approach Other Runway on Airport AFCS ADDITIONAL FEATURES APPENDICES Figure 8-9 Airport Runways INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 443 SYSTEM OVERVIEW Additional Features Terrain - SVS and TAWS 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 and TAWS, 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 444 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 Potential Impact Point HAZARD AVOIDANCE Figure 8-11 Obstacle AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 445 SYSTEM OVERVIEW Additional Features Field of View FLIGHT INSTRUMENTS The PFD field of view can be represented on the MFD Navigation Map Page. Two dashed lines forming a V‑shape in front of the aircraft symbol on the map, represent the forward viewing area shown on the PFD. Configuring field of view: 1) While viewing the Navigation Map Page, press the MENU Key to display the PAGE MENU. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 2) Turn the large FMS Knob to highlight Map Setup and press the ENT Key. HAZARD AVOIDANCE Field of View Navigation Map Page OPTIONS Menu Map Setup Menu, Map Group, Field of View Option AFCS Figure 8-12 Option Menus 3) Turn the FMS Knob to select the Map Group and press the ENT Key. 4) Turn the large FMS Knob to scroll through the Aviation Group options to FIELD OF VIEW. ADDITIONAL FEATURES 5) Turn the small FMS Knob to select On or Off. INDEX APPENDICES 6) Press the FMS Knob to return to the Navigation Map Page. 446 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW The following figure compares the PFD forward looking depiction with the MFD plan view and FIELD OF VIEW turned on. FLIGHT INSTRUMENTS Lines Depict PFD Field of View EIS Field of View on the MFD AUDIO PANEL & CNS SVS View on the PFD Figure 8-13 MFD and PFD Field of View Comparison FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 447 SYSTEM OVERVIEW Additional Features 8.2 Enhanced Vision System (EVS) FLIGHT INSTRUMENTS The Perspective™ system provides a control and display interface to an Enhanced Vision System. EVS is designed to provide an aid to situational awareness while operating in low visibility environments. The EVS camera view is displayed on the AUX - VIDEO page. Image Quality and Interpretation EIS Image quality may vary according to target size, target temperature, background temperature, and attenuation from airborne particles or moisture within view of the sensor. If the video signal is ever completely interrupted, the display may appear as a solid field of gray, white, or blue, and the message No Video or NO DATA AVAILABLE may appear. HAZARD AVOIDANCE FLIGHT MANAGEMENT The EVS periodically calibrates itself to optimize the image. The calibration process can be observed on the display as a one second image interruption, which happens every five minutes or when calibration is manually activated. AUDIO PANEL & CNS Upon power-up the EVS requires approximately 30 seconds to produce a usable image. The image generated is monochrome (black and white). Normally the hotter an object is the whiter it appears on the display. EVS Data Unavailable EVS Calibration AFCS Figure 8-14 EVS Messages EVS Softkeys ADDITIONAL FEATURES While on the AUX - VIDEO Page, pressing the VID ZM + or VID ZM - Softkeys increases or decreases EVS display magnification between 1x and 2x. APPENDICES Pressing the HIDE MAP Softkey removes the map and displays EVS on the full screen. The softkey label changes to grey with black characters. Pressing the HIDE MAP Softkey again restores the map view and the small EVS image. The softkey label returns to white characters on a black background. Pressing the SETUP Softkey advances to the next level of softkeys: CNTRST -, CNTRST +, BRIGHT -, BRIGHT +, SAT -, SAT +, RESET, and BACK. INDEX Pressing the CNTRST - and CNTRST + Softkeys adjust display contrast in five percent increments from 0 to 100%. Pressing the BRIGHT - and BRIGHT + Softkeys adjust display brightness in five percent increments from 0 to 100%. Pressing the SAT - and SAT + Softkeys adjust display saturation in five percent increments from 0 to 100%. 448 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW Pressing the RESET Softkey returns all video adjustments options to the default settings. While viewing the SETUP Softkeys, pressing the BACK Softkey or after 45 seconds of softkey inactivity, the system reverts to the AUX - VIDEO Page softkeys. ENGINE CNTRST + SETUP BRIGHT - BRIGHT + ZOOM IN ZOOM OUT SAT - SAT + HIDE MAP RESET EIS CNTRST - MAP FLIGHT INSTRUMENTS The EVS softkeys shown below appear on the AUX - VIDEO Page. BACK AUDIO PANEL & CNS Pressing the BACK Softkey returns to the Previous Level Softkeys. Figure 8-15 EVS Softkeys FLIGHT MANAGEMENT The video adjustment options can also be selected by using the page menu option. Selecting video adjustment options: 1) While viewing the AUX - VIDEO Page press the MENU Key to display the Page Menu OPTIONS. HAZARD AVOIDANCE 2) Turn the large FMS Knob to highlight the desired video adjustment option and press the ENT Key. Once the ENT key is pressed on any option, the page menu closes and returns to the AUX - VIDEO Page. AFCS ADDITIONAL FEATURES APPENDICES Figure 8-16 AUX - VIDEO Page Menu INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 449 SYSTEM OVERVIEW Additional Features EIS FLIGHT INSTRUMENTS EVS Camera View FLIGHT MANAGEMENT AUDIO PANEL & CNS Map View EVS Softkeys HAZARD AVOIDANCE Figure 8-17 EVS and Map on the AUX - Video Page INDEX APPENDICES ADDITIONAL FEATURES AFCS EVS View with Map Hidden Figure 8-18 Full Screen EVS Image 450 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW 8.3 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. • VOR Information Page • Inset Map (PFD) • User Waypoint Information Page • Weather Datalink Page • Trip Planning Page • Airport Information Page • Nearest Pages • Intersection Information Page • Active and Stored Flight Plan Pages FLIGHT MANAGEMENT • Navigation Map Page 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: HAZARD AVOIDANCE • NDB Information Page 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 451 SYSTEM OVERVIEW Additional Features FLIGHT INSTRUMENTS Taxiway Identification EIS Aircraft Position AUDIO PANEL & CNS Airport Hot Spot Outline FLIGHT MANAGEMENT Airport Features Figure 8-19 SafeTaxi Depiction on the Navigation Map Page DCLTR Softkey Removes Taxiway Markings INDEX APPENDICES ADDITIONAL FEATURES 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 and station ID, the VOR symbol, and intersection names if within the airport plan view. Pressing the DCLTR-2 Softkey removes the airport diagram and 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. 452 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW Configuring SafeTaxi range: 1) While viewing the Navigation Map Page, press the MENU Key to display the PAGE MENU. 2) Turn the large FMS Knob to highlight the Map Setup Menu Option and press the ENT Key. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS Figure 8-20 Navigation Map PAGE MENU, Map Setup Option 3) Turn the FMS Knob to select the Aviation Group and press the ENT Key. 4) Turn the large FMS Knob to scroll through the Aviation Group options to SAFETAXI. FLIGHT MANAGEMENT 5) Turn the small FMS Knob to display the range of distances. 6) Turn either FMS Knob to select the desired distance for maximum SafeTaxi display range. 7) Press the ENT Key to complete the selection. HAZARD AVOIDANCE 8) Press the FMS Knob to return to the Navigation Map Page. AFCS SAFETAXI Option ADDITIONAL FEATURES SafeTaxi Range Options APPENDICES INDEX Figure 8-21 MAP SETUP Menu, Aviation Group, SAFETAXI Range Options 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 453 SYSTEM OVERVIEW Additional Features SafeTaxi Cycle Number and Revision FLIGHT INSTRUMENTS SafeTaxi database is revised every 56 days. SafeTaxi is always available for use after the expiration date. When turning on the system, the Power-up Page indicates whether the databases are current, out of date, or not available. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS SafeTaxi Database Figure 8-22 Power-up Page, SafeTaxi Database HAZARD AVOIDANCE Power-up Page Display Definition Normal operation. SafeTaxi database is valid and within current cycle. SafeTaxi database has expired. AFCS Database card contains no SafeTaxi data. Table 8-1 SafeTaxi Annunciation Definitions ADDITIONAL FEATURES The SafeTaxi Region, Version, Cycle, Effective date and Expires date of the database cycle can also be found on the AUX - System Status page, as seen in Figure 8-23. INDEX APPENDICES Select the MFD1 DB Softkey to place the cursor in the DATABASE window. Scroll through the listed information by turning the FMS Knob or pressing the ENT Key until the SafeTaxi database information is shown. 454 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW The SafeTaxi database cycle number shown in the figure, 09S3, is deciphered as follows: 09 – Indicates the year 2009 S – Indicates the data is for SafeTaxi FLIGHT INSTRUMENTS 3 – Indicates the third issue of the SafeTaxi database for the year The SafeTaxi EFFECTIVE date 07–MAY–09 is the beginning date for the current database cycle. SafeTaxi EXPIRES date 02–JUL–09 is the revision date for the next database cycle. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT SafeTaxi Data HAZARD AVOIDANCE AFCS Figure 8-23 AUX – System Status Page, SafeTaxi Current Information ADDITIONAL FEATURES 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 8‑23 and 8-24). NOT AVAILABLE appears in blue in the REGION field if SafeTaxi data is not available on the database card (Figure 8‑24). An expired SafeTaxi database is not disabled and will continue to function indefinitely. APPENDICES Select the MFD1 DB Softkey a second time. The softkey label will change to PFD1 DB. The DATABASE window will now be displaying database information for the PFD. As before, scroll through the listed information by turning the FMS Knob or pressing the ENT Key until the SafeTaxi database information is shown. Refer to Updating Garmin Databases in Appendix B for instructions on revising the SafeTaxi database. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 455 SYSTEM OVERVIEW Additional Features 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. FLIGHT MANAGEMENT Current Date is before Effective Date SafeTaxi Database has Expired SafeTaxi Database Not Installed INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Figure 8-24 AUX – System Status Page, SafeTaxi Expired, SafeTaxi Not Available 456 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW 8.4 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 8-25 ChartView SHW CHRT, Chart Selection, and Chart Option Softkeys INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 457 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 8-26 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 8-27 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 8-28 Unable To Display Chart Banner 458 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 the one associated with the WPT – Airport Information page. Usually this is the airport runway diagram. Where no runway diagram exists, but Take Off Minimums or Alternate Minimums are available, that page appears. If Airport Information pages are unavailable, the Approach Chart for the airport is shown. EIS Selecting a chart: AUDIO PANEL & CNS 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. 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 Scale Select Desired Approach Chart From Menu ADDITIONAL FEATURES Scroll Through Chart With the Joystick APPENDICES INDEX Figure 8-29 Approach Information Page, Chart Selection 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 459 SYSTEM OVERVIEW Additional Features While the APPROACH Box is selected using the FMS Knob, the MFD 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 8‑33). 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 8-30 CHRT Softkey, Airport Information Page 460 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW Pressing the INFO-1 or INFO-2 Softkey returns to the airport diagram chart when the view is on a terminal procedure chart. If the displayed chart is the airport diagram chart, pressing the INFO-1 or INFO-2 Softkey returns to the Airport Information Page. 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-1 or INFO-2 Softkey. When the INFO Box is selected using the FMS Knob, the MFD 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 HAZARD AVOIDANCE Aircraft Current Position AFCS Figure 8-31 Airport Information Page, INFO View, Full Screen Width ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 461 SYSTEM OVERVIEW Additional Features FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS In the example shown in Figure 8-31, the Class B Chart is selected. Pressing the ENT Key displays the Charlotte Class B Airspace Chart (Figure 8-32). HAZARD AVOIDANCE Figure 8-32 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 8-33 Departure Information Page 462 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 8-34 Arrival Information Page HAZARD AVOIDANCE Pressing the APR Softkey displays the approach chart for the airport if available. AFCS ADDITIONAL FEATURES APPENDICES 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX Figure 8-35 Approach Information Page 463 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 8-36 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 8-36. The NOTAM Softkey may appear on the Airport Information Page and all of the chart page selections. 464 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT NOTAM Softkey Appears for Selected Airports Figure 8-37 NOTAM Softkey Highlighted HAZARD AVOIDANCE Local NOTAM on This Airport AFCS ADDITIONAL FEATURES APPENDICES NOTAM Softkey Selected Figure 8-38 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). 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 465 SYSTEM OVERVIEW Additional Features Chart Options Pressing the CHRT OPT Softkey displays the next level of softkeys, the chart options level (Figure 8-25). 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 8-39 Approach Information Page, ALL View 466 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 8-40 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 8-41 Approach Information Page, Plan View 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 467 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 8-42 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 8-43 Approach Information Page, Minimums View, Full Screen Width 468 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 8-44 Airport Information Page, FIT WDTH Softkey Selected APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 469 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 INDEX Figure 8-45 Airport Information Page, Full Screen and Info Window Pressing the BACK Softkey, or waiting for 45 seconds reverts to the chart selection softkeys. 470 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 8-46 Page Menus AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 471 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 MFD 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 8-47 Waypoint Information Page, OPTIONS Menu 3) Turn the large FMS Knob to move to the COLOR SCHEME Option (Figure 8‑48). 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. 472 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-48 Arrival Information Page, Day View HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES Figure 8-49 Arrival Information Page, Night View INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 473 SYSTEM OVERVIEW Additional Features ChartView Cycle Number and Expiration Date AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS ChartView database is revised every 14 days. Charts are still viewable during a period that extends from the cycle expiration date to the disables date. ChartView is disabled 70 days after the expiration date and is no longer available for viewing. When turning on the system, the Power-up Page displays the current status of the ChartView database. See the table below for the various ChartView Power-up Page displays and the definition of each. FLIGHT MANAGEMENT ChartView Database Figure 8-50 Power-up Page, ChartView Database INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Power-up Page Display Definition Blank Line. System is not configured for ChartView. Contact a Garminauthorized service center for configuration. System is configured for ChartView but no chart database is installed. Contact Jeppesen for a ChartView database. Normal operation. ChartView database is valid and within current cycle. ChartView database is within 1 week after expiration date. A new cycle is available for update. ChartView database is beyond 1 week after expiration date, but still within the 70 day viewing period. ChartView database has timed out. Database is beyond 70 days after expiration date. ChartView database is no longer available for viewing. System time is not available. GPS satellite data is unknown or the system has not yet locked onto satellites. Check database cycle number for effectivity. System is verifying chart database when new cycle is installed for the first time. After verifying, chart database is found to be corrupt. ChartView is not available. Table 8-2 ChartView Power-up Page Annunciations and Definitions 474 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW 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. NOTE: A subdued softkey label indicates the function is disabled. EIS Select the MFD1 DB Softkey to place the cursor in the DATABASE window. Scroll through the listed information by turning the FMS Knob or pressing the ENT Key until the ChartView database information is shown. AUDIO PANEL & CNS The ChartView database cycle number shown in the figure, 0904, is deciphered as follows: 09 – Indicates the year 2009 04 – Indicates the fourth issue of the ChartView database for the year The EXPIRES date 05–MAR–09 is the date that this database should be replaced with the next issue. FLIGHT MANAGEMENT The DISABLES date 14–MAY–09 is the date that this database becomes inoperative. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES ChartView Data APPENDICES Figure 8-51 AUX – System Status Page, ChartView Current and Available 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX The ChartView database is provided directly from Jeppesen. Refer to Updating Jeppesen Databases in Appendix B for instructions on revising the ChartView database. 475 SYSTEM OVERVIEW Additional Features AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Other possible AUX - System Status page conditions are shown in Figure 8-52. The EXPIRES date, in yellow, is the revision date for the next database cycle. The DISABLES date, in yellow, is the date that this database cycle is no longer viewable. CYCLE NOT AVAILABLE in blue, indicates no ChartView data is available on the database card or no database card is inserted. FLIGHT MANAGEMENT ChartView has Expired, but is not Disabled ChartView Database is Disabled ChartView Database is Not Available INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Figure 8-52 AUX – System Status Page, ChartView Expired, ChartView Disabled, ChartView Not Available 476 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW 8.5 FliteCharts • Departure Procedures (DP) FLIGHT INSTRUMENTS FliteCharts resemble the paper version of AeroNav Services 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 • Airport Diagrams FliteCharts Softkeys EIS 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. 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. FLIGHT MANAGEMENT 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. CHRT OPT CHRT INFO DP STAR APR WX HAZARD AVOIDANCE SHW CHRT GO BACK AFCS Presssing the GO BACK Softkey returns to the top-level softkeys and previous page. FIT WDTH FULL SCN BACK ADDITIONAL FEATURES ALL Pressing the BACK Softkey returns to the Chart Selection Softkeys. APPENDICES Figure 8-53 FliteCharts SHW CHRT, Chart Selection, and Chart Option Softkeys INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 477 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 8-54 Option Menus ADDITIONAL FEATURES 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. Figure 8-55 Chart Not Available Banner INDEX 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. Figure 8-56 Unable To Display Chart Banner 478 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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. Chart Not To Scale AFCS Select Desired Approach Chart from Menu ADDITIONAL FEATURES Pan Chart With the Joystick APPENDICES Aircraft Not Shown Icon INDEX Figure 8-57 Approach Information Page, Chart Selection 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 479 SYSTEM OVERVIEW Additional Features While the APPROACH Box is selected using the FMS Knob, the MFD 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. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 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. APPENDICES ADDITIONAL FEATURES AFCS Press CHRT Softkey to Switch Between FliteCharts and Navigation Map Page INDEX Figure 8-58 CHRT Softkey, Airport Information Page 480 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW Pressing the INFO-1 or INFO-2 Softkey returns to the airport diagram chart when the view is on a terminal procedure chart. If the displayed chart is the airport diagram chart, pressing the INFO-1 or INFO-2 Softkey returns to the Airport Information Page. FLIGHT INSTRUMENTS Another source for additional airport information is from the INFO Box above the chart (Figure 8-65) or to the right of the chart (Figure 8-59) for certain airports. This information source is not related to the INFO‑1 or INFO-2 Softkey. When the INFO Box is selected using the FMS Knob, the MFD softkeys are blank. The Charlotte, NC airport has three additional charts offering information; the Airport Diagram, Alternate Minimums, and Take-off Minimums. EIS AUDIO PANEL & CNS Info Box Selected FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 8-59 Airport Information Page, INFO View with Airport Information AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 481 SYSTEM OVERVIEW Additional Features FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS In the example shown in Figure 8-59, TAKE OFF MINIMUMS is selected. Pressing the ENT Key displays the Take-off Minimums and Departure Procedures Chart (Figure 8-60). HAZARD AVOIDANCE Figure 8-60 Airport Information Page, TAKE OFF MINIMUMS Selected from INFO View INDEX APPENDICES ADDITIONAL FEATURES AFCS Pressing the DP Softkey displays the Departure Procedure Chart if available. Figure 8-61 Departure Information Page 482 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW Pressing the STAR Softkey displays the Standard Terminal Arrival Chart if available. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure 8-62 Arrival Information Page Pressing the APR Softkey displays the approach chart for the airport if available. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX Figure 8-63 Approach Information Page 483 SYSTEM OVERVIEW Additional Features 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 MFD 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. FLIGHT MANAGEMENT AUDIO PANEL & CNS 5) Press the FMS Knob again to deactivate the cursor. HAZARD AVOIDANCE WX Info When Available AFCS Info Available on This Airport Chart Not To Scale ADDITIONAL FEATURES Softkeys are Blank during Info Box Selection APPENDICES Figure 8-64 Weather Information Page, WX Softkey Selected WX Softkey Selected INDEX Pressing the GO BACK Softkey reverts to the previous page (Navigation Map Page or Flight Plan Page). 484 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW Chart Options Pressing the CHRT OPT Softkey displays the next level of softkeys, the chart options level (Figure 8-53). Pressing the ALL Softkey shows the complete chart on the screen. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS Complete Chart Shown FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 8-65 Airport Information Page, ALL View Selected AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 485 SYSTEM OVERVIEW Additional Features ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 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. Press FIT WDTH Softkey to Show Full Chart Width INDEX APPENDICES Figure 8-66 Approach Information Page, FIT WDTH Softkey Selected 486 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW Pressing the FULL SCN Softkey alternates between removing and replacing the data window to the right. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Press FULL SCN Softkey to Switch Between Chart on Full Screen and Chart with Info Window AFCS Figure 8-67 Airport Information Page, Full Screen and Info Window ADDITIONAL FEATURES Pressing the BACK Softkey, or waiting for 45 seconds reverts to the chart selection softkeys. The full screen view can also be selected by using the page menu option. APPENDICES Selecting full screen On or Off: 1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS. 2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key. 3) Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX 4) Turn the small FMS Knob to choose between the On and Off Full Screen Options. 487 EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Additional Features AUDIO PANEL & CNS Chart Setup Option Full Screen On/Off Selection Figure 8-68 Page Menus Day/Night View FLIGHT MANAGEMENT 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 MFD softkeys are blank. Selecting Day, Night, or Automatic View: HAZARD AVOIDANCE 1) While viewing a terminal chart press the MENU Key to display the Page Menu OPTIONS. APPENDICES ADDITIONAL FEATURES AFCS 2) Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key. Figure 8-69 Waypoint Information Page, OPTIONS Menu 3) Turn the large FMS Knob to move to the COLOR SCHEME Option (Figure 8‑70). 4) Turn the small FMS Knob to choose between Day, Auto, and Night Options. INDEX 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. 488 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW The display must be changed in order for the new setting to become active. This may be accomplished by selecting another page or changing the display range. 6) Press the FMS Knob when finished to remove the Chart Setup Menu. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 8-70 Approach Information Page, Day View AFCS ADDITIONAL FEATURES APPENDICES INDEX Figure 8-71 Approach Information Page, Night View 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 489 SYSTEM OVERVIEW Additional Features FliteCharts Cycle Number and Expiration Date AUDIO PANEL & CNS EIS 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 disables date. FliteCharts is disabled 180 days after the expiration date and are no longer available for viewing upon reaching the disables date. When turning on the system, the Power-up Page displays the current status of the FliteCharts database. See the table below for the various FliteCharts Power-up Page displays and the definition of each. FLIGHT MANAGEMENT FliteCharts Database HAZARD AVOIDANCE Figure 8-72 Power-up Page, FliteCharts Database ADDITIONAL FEATURES AFCS Power-up Page Display Definition Blank Line. 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. 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. APPENDICES Table 8-3 FliteCharts Power-up Page Annunciations and Definitions When the 180 day grace period has expired, ‘Chart data is disabled.’ in yellow indicates 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. INDEX 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. 490 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW 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. FLIGHT INSTRUMENTS NOTE: A subdued softkey label indicates the function is disabled. Select the MFD1 DB Softkey to place the cursor in the DATABASE window. Scroll through the listed information by turning the FMS Knob or pressing the ENT Key until the FliteCharts database information is shown. EIS The FliteCharts database cycle number shown in the figure, 0905, is deciphered as follows: 09 – Indicates the year 2009 05 – Indicates the fifth issue of the FliteCharts database for the year AUDIO PANEL & CNS The FliteCharts EFFECTIVE date 07–MAY–09 is the first date that this database is current. The FliteCharts EXPIRES date 04–JUN–09 is the last date that this database is current. The DISABLES date 01–DEC–09 is the date that this database becomes inoperative. FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES FliteCharts Data APPENDICES Figure 8-73 AUX – System Status Page, FliteCharts Current and Available The FliteCharts database is provided from Garmin. Refer to Updating Garmin Databases in Appendix B for instructions on revising the FliteCharts database. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 491 SYSTEM OVERVIEW Additional Features AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 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 MANAGEMENT FliteCharts Expired, but is not Disabled FliteCharts Database is Disabled FliteCharts Database is Not Available INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE Figure 8-74 AUX – System Status Page, FliteCharts Expired, FliteCharts Disabled, FliteCharts Not Available 492 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW 8.6 AOPA Airport Directory FLIGHT INSTRUMENTS The Aircraft Owners and Pilots Association (AOPA) Airport Directory database offers detailed information regarding services, hours of operation, lodging options, and more. This information is viewed on the Airport Information Page by selecting the INFO Softkey until INFO-2 is displayed as shown in Figure 8-75. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE Figure 8-75 AOPA Information on the Airport Information Page AOPA Database Cycle Number and Revision AFCS The AOPA Airport Directory database is revised four times per year. Check fly.garmin.com for the current database. The Airport Directory is always available for use after the expiration date. When turning on the system, the Power-up Page indicates whether the databases are current, out of date, or not available. ADDITIONAL FEATURES APPENDICES AOPA Database INDEX Figure 8-76 Power-up Page, Airport Directory Database 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 493 SYSTEM OVERVIEW Additional Features FLIGHT INSTRUMENTS Power-up Page Display Definition Normal operation. AOPA Airport Directory database is valid and within current cycle. AOPA Airport Directory database has expired. Database card contains no AOPA Airport Directory data. Table 8-4 Airport Directory Annunciation Definitions EIS The Airport Directory Region, Version, Cycle, Effective date and Expires date of the database cycle can also be found on the AUX - System Status page, as seen in Figure 8-77. AUDIO PANEL & CNS Select the MFD1 DB Softkey to place the cursor in the DATABASE window. Scroll through the listed information by turning the FMS Knob or pressing the ENT Key until the Airport Directory database information is shown. The Airport Directory database cycle number shown in the figure, 09D2, is deciphered as follows: 09 – Indicates the year 2009 FLIGHT MANAGEMENT D – Indicates the data is for Airport Directory 2 – Indicates the second issue of the Airport Directory database for the year ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE The Airport Directory EFFECTIVE date 15–APR–09 is the beginning date for the current database cycle. The Airport Directory EXPIRES date 14–JUL–09 is the revision date for the next database cycle. APPENDICES Airport Directory Data Figure 8-77 AUX – System Status Page, Airport Directory Current Information INDEX Airport Directory information appears in blue and yellow text. The EFFECTIVE date appears in blue when data is current and in yellow when the current date is before the effective date. The EXPIRES date appears in blue when data is current and in yellow when expired (Table 8-4). NOT AVAILABLE appears in blue in the REGION field if Airport Directory data is not available on the database card. An expired Airport Directory database is not disabled and will continue to function indefinitely. 494 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW 8.7 XM Radio Entertainment 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. 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. AUDIO PANEL & CNS 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. These IDs are located: HAZARD AVOIDANCE • On the label on the back of the Data Link Receiver • On the XM Information Page on the MFD (Figure 8-78) • On the XM Satellite Radio Activation Instructions included with the unit (available at www.garmin.com, P/N 190-00355-04) AFCS Contact the installer if the Data Radio ID and the Audio Radio ID cannot be located. ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 495 SYSTEM OVERVIEW Additional Features NOTE: The LOCK Softkey on the XM Information Page (AUX Page Group) is used to save GDL 69A activation FLIGHT INSTRUMENTS 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 H or later) for further information. Activating the XM Satellite Radio services: EIS 1) Contact XM Satellite Radio through the e-mail 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 AUX 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 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. AFCS HAZARD AVOIDANCE Data Radio ID Audio Radio ID APPENDICES ADDITIONAL FEATURES Weather Products Window RADIO and INFO Softkeys Figure 8-78 XM Information Page LOCK Softkey is Used to Save Activation Data During Initial Setup 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. 496 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW Using XM Radio The XM Radio Page provides information and control of the audio entertainment features of the XM Satellite Radio. FLIGHT INSTRUMENTS Selecting the XM Radio Page: 1) Turn the large FMS Knob to select the AUX Page Group. 2) Turn the small FMS Knob to select the displayed AUX - XM Information Page. 3) Press the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled. EIS AUDIO PANEL & CNS Active Channel FLIGHT MANAGEMENT Channel List HAZARD AVOIDANCE Volume Field Categories Field AFCS Figure 8-79 XM Radio Page Active Channel and Channel List ADDITIONAL FEATURES The Active Channel Box on the XM Radio Page displays the currently selected channel the XM Radio is using. The Channels List Box of the XM Radio Page shows a list of the available channels for the selected category. Channels can be stepped through one at a time or may be selected directly by channel number. APPENDICES Selecting a channel from the channel list: 1) While on the XM Radio Page, press the CHNL Softkey. 2) Press the CH + Softkey to go up through the list in the Channel Box, or move down the list with the CH – Softkey. Or: INDEX 1) Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels. 2) Press the ENT Key to activate the selected channel. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 497 SYSTEM OVERVIEW Additional Features Selecting a channel directly: 1) While on the XM Radio Page, press the CHNL Softkey. FLIGHT INSTRUMENTS 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. 4) Press the ENT Key to activate the selected channel. Category EIS 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. AUDIO PANEL & CNS Selecting a category: 1) Press the CATGRY Softkey on the XM Radio Page. 2) Press the CAT + and CAT - Softkeys to cycle through the categories. FLIGHT MANAGEMENT Or: ADDITIONAL FEATURES AFCS 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. INDEX APPENDICES Figure 8-80 Categories List 498 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW 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 Press SET to Save Each Preset Channel HAZARD AVOIDANCE Figure 8-81 Accessing and Selecting XM Preset Channels Pressing the BACK Softkey, or 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. 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.) APPENDICES 3) Press the MUTE Softkey to mute the audio. Press the MUTE Softkey again to unmute the audio. INDEX Figure 8-82 Volume Control 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 499 SYSTEM OVERVIEW Additional Features 8.8 Scheduler FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 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 Messages Window on the PFD. Messages can be set to display based on a specific date and time (event), once the message timer reaches zero (one-time; default setting), or recurrently whenever the message timer reaches zero (periodic). Message timers set to periodic alerting automatically reset to the original timer value once the message is displayed. When power is cycled, all messages are retained until deleted, and message timer countdown is resumed. HAZARD AVOIDANCE Figure 8-83 Scheduler (Utility Page) Entering a scheduler message: 1) Select the AUX - Utility Page. 2) Press the FMS Knob momentarily to activate the flashing cursor. AFCS 3) Turn the large FMS Knob to highlight the first empty scheduler message naming field. 4) Use the FMS Knob to enter the message text to be displayed in the Messages Window and press the ENT Key. 5) Press the ENT Key again or use the large FMS Knob to move the cursor to the field next to Type. ADDITIONAL FEATURES 6) Turn the small FMS Knob to select the message alert type: • Event—Message issued at the specified date/time • One-time—Message issued when the message timer reaches zero (default setting) APPENDICES • Periodic—Message issued each time the message timer reaches zero 7) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field. INDEX 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. 500 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW 9) For event-based messages: a) Use the FMS Knob to enter the desired date (DD-MM-YY) and press the ENT Key. b) Press the ENT Key again or use the large FMS Knob to move the cursor to the next field. FLIGHT INSTRUMENTS 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 time. 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. HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Figure 8-84 PFD Messages Window APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 501 SYSTEM OVERVIEW Additional Features 8.9 Electronic Checklists FLIGHT INSTRUMENTS NOTE: The optional checklists presented here are for example only and may differ from checklists available for the SR20/SR22. 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 EIS 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. AUDIO PANEL & CNS (Optional) SYSTEM MAP DCLTR FLIGHT MANAGEMENT SYSTEM SHW CHRT CHKLIST CHECK EXIT EMERGCY The CHECK Softkey label changes to UNCHECK when the checklist item is already checked. Figure 8-85 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 system 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 ‘Checklist File: Invalid’ or ‘Checklist File: N/A’ (not available) and the CHKLIST Softkey is not available. AFCS Accessing and navigating checklists: 1) From any page on the MFD (except the EIS Pages), press the CHKLIST Softkey or turn the large FMS Knob to select the Checklist Page. ADDITIONAL FEATURES 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. APPENDICES 5) Turn the FMS Knob to select the desired checklist and press the ENT Key. The selected checklist item is indicated with white text surrounded by a white box. 6) Press the ENT Key or CHECK Softkey to check the selected checklist item. The line item turns green and a checkmark is placed in the associated box. The next line item is automatically selected for checking. Either FMS Knob can be used to scroll through the checklist and select the desired checklist item. INDEX Press the CLR Key or UNCHECK Softkey to remove a check mark from an item. 502 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW 7) When all checklist items have been checked, ‘*Checklist Finished*’ is displayed in green text at the bottom left of the checklist window. If all items in the checklist have not be checked, ‘*Checklist Not Finished*’ will be displayed in yellow text. FLIGHT INSTRUMENTS 8) Press the ENT Key. ‘GO TO NEXT CHECKLIST?’ will be highlighted by the cursor. 9) Press the ENT Key to advance to the next checklist. 10) Press the EXIT Softkey to exit the Checklist Page and return to the page last viewed. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES Figure 8-86 Sample Checklist APPENDICES Accessing emergency procedures: 1) From any page on the MFD (except the EIS Pages), press the CHKLIST Softkey or turn the large FMS Knob to select the Checklist Page. 2) Press the EMERGCY Softkey. INDEX 3) Turn the FMS Knob to select the desired emergency checklist and press the ENT Key. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 503 SYSTEM OVERVIEW Additional Features 4) Press the ENT Key or CHECK Softkey to check the selected emergency checklist item. The line item turns green and a checkmark is placed in the box next to it. The next line item is automatically highlighted for checking. Either FMS Knob can be used to scroll through the checklist and select the desired checklist item. FLIGHT INSTRUMENTS Press the CLR Key or UNCHECK Softkey to remove a check mark from an item. 5) When all checklist items have been checked, ‘*Checklist Finished*’ is displayed in green text at the bottom left of the checklist window. If all items in the checklist have not be checked, ‘*Checklist Not Finished*’ will be displayed in yellow text. 6) Press the ENT Key. ‘GO TO NEXT CHECKLIST?’ will be highlighted by the cursor. EIS 7) Press the ENT Key to advance to the next checklist. 8) Press the RETURN Softkey to return to the previous checklist. APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS 9) Press the EXIT Softkey to exit the Checklist Page and return to the page last viewed. INDEX Figure 8-87 Emergency Checklist Page Example 504 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW 8.10 Flight Data Logging NOTE: Some aircraft installations may not provide all aircraft/engine data capable of being logged by the FLIGHT INSTRUMENTS system. The Flight Data Logging feature will automatically store critical flight and engine data on an SD data card (up to 16GB) inserted into the top card slot of the MFD. Approximately 1,000 flight hours can be recorded for each 1GB of available space on the card. EIS Data is written to the SD card once each second while the MFD is powered on. All flight data logged on a specific date is stored in a file named in a format which includes that date (dataYYYY_MM_DD.csv). The file is created automatically each time the Perspective™ system is powered on, provided an SD card has been inserted. AUDIO PANEL & CNS The status of the Flight Data Logging feature can be viewed on the AUX-UTILITY Page. If no SD card has been inserted, “NO CARD” is displayed. When data is being written to the SD card, “LOGGING DATA” is displayed. The .csv file may be viewed with Microsoft Excel® or other spreadsheet applications. The following is a list of data parameters the Perspective™ system is capable of logging for the SR20 and SR22. • GPS altitude (MSL) • Magnetic Heading (degrees) • GPS vertical alert limit • GPS altitude (WGS84 datum) • HSI source • Baro-Corrected altitude (feet) • Selected course • SBAS GPS horizontal protection level • Baro Correction (in/Hg) • Com1/Com2 frequency • Indicated airspeed (kts) • Nav1/Nav2 frequency • SBAS GPS vertical protection level • Vertical speed (fpm) • CDI deflection • Fuel Qty (right & left)(gals) • GPS vertical speed (fpm) • VDI/GP/GS deflection • Fuel Flow (gph) • OAT (degrees C) • Wind Direction (degrees) • Fuel Pressure (psi) • True airspeed (knots) • Wind Speed (knots) • Voltage 1 and/or 2 • Pitch Attitude Angle (degrees) • Active Waypoint Identifier • Amps 1 and/or 2 • Roll Attitude Angle (degrees) • Distance to next waypoint (nm) • Engine RPM • Lateral and Vertical G Force (g) • Bearing to next waypoint (degrees) • Oil Pressure (psi) • Magnetic variation (degrees) • TIT (deg. F) • Autopilot On/Off • Manifold Pressure (in. Hg) • AFCS roll/pitch modes • CHT • AFCS roll/pitch commands • EGT ADDITIONAL FEATURES • Oil Temperature (deg. F) APPENDICES • Latitude (degrees; geodetic; +North) AFCS • Ground Track (degrees magnetic) • GPS horizontal alert limit HAZARD AVOIDANCE • Ground Speed (kts) FLIGHT MANAGEMENT • GPS fix • Time • Longitude (degrees; geodetic; +East) • Date INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 505 SYSTEM OVERVIEW Additional Features FLIGHT INSTRUMENTS The file containing the recorded data will appear in the format shown in Figure 8-88. This file can be imported into most computer spreadsheet applications. Local Date YYMMDD Local 24hr Time HHMMSS Nearest Airport (A blank will be inserted if no airport is found) EIS log_090210_104506_KIXD.csv AUDIO PANEL & CNS Figure 8-88 Log File Format INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT Data logging status can be monitored on the AUX-UTILITY Page. 506 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW 8.11 Hypoxia Recognition with Automatic Descent Mode FLIGHT INSTRUMENTS Hypoxia Recognition detects pilot incapacitation due to the affects of hypoxia or other physical condition. This is accomplished by monitoring pilot interaction with the Perspective™ system. If the system determines the pilot is not responding, Automatic Descent Mode is activated placing the aircraft in a descent to a lower altitude to provide the pilot and passengers an opportunity to recover from the effects of hypoxia.” EIS The system is operative when the aircraft altitude is above 14,900 feet (pressure altitude) and the GFC 700 autopilot is engaged. Pilot interaction with the Perspective™ system is monitored by detecting key presses and turns of the knobs (Audio Panel and push-to-talk switch excluded). If a period of inactivity (time dependent on altitude, see Figure 8-89) is detected, Hypoxia Recognition initiates and automatic descent. Upon activation, there are three sequential phases employed by the system; determining pilot alertness, descent to 14,000 feet MSL, and descent to 12,500 feet MSL. AUDIO PANEL & CNS Determining Pilot Alertness When the system detects a sufficient period of inactivity (Figure 8-89) the Advisory Annunciation ‘Are you alert?’ is displayed. Selecting the ALERT Softkey will acknowledge the message and reset the system. Pressing any other softkey, or turning a knob will also reset the system. FLIGHT MANAGEMENT When no pilot interaction is detected for an additional 60 seconds, the Caution Annunciation ‘HYPOXIA ALERT’ is displayed. Again, selecting the ALERT Softkey will acknowledge the message and reset the system. Pressing any other softkey, or turning a knob will also reset the system. HAZARD AVOIDANCE When no pilot interaction is detected for an additional 60 seconds, the Warning Annunciation ‘AUTO DESCENT’ is displayed in the Annunciation Window and ‘Automatic descent to 14,000FT in 60 seconds’ is displayed in the Alerts Window. Once again, selecting the ALERT Softkey will acknowledge the message and reset the system. Pressing any other softkey, or turning a knob will also reset the system. When no interaction is detected for another 60 seconds, the system will automatically proceed with the descent. 30 25 ADDITIONAL FEATURES 20 15 APPENDICES Period of Detected Inactivity (Minutes) Time of Useful Conciousness (min) e of Useful Conciousness (min) AFCS 35 10 5 15000 18000 21000 24000 27000 INDEX 0 30000 Aircraft Altitude (Feet) Aircraft Altitude (ft) Figure 8-89 Hypoxia Recognition Activation Times 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 507 SYSTEM OVERVIEW Automatic Descent Mode FLIGHT INSTRUMENTS Additional Features As the system prepares for descent, the Selected Altitude is set to 14,000 and the AFCS enters Indicated Airspeed (IAS) mode with the airspeed reference set to the maximum allowable airspeed setting for the specific aircraft model. Refer to the Flight Director Vertical Modes in the AFCS section. AFCS lateral mode settings are not affected. NOTE: Hypoxia Recognition does not account for terrain elevation. AUDIO PANEL & CNS EIS As the descent begins, an ‘AUTO DESCENT’ warning is displayed in the Annunciation Window. ‘AUTO DESCENT - Aircraft Descending to 14,000FT’ is displayed in the Alerts Window. ‘EDM’ is shown as an AFCS Status Annunciation indicating the system has entered Automatic Descent Mode. ‘EDM’ (Emergency Descent Mode) is the AFCS mode that is activated when Hypoxia Recognition initiates an automatic descent. A continuous repeating chime will be heard as long as Automatic Descent Mode is active. After the descent begins, Automatic Descent Mode can only be canceled by disconnecting the autopilot. As the aircraft reaches 14,000 feet the system sets the AFCS to Altitude Hold mode. The AFCS will also remain in Automatic Descent Mode as indicated by ‘EDM’ continuing to be displayed as an AFCS Status Annunciation. The system again begins monitoring for pilot interaction. FLIGHT MANAGEMENT If no pilot interaction is detected for four minutes, the system initiates the second descent. As the system prepares for this descent, the Selected Altitude is set to 12,500 and the AFCS again enters IAS mode with the airspeed reference set to the maximum allowable airspeed for the specific aircraft model. HAZARD AVOIDANCE As the descent begins, an ‘AUTO DESCENT’ warning is displayed in the Annunciation Window. ‘AUTO DESCENT - Aircraft Descending to 12,500FT’ is displayed in the Alerts Window. ‘EDM’ is shown as an AFCS Status Annunciation. Also, the continuous repeating chime is heard. INDEX APPENDICES ADDITIONAL FEATURES AFCS As the aircraft reaches 12,500 feet the system sets the AFCS to Altitude Hold mode. The AFCS will also remain in Automatic Descent Mode as indicated by ‘EDM’ continuing to be displayed as an AFCS Status Annunciation as well as the continuing presence of the repeating chime. At this point, the AFCS must be disconnected to cancel Automatic Descent Mode. 508 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW 8.12 Electronic Stability and Protection (ESP™) FLIGHT INSTRUMENTS The Electronic Stability and Protection (ESP™) system is available only when the GFC 700 AFCS is installed. This system is designed to provide automatic control inputs to discourage aircraft operation outside a desired flight envelope. ESP™ works to maintain the desired roll operating envelope by automatically engaging one or more servos when the aircraft is near a defined roll operating limit. While ESP™ utilizes the same sensors, processors, and actuators as the GFC 700 autopilot, it is a separate function. When the GFC 700 autopilot is engaged and/or the aircraft is at or below 200 feet AGL, the ESP™ system will not operate. EIS The pilot can interrupt ESP by pressing and holding the Autopilot Disconnect (AP DISC) switch. Upon releasing the or AP DISC switch, ESP force will again be applied, provided aircraft roll attitude is within engagement limits. ESP can also be overridden by overpowering the servo’s mechanical torque limit. ESP can be enabled or disabled on the AUX-System Setup 2 Page on the MFD. AUDIO PANEL & CNS To enable or disable ESP: 1) Turn the large FMS Knob to select the AUX Page Group. 2) Turn the small FMS Knob to select the System Setup Page. FLIGHT MANAGEMENT 3) If necessary, select the SETUP 2 Softkey to display the AUX-SYSTEM SETUP 2 Page. If the AUX-SYSTEM SETUP 2 is already displayed, proceed to step 4. 4) Press the FMS Knob to activate the cursor. 5) Turn the large FMS Knob to place the cursor in the STABILITY & PROTECTION field. HAZARD AVOIDANCE 6) Turn the small FMS Knob to select ‘ENABLE’ or ‘DISABLE’. 7) Press the FMS Knob to remove the cursor. ESP is automatically enabled on system power up. AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 509 SYSTEM OVERVIEW Additional Features Operation FLIGHT INSTRUMENTS Roll Limit Indicators are displayed on the roll scale at 45° right and left, indicating where ESP will engage (see Figure 8-90). As roll attitude exceeds 45°, ESP will engage and the on-side Roll Limit Indicator will move to 30°, as shown in Figure 8-91. The Roll Limit Indicator is now showing where ESP will disengage as roll attitude decreases to within the desirable roll attitude range. Roll Limit Indicator ESP Engage (45°) FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS Roll Limit Indicator ESP Engage (45°) Figure 8-90 ESP Roll Engagement Indication (ESP NOT Engaged) ESP Disengage (30°) Aircraft Roll Attitude = 46° ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE ESP Engage (45°) Aircraft Roll Attitude = 44° APPENDICES Before ESP Engage After ESP Engage INDEX Figure 8-91 Roll Increasing to ESP Engagement 510 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Additional Features SYSTEM OVERVIEW Once engaged, ESP force will be applied between 30° and 75°, as illustrated in Figure 8-92. The force increases as roll attitude increases and decreases as roll attitude decreases. The applied force is intended to encourage pilot input that returns the airplane to a more normal roll attitude. As roll attitude decreases, ESP will disengage at 30°. 10º 0º 10º 20º º 30 º EIS 90º 90º AUDIO PANEL & CNS 75º 75º º 60 60 º º 45 45 FLIGHT INSTRUMENTS º 30 20º FLIGHT MANAGEMENT Figure 8-92 ESP Roll Operating Range When Engaged (Force Increases as Roll Increases & Decreases as Roll Decreases) ESP is automatically disengaged if the aircraft reaches the autopilot roll engagement attitude limit of 75° (Figure 8-93). HAZARD AVOIDANCE ESP Upper Disengage Limit (75°) Aircraft Roll Attitude = 74° AFCS ADDITIONAL FEATURES APPENDICES Figure 8-93 Roll Attitude Autopilot Engagement Limit (ESP Engaged) INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 511 SYSTEM OVERVIEW Additional Features 8.13 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 • TAWS 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 8-94 SVS Reversionary Mode 512 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A 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 8-95 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 8-96 Blue Sky Bar with Full Display Terrain APPENDICES GDL 69/69A Data Link Receiver Troubleshooting Some quick troubleshooting steps listed below can be performed to find the possible cause of a failure. • Ensure the owner/operator of the aircraft in which the Data Link Receiver is installed has subscribed to XM • Ensure the XM subscription has been activated INDEX • Perform a quick check of the circuit breakers to ensure that power is applied to the Data Link Receiver • Ensure that nothing is plugged into the Aux Audio In jack because this would prevent XM radio from being heard 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 513 SYSTEM OVERVIEW Additional Features 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. FLIGHT INSTRUMENTS Selecting the AUX - System Status Page: 1) Turn the large FMS Knob to select the AUX Page Group. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 2) Turn the small FMS Knob to select the AUX - System Status Page. Figure 8-97 LRU Information Window on System Status Page AFCS If a failure still exists, the following messages may provide insight as to the possible problem: ADDITIONAL FEATURES Message CHECK ANTENNA UPDATING 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 Loss of signal; signal strength too low for receiver APPENDICES 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 5 minutes ACTIVATION REQUIRED Weather Datalink Page - center of page XM subscription is not activated INDEX Table 8-5 GDL 69/69A Data Link Receiver Error Messages 514 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22SR22T 190-00820-06 Rev. A Appendix A SYSTEM OVERVIEW Annunciations and Alerts Note: The Pilot’s Operating Handbook (POH) supersedes information found in this document. FLIGHT INSTRUMENTS The Perspective™ 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 Perspective™ System Annunciations Section for more information. HAZARD AVOIDANCE Comparator Window Reversionary Sensor Window AFCS ADDITIONAL FEATURES Annunciation Window Alerts Window APPENDICES Softkey Annunciation INDEX Figure A-1 Alerting System 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 515 SYSTEM OVERVIEW Appendix A • Audio Alerting System: The 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 ADDITIONAL FEATURES Figure A-2 Annunciation Tone Testing (AUX-System Status Page) INDEX APPENDICES • Comparator Window (Dual AHRS and/or Dual Air Data Computer installations only): Critical values generated by redundant sensors are monitored by comparators. If differences in the sensors exceed a specified amount, the Comparator Window appears in the upper right corner of the PFD and the discrepancy is annunciated in the Comparator Window as a ‘MISCOMP’ (miscompare). If one or both of the sensed values are unavailable, it will be annunciated as a ‘NO COMP’ (no compare). Figure A-3 Comparator Window 516 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix A SYSTEM OVERVIEW FLIGHT INSTRUMENTS • Reversionary Sensor Window (Dual AHRS and/or Dual Air Data Computer installations only): Reversionary sensor selection is annunciated in a window on the right side of the PFD. These annunciations reflect reversionary sensors selected on the PFD. Pressing the SENSOR Softkey accesses the ADC1, ADC2, AHRS1, and AHRS2 softkeys. These softkeys allow switching of the sensors being viewed on the PFD. The GPS sensor cannot be switched manually. Figure A-4 Reversionary Sensor Window EIS Alert Level Definitions AUDIO PANEL & CNS The Perspective™ Alerting System uses three alert levels. FLIGHT MANAGEMENT • WARNING: This level of alert requires immediate attention. Warning alert text is shown in red in the Annunciation Window and a flashing ‘WARNING’ Softkey annunciation. A repeating double chime accompanies select warning conditions. Pressing the WARNING Softkey acknowledges the presence of the warning alert and stops the aural chime (if present). Refer to Table A-1 for warning conditions and alerting behaviors. HAZARD AVOIDANCE • CAUTION: This level of alert indicates the existence of abnormal conditions on the aircraft that may require intervention. Caution alert text is shown in yellow in the Annunciation Window and is accompanied by a flashing ‘CAUTION’ Softkey annunciation. A double chime lasting for one second occurs with select caution alerts. Pressing the CAUTION Softkey acknowledges the presence of the caution alert. Refer to Table A-2 for caution conditions and alerting behaviors. AFCS • 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 with the exception of the 'OXYGEN LEFT ON' advisory alert, which produces a one second double chime. An annunciation alert is accompanied by a flashing ADVISORY Softkey annunciation. Pressing the ADVISORY Softkey acknowledges the presence of the annunciation alert. Refer to Table A-3 for annunciation alert conditions and behaviors. ADDITIONAL FEATURES 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. APPENDICES Figure A-5 Softkey Annunciation (ALERTS Softkey Labels) INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 517 SYSTEM OVERVIEW Appendix A Aircraft Alerts FLIGHT INSTRUMENTS The following alerts are configured specifically for the Cirrus SR20 and SR22 models. Red annunciation window text signifies warnings and yellow, cautions. See the Pilot’s Operating Handbook (POH) for recommended pilot actions. NOTE: The ice protection system (optional) must be operated in accordance with the approved flight manual limitations. This option is only available on the SR22 models. EIS Annunciation Window Text APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS ANTI ICE CTL Alerts Window Text Audio Alert Tank valves cannot be controlled (closed) (TKS). Repeating Double Chime ANTI ICE FLOW Flow rate is low (TKS). Repeating Double Chime ANTI ICE QTY Left and right fluid quantities are unknown (TKS) Repeating Double Chime ANTI ICE QTY Fluid quantity is low (TKS). Repeating Double Chime AOA OVERHEAT AUTO DESCENT† AUTO DESCENT† AUTO DESCENT† BRAKE TEMP CHT CO LVL HIGH ESS BUS FUEL FLOW* FUEL QTY M BUS 1 M BUS 2 AOA probe is overheated. Repeating Double Chime Automatic descent to 14,000FT in 60 seconds. Aircraft descending to 14,000FT. Aircraft descending to 12,500FT. Brake termperature is high. Cylinder head temperature is high. Carbon monoxide level is too high. Check essential power bus voltage. Check fuel flow. Check fuel tank levels. Check main power bus 1 voltage. Check main power bus 2 voltage. MAN PRESSURE* Check manifold pressure. OIL PRESSURE OIL TEMP OXYGEN FAULT OXYGEN QTY RPM STALL START ENGAGED TIT* UNDERSPEED PROTECT ACTIVE† Oil pressure is out of range. Oil temperature is high. Oxygen system fault. Oxygen quantity is low. Check engine RPM. Stall warning. Starter is engaged. TIT temperature is high. Repeating Double Chime Repeating Double Chime Repeating Double Chime Repeating Double Chime Repeating Double Chime Repeating Double Chime Repeating Double Chime1 None Repeating Double Chime Repeating Double Chime Repeating Double Chime Repeating Double Chime (after 30 seconds) Repeating Double Chime1 Repeating Double Chime Repeating Double Chime Repeating Double Chime Repeating Double Chime Tone Repeating Double Chime Repeating Double Chime None "Airspeed" INDEX Optional / * Not applicable to all models / TKS NH (optional) / TKS FIKI (optional) / 1 In air only / ^ SR22T only / † GFC 700 required Table A-1 Warning Alerts 518 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix A Double Chime ANTI ICE PRESS Tail pressure is low (TKS). Double Chime ANTI ICE PRESS Pressure is high (TKS). Double Chime Fluid quantity imbalance has been detected (TKS) Double Chime ANTI ICE QTY Fluid quantity is low (TKS) Double Chime ANTI ICE SPEED Airspeed is too low for ice protection (TKS). Double Chime1 ANTI ICE SPEED AP MISCOMPARE AP/PFD DIF ADC AP/PFD DIF AHRS AVIONICS OFF BATT 1 BRAKE TEMP CHT FLAP OVERSPEED FUEL FILTER FUEL QTY HYPOXIA ALERT† M BUS 1 M BUS 2 MAN PRESSURE* NO ADC MODES NO VERT MODES OIL PRESSURE OIL TEMP OXYGEN QTY OXYGEN RQD PARK BRAKE PITOT HEAT FAIL PITOT HEAT REQD START ENGAGED Airspeed is to high for ice protection (TKS). Double Chime1 Autopilot miscompare, autopilot is not available. Autopilot and PFD are using different ADCs. Autopilot and PFD are using different AHRSs. Avionics master switch is off. Check battery 1 current. Brake temperature is high. Cylinder head temperature is high. Flaps are extended beyond airspeed limitations. Fuel filter in bypass Check fuel tank levels. Hypoxia caution alert. Check main power bus 1. Check main power bus 2. Check manifold pressure. Autopilot air data modes are not available. Autopilot vertical modes are not available. Oil pressure is out of range. Oil temperature is high. Oxygen quantity is low. Oxygen is required. Parking break is set. Pitot heat failure. Pitot heat is required. Starter is engaged. Double Chime Double Chime Double Chime Double Chime Double Chime1 Double Chime Double Chime Double Chime Double Chime Double Chime Double Chime Double Chime1 Double Chime1 None Double Chime Double Chime Double Chime1 Double Chime Double Chime Double Chime None Double Chime Double Chime1 Double Chime APPENDICES Right tank fluid quantity is unreliable (TKS). ADDITIONAL FEATURES ANTI ICE LEVEL AFCS Double Chime HAZARD AVOIDANCE Left tank fluid quantity is unreliable (TKS). FLIGHT MANAGEMENT ANTI ICE LEVEL AUDIO PANEL & CNS Double Chime EIS Stall warning/AoA heater has failed. FLIGHT INSTRUMENTS Audio Alert Double Chime1 Double Chime1 Double Chime ANTI ICE HEAT ANTI ICE QTY SYSTEM OVERVIEW Annunciation Window Text Alerts Window Text ALT 1 Check alternator 1 current. ALT 2 Check alternator 2 current. ALT AIR OPEN* Alternate air door is open. INDEX Optional / * Not applicable to all models / TKS NH (optional) / TKS FIKI (optional) / 1 In air only / † GFC 700 required Table A-2 Caution Alerts 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 519 SYSTEM OVERVIEW Appendix A NOTE: The ice protection system (optional) must be operated in accordance with the approved flight manual FLIGHT INSTRUMENTS limitations. This option is only available on SR22 models. Annunciation Window Text None ALTITUDE SEL Descending away from selected altitude. None AOA FAIL ARE YOU ALERT?† Dynamic stall speed band is not available. None Are you alert? None COURSE SEL Current track will not intercept selected course. None HIGH MP FF* Avoid fuel flow 18 to 30 GPH and MP above 26”. None Check left fuel tank level. None EIS L FUEL QTY AUDIO PANEL & CNS Audio Alert Climbing away from selected altitude. OXYGEN LEFT ON OXYGEN QTY PUMP BACKUP R FUEL QTY FLIGHT MANAGEMENT Alerts Window Text ALTITUDE SEL Oxygen system is left on after shutdown. Double Chime Oxygen quantity is low. None Anti-ice backup pump mode has been selected (TKS). None Check right fuel tank level. None Optional / * Not applicable to all models / TKS FIKI (optional)/ † GFC 700 required Table A-3 Advisory Alerts HAZARD AVOIDANCE Comparator Window Text ALT MISCOMP Condition Difference in altitude sensors is > 200 ft. If both airspeed sensors detect < 35 knots, this is inhibited. IAS MISCOMP If either airspeed sensor detects > 35 knots, and the difference in sensors is > 10 kts. ADDITIONAL FEATURES AFCS If either airspeed sensor detects > 80 knots, and the difference in sensors is > 7 kts. HDG MISCOMP Difference in heading sensors is > 6 degrees. PIT MISCOMP Difference in pitch sensors is > 5 degrees. ROL MISCOMP Difference in roll sensors is > 6 degrees. ALT NO COMP No data from one or both altitude sensors. IAS NO COMP No data from one or both airspeed sensors. HDG NO COMP No data from one or both heading sensors. PIT NO COMP No data from one or both pitch sensors. ROL NO COMP No data from one or both roll sensors.. APPENDICES Table A-4 Comparator Alerts (Dual AHRS and/or Dual Air Data Computer installations only) Reversionary Sensor Window Text Condition INDEX The PFD is displaying data from the #2 Air Data Computer. USING ADC2 The PFD is displaying data from the #2 AHRS. USING AHRS2 Table A-5 Reversionary Sensor Alerts (Dual AHRS and/or Dual Air Data Computer installations only) 520 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix A SYSTEM OVERVIEW NOTE: The ice protection system (optional) must be operated in accordance with the approved flight manual limitations. This option is only available on the SR22 models. Audio Alert EIS None AUDIO PANEL & CNS ANTI ICE QTY – Fluid quantity is low (TKS) CO DET FAIL – The carbon monoxide detector is inoperative CO DET SRVC – The carbon monoxide detector needs service ESP CONFIG† – ESP config error. Config service req'd. ESP FAIL† – ESP is inoperative. ESP OFF† – ESP selected off. ESP DEGRADE† – ESP IAS mode is inoperative. EXIT ICING – Exit icing conditions FAILED PATH – An autopilot servo data path has failed MFD FAN FAIL – MFD cooling fan is inoperative. PFD FAN FAIL – PFD cooling fan is inoperative. FLIGHT INSTRUMENTS Alerts Window Message FLIGHT MANAGEMENT Optional/ TKS NH (optional)/ TKS FIKI (optional)/ † GFC 700 required Table A-6 Message Advisory Alerts Perspective™ Voice Alerts 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 Issued when the airspeed is low and the autopilot is engaged Issued when the aircraft transitions beyond the set altitude limit Table A-7 Voice Alerts AFCS Voice Alert “Minimums, Minimums” “Vertical Track” "Airspeed" “Altitude” HAZARD AVOIDANCE The following audio alerts are announced by the system using a voice of male or female gender. If the optional Terrain Awareness and Warning System is installed, voice alerts are also generated (refer to the TAWS Alerts section). ADDITIONAL FEATURES 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. APPENDICES 3) Turn the large FMS Knob to highlight the voice in the Audio Alert Box. 4) Turn the small FMS Knob to select the desired voice, press the ENT Key. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 521 SYSTEM OVERVIEW Appendix A GTS 800 Traffic Advisory System Voice Alerts FLIGHT INSTRUMENTS The optional GTS 800 Traffic Advisory System (TAS) issues alerts using a male or female voice. The voice alert gender is configured at installation. EIS Voice Alert Alert Trigger “TAS System Test Passed" GTS system has passed a pilot-initiated system test. “TAS System Test Failed" GTS system has failed a pilot-initiated system test. “Traffic” Issued each time a new traffic advisory (TA) occurs. Table A-8 GTS 800 System Voice Alerts FLIGHT MANAGEMENT AUDIO PANEL & CNS Each time a new traffic advisory occurs, the GTS 800 system provides descriptive aural information to assist the pilot in visually locating TA traffic in the following format: Bearing, Relative Altitude, Distance. Bearing Relative Altitude Distance (nm) “One o’clock” through “Twelve o’clock” or “No Bearing” “High”, “Low”, “Same Altitude” (if within 200 feet of own altitude), or “Altitude not available” “Less than one mile”, “One Mile” through “Ten Miles”, or “More than ten miles” Table A-9 GTS 800 Descriptive TA Voice Alerts HAZARD AVOIDANCE System Annunciations NOTE: Upon power-up, certain windows remain invalid as Perspective™ equipment begins to initialize. All windows should be operational within one minute of power-up. If any window continues to remain flagged, the Perspective™ System should be serviced by a Garmin-authorized repair facility. INDEX APPENDICES ADDITIONAL FEATURES AFCS 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 Pilot’s Operating Handbook (POH) for additional information regarding pilot responses to these annunciations. 522 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix A SYSTEM OVERVIEW GIA 63W Integrated Avionics Units FLIGHT INSTRUMENTS GEA 71 Engine Airframe Unit OR GIA 63W Integrated Avionics Unit (A Failed GDC 74A Displays a Red-X Over the Percent Power Gauge in the SR22) EIS GDC 74A Air Data Computer Database Mismatch in PFD and MFD GRS 77 AHRS OR GMU 44 Magnetometer GTX 33 Transponder OR GIA 63W Integrated Avionics Units FLIGHT MANAGEMENT GDC 74A Air Data Computer AUDIO PANEL & CNS GIA 63W Integrated Avionics Units Figure A-6 System Failure Annunciations HAZARD AVOIDANCE 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. AFCS 2) To place the cursor in the ‘LRU Info’ Box, a) Select the LRU Softkey. Or: ADDITIONAL FEATURES a) Press the MENU Key. 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. APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 523 SYSTEM OVERVIEW Appendix A System Annunciation Comment System Annunciation FLIGHT INSTRUMENTS Attitude and Heading Reference System is aligning. Display system is not receiving vertical speed input from the air data computer. ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS Display system is not receiving attitude information from the AHRS. APPENDICES Comment Display system is not receiving valid heading input from AHRS. AHRS calibration incomplete or configuration module failure. Display system is not receiving altitude input from the air data computer. 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 POH). Display system is not receiving valid true airspeed information from air data computer. Display system is not receiving valid OAT information from air data computer. Display system is not receiving valid transponder information. 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. A cross-talk error between the PFD and MFD will also cause this annunciation. A red ‘X’ through any other display field (such as engine instrumentation fields) indicates that the field is not receiving valid data. Other Various Red X Indications INDEX Display system is not receiving airspeed input from air data computer. 524 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix A SYSTEM OVERVIEW System Message Advisories NOTE: This section provides information regarding Perspective™ message advisories that may be displayed FLIGHT INSTRUMENTS by the 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 Perspective™ 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 Perspective™ System Annunciations section. The PFD and/or MFD self-test has detected a problem. The Perspective™ system should be serviced. FLIGHT MANAGEMENT The PFD and/or MFD has incorrect software installed. The Perspective™ system should be serviced. HAZARD AVOIDANCE The PFD configuration settings do not match backup configuration memory. The Perspective™ system should be serviced. The MFD configuration settings do not match backup configuration memory. The Perspective™ system should be serviced. The MFD and PFD have different software versions installed. The Perspective™ system should be serviced. AFCS ADDITIONAL FEATURES The PFD and/or MFD is overheating and is reducing power consumption by dimming the display. If problem persists, the Perspective™ system should be serviced. A key is stuck on the PFD and/or MFD bezel. Attempt to free the stuck key by pressing it several times. The Perspective™ system should be serviced if the problem persists. APPENDICES The PFD1 configuration module backup memory has failed. The Perspective™ system should be serviced. The PFD1 voltage is low. The Perspective™ system should be serviced. INDEX 190-00820-06 Rev. A 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 Perspective™ 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 Perspective™ system should be serviced. Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 525 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 navigation database error exists. PFD1 DB ERR – PFD1 navigation 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. 526 Comments The MFD and/or PFD detected a failure in the aviation database. Attempt to reload the navigation database. If problem persists, the Perspective™ 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 Perspective™ 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 Perspective™ 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 Perspective™ 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 Perspective™ 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 Perspective™ 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 Perspective™ system should be serviced. Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix A SYSTEM OVERVIEW Comments The PFD and MFD have different navigation database versions installed. Crossfill is off. Install correct navigation database version in both displays. FLIGHT INSTRUMENTS Message Advisory DB MISMATCH – Navigation database version mismatch. Xtalk is off. DB MISMATCH – Navigation database type mismatch. Xtalk is off. EIS The PFD and MFD have different navigation database types installed (Americas, European, etc.). Crossfill is off. Install correct navigation database type in both displays. DB MISMATCH – Terrain database The PFD and MFD have different terrain database versions installed. Install correct version mismatch. terrain database version in both displays. DB MISMATCH – Terrain database The PFD and MFD have different terrain database types installed. Install correct type mismatch. terrain database type in both displays. DB MISMATCH – Obstacle database The PFD and MFD have different obstacle database versions installed. Install correct version mismatch. obstacle database version in both displays. DB MISMATCH – Airport Terrain The PFD and MFD have different airport terrain databases installed. Install correct database mismatch. airport terrain database in both displays. NAV DB UPDATED – Active System has updated the active navigation database from the standby navigation navigation database updated. database. TERRAIN DSP – [PFD1, MFD1] Terrain One of the terrain, airport terrain, or obstacle databases required for TAWS in the awareness display unavailable. specified PFD or MFD is missing or invalid. AUDIO PANEL & CNS FLIGHT MANAGEMENT GMA 347 Audio Panel AFCS 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 Perspective™ system should be serviced. The audio panel configuration settings do not match backup configuration memory. The Perspective™ system should be serviced. The audio panel has incorrect software installed. The Perspective™ 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 Perspective™ system should be serviced when possible. HAZARD AVOIDANCE Message Advisory GMA1 FAIL – GMA1 is inoperative. ADDITIONAL FEATURES GEA 71 Engine/Airframe Unit Comments The GEA1 configuration settings do not match those of backup configuration memory. The Perspective™ system should be serviced. The #1 GEA 71 has incorrect software installed. The Perspective™ system should be serviced. APPENDICES Message Advisory GEA1 CONFIG – GEA1 config error. Config service req’d. MANIFEST – GEA1 software mismatch, communication halted. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 527 SYSTEM OVERVIEW Appendix A GIA 63W Integrated Avionics Unit INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS 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. 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. 528 Comments The GIA1 and/or GIA2 configuration settings do not match backup configuration memory. The Perspective™ system should be serviced. The GIA1 and/or GIA2 have an error in the audio configuration. The Perspective™ system should be serviced. The GIA1 and/or GIA2 temperature is too low to operate correctly. Allow units to warm up to operating temperature. The GIA1 and/or GIA2 temperature is too high. If problem persists, the Perspective™ system should be serviced. The GIA1 and/or GIA2 self-test has detected a problem in the unit. The Perspective™ system should be serviced. A GIA mismatch has been detected, where only one is SBAS capable. The GIA1 and/or GIA 2 has incorrect software installed. The Perspective™ 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 Perspective™ system should be serviced. The system has detected a failure in COM1 and/or COM2. COM1 and/or COM2 may still be usable. The Perspective™ system should be serviced when possible. Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix A 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 Perspective™ system should be serviced. GPS integrity is insufficient for the current phase of flight. Loss of GPS navigation due to insufficient satellites. AUDIO PANEL & CNS Loss of GPS navigation due to position error. Loss of GPS navigation due to GPS failure. FLIGHT MANAGEMENT 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’. HAZARD AVOIDANCE A failure has been detected in the GPS1 and/or GPS2 receiver. The receiver may still be available. The Perspective™ system should be serviced. AFCS A failure has been detected in the NAV1 and/or NAV2 receiver. The receiver may still be available. The Perspective™ system should be serviced. ADDITIONAL FEATURES 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 Perspective™ system should be serviced. APPENDICES A failure has been detected in glideslope receiver 1 and/or receiver 2. The Perspective™ system should be serviced. A failure has been detected in glideslope receiver 1 and/or receiver 2. The receiver may still be available. The Perspective™ system should be serviced when possible. Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX 190-00820-06 Rev. A 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 Perspective™ system should be serviced. EIS 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 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. 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. 529 SYSTEM OVERVIEW Appendix A GDL 69/69A Satellite Datalink Receiver Comments GDL 69 configuration settings do not match those of backup configuration memory. The Perspective™ system should be serviced. A failure has been detected in the GDL 69. The receiver is unavailable. The Perspective™ system should be serviced. MANIFEST – GDL software mismatch, The GDL 69 has incorrect software installed. The Perspective™ system should be communication halted. serviced. FLIGHT INSTRUMENTS Message Advisory GDL69 CONFIG – GDL 69 config error. Config service req’d. GDL69 FAIL – GDL 69 has failed. EIS GTX 32/33 Transponder FLIGHT MANAGEMENT AUDIO PANEL & CNS Message Advisory Comments XPDR1 CONFIG – XPDR1 config error. The transponder configuration settings do not match those of backup configuration Config service req’d. memory or the Mode S address is invalid. The Perspective™ system should be serviced. MANIFEST – GTX1 software The transponder has incorrect software installed. The Perspective™ system should be mismatch, communication halted. serviced. XPDR1 SRVC – XPDR1 needs service. The #1 transponder should be serviced when possible. Return unit for repair. XPDR1 FAIL – XPDR1 is inoperative. There is no communication with the #1 transponder. HAZARD AVOIDANCE GDC 74A Air Data Computer APPENDICES ADDITIONAL FEATURES AFCS Message Advisory ADC1 ALT EC – ADC1 altitude error correction is unavailable. ADC2 ALT EC – ADC2 altitude error correction is unavailable. ADC1 AS EC – ADC1 airspeed error correction is unavailable. ADC2 AS EC – ADC2 airspeed error correction is unavailable. MANIFEST – GDC1 software mismatch, communication halted. MANIFEST – GDC2 software mismatch, communication halted. Comments GDC1 or GDC2 is reporting that the altitude error correction is unavailable. GDC1 or GDC2 is reporting that the airspeed error correction is unavailable. The GDC 74A has incorrect software installed. The Perspective™ system should be serviced. GRS 77 Attitude and Heading Reference System INDEX Message Advisory AHRS1 TAS – AHRS1 not receiving valid airspeed. AHRS2 TAS – AHRS2 not receiving valid airspeed. 530 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 Perspective™ system should be serviced. The #2 AHRS is not receiving true airspeed from the air data computer. The AHRS relies on GPS information to augment the lack of airspeed. The Perspective™ system should be serviced. Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix A SYSTEM OVERVIEW Comments The #1 AHRS is using the backup GPS path. Primary GPS path has failed. The Perspective™ system should be serviced when possible. The #2 AHRS is using the backup GPS path. Primary GPS path has failed. The Perspective™ system should be serviced when possible. The #1 AHRS is not receiving any or any useful GPS information. Check AFMS limitations. The Perspective™ system should be serviced. The #2 AHRS is not receiving any or any useful GPS information. Check AFMS limitations. The Perspective™ system should be serviced. The #1 AHRS is not receiving backup GPS information. The Perspective™ system should be serviced. The #2 AHRS is not receiving backup GPS information. The Perspective™ system should be serviced. The #1 AHRS is operating exclusively in no-GPS mode. The Perspective™ system should be serviced. The #2 AHRS is operating exclusively in no-GPS mode. The Perspective™ system should be serviced. The #1 AHRS earth magnetic field model is out of date. Update magnetic field model when practical. The #1 AHRS earth magnetic field model is out of date. Update magnetic field model when practical. The #2 AHRS earth magnetic field model is out of date. Update magnetic field model when practical. FLIGHT INSTRUMENTS EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE The aircraft is outside geographical limits for approved AHRS operation. Heading is flagged as invalid. AFCS The #1 AHRS has incorrect software installed. The Perspective™ system should be serviced. The #2 AHRS has incorrect software installed. The Perspective™ system should be serviced. ADDITIONAL FEATURES Message Advisory AHRS1 GPS – AHRS1 using backup GPS source. AHRS2 GPS – AHRS2 using backup GPS source. AHRS1 GPS – AHRS1 not receiving any GPS information. AHRS2 GPS – AHRS2 not receiving any GPS information. AHRS1 GPS – AHRS1 not receiving backup GPS information. AHRS2 GPS – AHRS2 not receiving backup GPS information. AHRS1 GPS – AHRS1 operating exclusively in no-GPS mode. AHRS2 GPS – AHRS2 operating exclusively in no-GPS mode. AHRS MAG DB – AHRS magnetic model database version mismatch. AHRS1 SRVC – AHRS1 Magnetic-field model needs update. AHRS2 SRVC – AHRS2 Magnetic-field model needs update. GEO LIMITS – AHRS1 too far North/ South, no magnetic compass. GEO LIMITS – AHRS2 too far North/ South, no magnetic compass. MANIFEST – GRS1 software mismatch, communication halted. MANIFEST – GRS2 software mismatch, communication halted. GCU 478 PFD/MFD Control Unit Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX 190-00820-06 Rev. A Comments GCU 478 configuration settings do not match those of backup configuration memory. The Perspective™ system should be serviced. A failure has been detected in the GCU 478. The GCU 478 is unavailable. The GCU 478 has incorrect software installed. The Perspective™ system should be serviced. A key is stuck on the GCU 478 bezel. Attempt to free the stuck key by pressing it several times. The Perspective™ system should be serviced if the problem persists. APPENDICES Message Advisory GCU CNFG – GCU Config error. Config service req’d. GCU FAIL – GCU is inoperative. MANIFEST – GCU software mismatch, communication halted. GCU KEYSTK – GCU [key name] Key is stuck. 531 SYSTEM OVERVIEW Appendix A GMC 705 AFCS Control Unit EIS FLIGHT INSTRUMENTS Message Advisory GMC CONFIG – GMC Config error. Config service req’d. GCU FAIL – GCU is inoperative. MANIFEST – GMC software mismatch, communication halted. GCU KEYSTK – GCU [key name] Key is stuck. Comments Error in the configuration of the GMC 705. A failure has been detected in the GMC 705. The GMC 705 is unavailable. The GMC 705 has incorrect software installed. The Perspective™ system should be serviced. A key is stuck on the GMC 705 bezel. Attempt to free the stuck key by pressing it several times. The Perspective™ system should be serviced if the problem persists. GMU 44 Magnetometer FLIGHT MANAGEMENT AUDIO PANEL & CNS Message Advisory HDG FAULT – AHRS1 magnetometer fault has occurred. HDG FAULT – AHRS2 magnetometer fault has occurred. MANIFEST – GMU1 software mismatch, communication halted. MANIFEST – GMU2 software mismatch, communication halted. Comments A fault has occurred in the #1 GMU 44. Heading is flagged as invalid. The AHRS uses GPS for backup mode operation. The Perspective™ system should be serviced. A fault has occurred in the #2 GMU 44. Heading is flagged as invalid. The AHRS uses GPS for backup mode operation. The Perspective™ system should be serviced. The GMU 44 has incorrect software installed. The Perspective™ system should be serviced. HAZARD AVOIDANCE GTS 800 TRAFFIC ADVISORY SYSTEM AFCS Message Advisory GTS CONFIG – GTS Config error. Config service req'd. MANIFEST – GTS software mismatch, communication halted. Comments The GTS and GDU have different copies of the GTS configuration, or the Mode S address is invalid. The Perspective™ system should be serviced. The GTS has incorrect software installed. The Perspective™ system should be serviced. Miscellaneous INDEX APPENDICES ADDITIONAL FEATURES Message Advisory Comments FPL WPT LOCK – Flight plan waypoint Upon power-up, the system detects that a stored flight plan waypoint is locked. This is locked. occurs when an navigation database update eliminates an obsolete waypoint. The flight plan cannot find the specified waypoint and flags this message. This can also occur with user waypoints in a flight plan that is deleted. Remove the waypoint from the flight plan if it no longer exists in any database, OR update the waypoint name/identifier to reflect the new information. FPL WPT MOVE – Flight plan The system has detected that a waypoint coordinate has changed due to a new waypoint moved. navigation 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. 532 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix A FPL TRUNC – Flight plan has been truncated. Special use airspace is near and ahead of the aircraft position. Special use airspace is within 2 nm of the aircraft position. The system notifies the pilot that the loaded approach is not active. Activate approach when required. The system notifies the pilot to load the approach frequency for the appropriate NAV receiver. Select the correct frequency for the approach. The system notifies the pilot to set the CDI to the correct NAV receiver. Set the CDI to the correct NAV receiver. AFCS Bad parallel track geometry. ADDITIONAL FEATURES Invalid leg type for parallel offset. IAF waypoint for parallel offset has been passed. The current vertical waypoint can not be reached within the maximum flight path angle and vertical speed constraints. The system automatically transitions to the next vertical waypoint. The lateral flight plan contains a procedure turn, vector, or other unsupported leg type prior to the active vertical waypoint. This prevents vertical guidance to the active vertical waypoint. INDEX Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T APPENDICES 190-00820-06 Rev. A A steep turn is 15 seconds ahead. Prepare to turn. The aircraft is inside the airspace. Special use airspace is ahead of aircraft. The aircraft will penetrate the airspace within 10 minutes. HAZARD AVOIDANCE VNV – Unavailable. Unsupported leg type in flight plan. Arriving at waypoint [xxxx], where [xxxx] is the waypoint name. FLIGHT MANAGEMENT SLCT FREQ – Select appropriate frequency for approach. SLCT NAV – Select NAV on CDI for approach. PTK FAIL – Parallel track unavailable: bad geometry. PTK FAIL – Parallel track unavailable: invalid leg type. PTK FAIL – Parallel track unavailable: past IAF. UNABLE V WPT – Can’t reach current vertical waypoint. AUDIO PANEL & CNS WPT ARRIVAL – Arriving at waypoint -[xxxx] STEEP TURN – Steep turn ahead. INSIDE ARSPC – Inside airspace. ARSPC AHEAD – Airspace ahead less than 10 minutes. ARSPC NEAR – Airspace near and ahead. ARSPC NEAR – Airspace near – less than 2 nm. APR INACTV – Approach is not active. EIS LOCKED FPL – Cannot navigate locked flight plan. Comments This occurs when a stored flight plan contains procedures that have been manually edited. This alert is issued only after an navigation database update. Verify that the user-modified procedures in stored flight plans are correct and up to date. This occurs when a stored flight plan contains an airway that is no longer consistent with the navigation database. This alert is issued only after a navigation database update. Verify use of airways in stored flight plans and reload airways as needed. This occurs when a newly installed navigation database eliminates an obsolete approach or arrival used by a stored flight plan. The obsolete procedure is removed from the flight plan. Update flight plan with current arrival or approach. This occurs when the pilot attempts to activate a stored flight plan that contains locked waypoint. Remove locked waypoint from flight plan. Update flight plan with current waypoint. FLIGHT INSTRUMENTS DB CHANGE – Database changed. Verify stored airways. SYSTEM OVERVIEW Message Advisory DB CHANGE – Database changed. Verify user modified procedures. 533 SYSTEM OVERVIEW Appendix A EIS FLIGHT INSTRUMENTS Message Advisory VNV – Unavailable. Excessive crosstrack error. VNV – Unavailable. Excessive track angle error. VNV – Unavailable. Parallel course selected. NON WGS84 WPT – Do not use GPS for navigation to [xxxx]. FLIGHT MANAGEMENT AUDIO PANEL & CNS TRAFFIC FAIL – Traffic device has failed. STRMSCP FAIL – Stormscope has failed. FAILED PATH – A data path has failed. FAILED PATH – An autopilot servo data path has failed. MAG VAR WARN – Large magnetic variance. Verify all course angles. Comments The current crosstrack exceeds the limit, causing vertical deviation to go invalid. The current track angle error exceeds the limit, causing the vertical deviation to go invalid. A parallel course has been selected, causing the vertical deviation to go invalid. The position of the selected waypoint [xxxx] is not calculated based on the WGS84 map reference datum and may be positioned in error as displayed. Do not use GPS to navigate to the selected non-WGS84 waypoint. The system is no longer receiving data from the traffic system. The traffic device should be serviced. Stormscope has failed. The Perspective™ System should be serviced. A data path connected to the GDU or the GIA 63/63W has failed. A data path connected to an autopilot servo has failed. ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE The GDU’s internal model cannot determine the exact magnetic variance for geographic locations near the magnetic poles. Displayed magnetic course angles may differ from the actual magnetic heading by more than 2°. SCHEDULER [#] – . Message criteria entered by the user is displayed 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. CHECK CRS – Database course for Selected course for LOC1 differs from published localizer course by more than 10 LOC1 / [LOC ID] is [CRS]°. degrees. CHECK CRS – Database course for Selected course for LOC2 differs from published localizer course by more than 10 LOC2 / [LOC ID] is [CRS]°. degrees. [PFD1 or MFD1] CARD 1 REM – Card The SD card was removed from the top card slot of the specified PFD or MFD. The SD 1 was removed. Reinsert card. card needs to be reinserted. The SD card was removed from the bottom card slot of the specified PFD or MFD. The SD card needs to be reinserted. The SD card in the top card slot of the specified PFD or MFD contains invalid data. The SD card in the bottom card slot of the specified PFD or MFD contains invalid data. INDEX APPENDICES [PFD1 or MFD1] CARD 2 REM – Card 2 was removed. Reinsert card. [PFD1 or MFD1] CARD 1 ERR – Card 1 is invalid. [PFD1 or MFD1] CARD 2 ERR – Card 2 is invalid. 534 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix A SYSTEM OVERVIEW GFC 700 AFCS Alerts FLIGHT INSTRUMENTS The following annunciations (listed in order of increasing priority) can appear on the PFD between 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-7 AFCS Status Annunciation Alert Condition Annunciation Rudder Mistrim Left Aileron Mistrim Right Elevator Mistrim Down Elevator Mistrim Up Pitch Trim Failure Pitch servo providing sustained force in the indicated direction Displayed when the AFCS enters Automatic Descent Mode as a result of the Hypoxia Recognition System detecting pilot incapacitation. When this mode is active, a continuous repeating chime is heard. If AP engaged, take control of the aircraft and disengage AP If AP disengaged, move MET switch to unstick YD control failure Roll axis control failure; AP inoperative Pitch Failure Pitch axis control failure 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 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. INDEX Preflight Test APPENDICES Roll Failure System Failure ADDITIONAL FEATURES Yaw Damper Failure Roll servo providing sustained force in the indicated direction AFCS Automatic Descent Mode Yaw servo providing sustained force in the indicated direction HAZARD AVOIDANCE Aileron Mistrim Left FLIGHT MANAGEMENT Rudder Mistrim Right Description Preflight system test failed; aural alert sounds at failure 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 535 SYSTEM OVERVIEW Appendix A GFC 700 Speed Condition/Stall Alert FLIGHT INSTRUMENTS The following annunciations can appear on the PFD directly above the Airspeed indicator. EIS Airspeed Indicator Figure A-8 Overspeed Annunciation Annunciation Description Overspeed Flashing annunciation indicating aircraft overspeed condition. The autopilot, if engaged, will follow the pitch up command for the flight director. Engine power should be reduced and/or the pitch reference adjusted to slow the aircraft. The annunciation disappears when the overspeed condition is resolved. Underspeed/Stall Flashing annunciation indicating aircraft underspeed or imminent stall condition. An underspeed condition initiates flight director commands for pitch down and, if engaged, the autopilot will follow the pitch down command. Engine power should be increased and/or the pitch reference adjusted to increase airspeed. A stall condition causes the flight director to capture the Stall Warning Reference Airspeed (i.e., the speed at which Stall Warning Mode was entered) and commands a pitch attitude to follow the reference speed. The Stall Warning Reference Airspeed is increased at a rate of one kt/sec. The annunciation disappears when the condition is resolved. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS Condition Terrain-SVS Alerts AFCS Annunciations appear on the PFD and MFD. Pop-up alerts appear only on the MFD. For more information on Terrain-SVS, refer to the Hazard Avoidance Section. INDEX APPENDICES ADDITIONAL FEATURES Alert Type 536 PFD/MFD TERRAIN-SVS Page Annunciation MFD Pop-Up Alert (except TERRAIN-SVS Page) Aural Message Reduced Required Terrain Clearance Warning (RTC) “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” Reduced Required Terrain Clearance Caution (RTC) “Caution; Terrain, Terrain” 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” Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix A SYSTEM OVERVIEW Terrain-SVS System Status Annunciations None None Single Chime None None TERRAIN DATABASE FAILURE None Terrain System Test Fail TERRAIN FAIL “Terrain System Failure” Terrain or Obstacle database unavailable or invalid, invalid software configuration, system audio fault TERRAIN FAIL “Terrain System Failure” NO GPS POSITION “Terrain System Not Available” None “Terrain System Not Available” None “Terrain System Available” System Test Pass None Terrain Alerting is disabled MFD Terrain or Obstacle database unavailable or invalid. Terrain-SVS operating with PFD Terrain or Obstacle databases None No GPS position Excessively degraded GPS signal, Out of database coverage area Sufficient GPS signal reception restored None FLIGHT MANAGEMENT TERRAIN TEST System Test in Progress AUDIO PANEL & CNS Aural Message EIS TERRAIN-SVS Page Center Banner Annunciation FLIGHT INSTRUMENTS PFD/MFD TERRAIN-SVS Page Annunciation Alert Type TAWS-B ALERTS Alert Type PFD/MFD TAWS-B Page Annunciation MFD Pop-Up Alert (except TAWS-B Page) Reduced Required Terrain Clearance Warning (RTC) Aural Message “Pull Up” Reduced Required Obstacle Clearance Warning (ROC) or “Obstacle, Obstacle; Pull Up, Pull Up” or “Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up” Imminent Obstacle Impact Warning (IOI) or “Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up” or “Obstacle, Obstacle; Pull Up, Pull Up” Reduced Required Terrain Clearance Caution (RTC) or “Caution, Terrain; Caution, Terrain” or “Terrain Ahead; Terrain Ahead” 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX or Terrain Ahead, Pull Up; Terrain Ahead, Pull Up” or “Terrain, Terrain; Pull Up, Pull Up” Imminent Terrain Impact Warning (ITI) APPENDICES “Terrain, Terrain; Pull Up, Pull Up” or “Terrain Ahead, Pull Up; Terrain Ahead, Pull Up” ADDITIONAL FEATURES or AFCS Excessive Descent Rate Warning (EDR) HAZARD AVOIDANCE Annunciations appear on the PFD and MFD. Pop-up alerts appear only on the MFD when the TAWS-B page is not in view. For more information on TAWS-B, refer to the Hazard Avoidance Section. 537 SYSTEM OVERVIEW Appendix A MFD Pop-Up Alert (except TAWS-B Page) Aural Message or “Terrain Ahead; Terrain Ahead” or “Caution, Terrain; Caution, Terrain” Reduced Required Obstacle Clearance Caution (ROC) or “Caution, Obstacle; Caution, Obstacle” or “Obstacle Ahead; Obstacle Ahead” Imminent Obstacle Impact Caution (IOI) or “Obstacle Ahead; Obstacle Ahead” or “Caution, Obstacle; Caution, Obstacle” Alert Type PFD/MFD TAWS-B Page Annunciation EIS FLIGHT INSTRUMENTS Imminent Terrain Impact Caution (ITI) AUDIO PANEL & CNS Premature Descent Alert Caution (PDA) Altitude Callout “500” “Too Low, Terrain” None None “Five-Hundred” Excessive Descent Rate Caution (EDR) “Sink Rate” Negative Climb Rate Caution (NCR) “Don’t Sink” or “Too Low, Terrain” FLIGHT MANAGEMENT or TAWS-B System Status Annunciations HAZARD AVOIDANCE Alert Type PFD/MFD Alert Annunciation AFCS System Test in Progress Aural Message TAWS TEST None System Test Pass None None Single Chime MFD Terrain or Obstacle database unavailable or invalid. TAWS operating with PFD Terrain or Obstacle databases None TERRAIN DATABASE FAILURE None TAWS-B System Test Fail TAWS FAIL “TAWS System Failure” Terrain or Obstacle database unavailable or invalid, invalid software configuration, system audio fault TAWS FAIL “TAWS System Failure” NO GPS POSITION “TAWS Not Available” None “TAWS Not Available” None “TAWS Available” No GPS position ADDITIONAL FEATURES TAWS-B Page Center Banner Annunciation Excessively degraded GPS signal, Out of database coverage area None INDEX APPENDICES Sufficient GPS signal reception restored 538 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix A SYSTEM OVERVIEW Flight plan Import/Export Messages In some circumstances, some messages may appear in conjunction with others. ‘User waypoint database full. Not all loaded.’ ‘Flight plan successfully exported.’ ‘Flight export failed.’ HAZARD AVOIDANCE ‘One or more user waypoints renamed.’ FLIGHT MANAGEMENT ‘Some waypoints not loaded. Waypoints locked.’ AUDIO PANEL & CNS ‘Too many points. Flight plan truncated.’ EIS ‘File contained user waypoints only.’ Description A flight plan file stored on the SD card was successfully imported as a stored flight plan. The file stored on the SD card did not contain a flight plan, only user waypoints. These waypoints have been saved to the system user waypoints. No flight plans stored in the system have been modified. The SD card contains no flight plan data. Flight plan data was not successfully imported from the SD card. Some flight plan waypoints were successfully imported from the SD card, however others had errors and were not imported. A partial stored flight plan now exists in the system. The file stored on the SD card did not contain a flight plan, only user waypoints. One or more of these waypoints did not import successfully. The flight plan on the SD card contains more waypoints than the system can support. The flight plan was imported with as many waypoints as possible. The flight plan on the SD card contains one or more waypoints that the system cannot find in the navigation database. The flight plan has been imported, but must be edited within the system before it can be activated for use. The flight plan file on the SD card contains user waypoints. The quantity of stored user waypoints has exceeded system capacity, therefore not all the user waypoints on the SD card have been imported. Any flight plan user waypoints that were not imported are locked in the flight plan. The flight plan must be edited within the system before it can be activated for use. One or more imported user waypoints were renamed when imported due to naming conflicts with waypoints already existing in the system. The stored flight plan was successfully exported to the SD card. The stored flight plan was not successfully exported to the SD card. The SD card may not have sufficient available memory or the card may have been removed prematurely. FLIGHT INSTRUMENTS Flight Plan Import/Export Results ‘Flight plan successfully imported.’ ‘File contained user waypoints only. User waypoints imported successfully. No stored flight plan data was modified.’ ‘No flight plan files found to import.’ ‘Flight plan import failed.’ ‘Flight plan partially imported.’ AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 539 INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Appendix A Blank Page 540 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix B SYSTEM OVERVIEW Database Management FLIGHT INSTRUMENTS The system uses Secure Digital (SD) cards to load and store various types of data. For basic flight operations, SD cards are required for database storage as well as Jeppesen navigation and Jeppesen ChartView database updates. Not all SD cards are compatible with the Perspective™. Use only SD cards supplied by Garmin or Cirrus. CAUTION: When downloading updates to the Jeppesen Navigation Database, copy the data to an SD card other than a Garmin Supplemental Data Card. Otherwise, data corruption can occur. Garmin Databases EIS The following databases are stored on Supplemental Data Cards provided by Garmin: • Airport terrain • SafeTaxi • Terrain • Obstacle • FliteCharts • Airport Directory (AOPA) AUDIO PANEL & CNS • Expanded basemap Bottom Card Slot HAZARD AVOIDANCE Bottom Card Slot FLIGHT MANAGEMENT After subscribing to the desired database product updates, a personal computer is used to copy these updated databases to the Supplemental Data Card which will reside in the bottom card slot of the MFD (this is also the card that contains the FliteCharts or ChartView database). This allows taking all applicable databases to the airplane on one card and using the Perspective™ system to update the remaining display Supplemental Data Cards. Figure B-1 illustrates the correct location of the Supplemental Data Cards and their respective databases. Since these databases are not stored internally in the displays, these Supplemental Data Cards must remain in the bottom card slot of each display. AFCS ADDITIONAL FEATURES MFD PFD APPENDICES Figure B-1 Correct Database Locations 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX 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. 541 SYSTEM OVERVIEW Appendix B The terrain database contains the terrain mapping data. The airport terrain database contains increased resolution terrain data around airports. These databases are updated periodically and have no expiration date. FLIGHT INSTRUMENTS The obstacle database contains data for obstacles, such as towers, that pose a potential hazard to aircraft. Obstacles 200 feet and higher are included in the obstacle database. It is very important to note that not all obstacles are necessarily charted and therefore may not be contained in the obstacle database. This database is updated on a 56-day cycle. NOTE: The data contained in the terrain and obstacle databases comes from government agencies. Garmin EIS accurately processes and cross-validates the data, but cannot guarantee the accuracy and completeness of the data. AUDIO PANEL & CNS The AOPA Airport Directory provides data on airports and heliports throughout the U.S., and offers detailed information for over 5,300 U. S. airports, along with the names and phone numbers of thousands of FBOs. This database is updated four times per year and has no expiration date 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. FLIGHT MANAGEMENT The FliteCharts database contains procedure charts for the United States only. This database is updated on a 28-day cycle. If not updated within 180 days of the expiration date, FliteCharts will no longer function. Obtaining Garmin Database Updates HAZARD AVOIDANCE The Garmin database updates can be obtained by following the instructions detailed in the ‘Aviation Databases’ section of the Garmin website (fly.garmin.com). Once the updated files have been downloaded from the website, a PC equipped with an appropriate SD card reader is used to unpack and copy the new databases onto the appropriate Supplemental Data Card. Equipment required to perform the update is as follows: AFCS • Windows-compatible PC computer (Windows 2000 or XP recommended) • SD Card Reader: SanDisk SDDR-93, SanDisk SDDR-99, Verbatim #96504, or equivalent • Updated database obtained from the Garmin website ADDITIONAL FEATURES • Existing Supplemental Database SD Card (010-00330-41, -42, or -43) from the MFD. The supplemental data card from the MFD should be used because all databases (except the active navigation database) are required to reside on this card. APPENDICES Jeppesen Databases The Jeppesen navigation database is updated on a 28-day cycle. The ChartView database is updated on a 14-day cycle. If the ChartView database is not updated within 70 days of the expiration date, ChartView will no longer function. Both of these databases are provided directly from Jeppesen. Note: The Jeppesen aviation navigation database is now referred to as the ‘navigation database’. Previously INDEX this database had been referred to as the ‘aviation database’. 542 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix B SYSTEM OVERVIEW The ChartView database should be copied to the Supplemental Data Card which will reside in the bottom card slot on the MFD. The navigation database is be loaded from the Jeppesen or user supplied SD data card. Contact Jeppesen (www.jeppesen.com) for subscription and update information. FLIGHT INSTRUMENTS Navigation Database The system allows each display to store a future update to the navigation database as the standby navigation database. The standby navigation database resides on the bottom SD card so it can be automatically loaded to internal memory as the active database when the new database becomes effective (the next cycle becomes available seven days prior to its effective date). Automatic loading of the active navigation database can only occur while the aircraft is on the ground. EIS AUDIO PANEL & CNS If an SD card containing a navigation database is inserted into the top SD card slot of a display, and a Supplemental Data Card is in the bottom slot, the system will prompt the user (upon power up) as to how the database should be stored. If the user responds affirmatively (YES) to the first prompt, the system will copy the navigation database from the top SD card to the bottom SD card as the standby navigation database. As long as the bottom SD card remains in the bottom card slot, this standby navigation database will be available for the system to use as the active database as soon as the effective date is reached, and power is cycled while the aircraft is on the ground. If the user responds negatively (NO), the system will display a second prompt to load the database into the internal memory of that display as the active database. Loading the new navigation database as the active database necessitates placing the SD card in the top card slot of each display and repeating the load process. FLIGHT MANAGEMENT HAZARD AVOIDANCE The system checks the active and standby navigation databases upon (on-ground only) power-up. If the effective date of the standby database has passed, and the active database is out of date, the system will load the standby database into the internal system memory as the active navigation database. Loading the standby database to the active location takes approximately 45-55 seconds. The pilot is alerted that the update is complete by a system alert message, ‘NAV DB UPDATED’. Automatic Database Synchronization AFCS The automatic database synchronization feature automatically transfers the databases from a single SD card residing in the bottom card slot of the MFD to the SD card in the bottom card slot of the PFD to ensure that all databases are synchronized. During power-up, the system compares all copies of each applicable database. If similar databases do not match, the most recent valid database is automatically copied to each card that does not already contain that database. ADDITIONAL FEATURES NOTE: Garmin recommends enabling the automatic database synchronization feature to protect against database mismatches. APPENDICES 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX The following databases are checked and synchronized: Standby Navigation, Basemap, Safetaxi, Airport Terrain, Obstacle, Airport Directory (AOPA), and Terrain. This feature applies only to databases that are stored on the SD card that resides in the bottom card slot of each display. This feature does not apply to the active navigation database which is stored in internal memory in each display, or to the charts databases (FliteCharts and ChartView) which are only required to reside on the SD card in the bottom card slot of the MFD. The typical procedure would be to copy new databases to the MFD card, then synchronize the data to the PFD. Perform this procedure only when the aircraft is on the ground. 543 SYSTEM OVERVIEW Appendix B NOTE: The terrain database may take as long as 100 minutes to synchronize using this method. Therefore FLIGHT INSTRUMENTS the user may want to transfer the data using a PC, or connect the system to a ground power source while performing the database synchronization. EIS The SYNC DBS Softkey (Figure B-2) on the AUX–System Status Page allows control of the automatic database synchronization feature. When database synchronization is enabled, the SYNC DBS Softkey is displayed as black text on gray background. When database synchronization is disabled, the softkey is displayed as white text on black background. If the SYNC DBS Softkey is pressed while a database synchronization is in progress, the current synchronization process will be canceled. Enabled Disabled AUDIO PANEL & CNS Figure B-2 SYNC DBS Softkey ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT The synchronization progress may be monitored on the AUX-System Status Page in the Sync Status section of the Database Window (Figure B-3). This window shows the synchronization status of each applicable database, including the percent complete, time remaining, and to which displays the databases are being copied. The Sync Status section is only present when synchronization is occurring or has occurred on the current power-up. When the synchronization is complete, the status is listed as ‘Complete’, followed by the displays to which the databases were copied. The database cycle numbers should be checked for each database on each display after synchronization to verify the display contains the proper database version. INDEX APPENDICES Sync Status Section Figure B-3 AUX-System Status Page, Database Window 544 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix B SYSTEM OVERVIEW Unselected FLIGHT INSTRUMENTS The Display Database Selection Softkey (Figure B-4) is used to place the cursor in the Database Window. Upon first press of the Display Database Selection Softkey, the softkey will change to a selected state (black text on gray background) and the cursor will appear in the Database Window. At this point the user can scroll through all databases in the Database Window to view status information. If the Display Database Selection Softkey is pressed repeatedly, the softkey will switch between PFD1 and MFD1. Database status information in the Database Window will reflect the database of the selected PFD or MFD. MFD1 DB Selected PFD1 DB Selected EIS Figure B-4 Display Database Selection Softkey AUDIO PANEL & CNS If an error occurs during synchronization, an error message will be displayed, followed by the affected display in the Sync Status section of the Database Window (Figure B-5). If synchronization completes on one display, but an error occurs on another, the error message will be displayed with the affected diaplays listed after it. When an error message (Table B-1) is displayed, the problem must be corrected before synchronization can be completed. A power cycle is required to restart synchronization when ‘Card Full’ or ‘Err’ is shown. FLIGHT MANAGEMENT HAZARD AVOIDANCE ‘Card Full’ Message Figure B-5 Synchronization Error Message AFCS Description An active synchronization has been canceled using the SYNC DBS Softkey SD card does not contain sufficient memory Displayed for all other errors that may cause the synchronization process to be halted System timed-out prior to the database transfer completing ADDITIONAL FEATURES Error Message Canceled Card Full Err Timeout Table B-1 Database Synchronization Error Messages APPENDICES Loading Updated Databases 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 545 SYSTEM OVERVIEW Appendix B Loading the Garmin database updates: 1) With system power OFF, remove the MFD database card from the bottom card slot of the MFD. FLIGHT INSTRUMENTS 2) Update the Garmin databases on the MFD card. 3) Insert the MFD database card into the bottom card slot of the MFD. FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 4) Apply power to the system, check that the databases are initialized and displayed on the power-up screen (Figure B-6). When updating the terrain and FliteCharts databases, a ‘Verifying’ message may be seen. If this message is present, wait for the system to finish loading before proceeding to step 5. HAZARD AVOIDANCE Figure B-6 Database Information on the Power-up Screen 5) Acknowledge the Power-up Page agreement by pressing the ENT Key or the right most softkey. 6) Turn the large FMS Knob to select the AUX Page group on the MFD. 7) Turn the small FMS Knob to select the System Status Page. AFCS 8) Make sure the SYNC DBS Softkey is in the enabled state (Figure B-2). 9) Monitor the Sync Status in the Database Window. Wait for all databases to complete synching, indicated by ‘Complete’ being displayed as seen in Figure B-5. ADDITIONAL FEATURES 10) Remove and reapply power to the system. 11) Turn the large FMS Knob to select the AUX Page group on the MFD. 12) Turn the small FMS Knob to select the System Status Page. APPENDICES 13) Press the Display Database Selection Softkey to show database information for each display (MFD1 DB, PFD1 DB). Verify the correct database cycle information is shown for each database for each display. Canceling an automatic database synchronization: INDEX 1) While synchronization is in progress, press the SYNC DBS Softkey to disable (Figure B-2) automatic database synchronization. 2) Acknowledge the cancelation by pressing the ENT Key. 546 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix B SYSTEM OVERVIEW Loading the Jeppesen navigation database as the active navigation database: NOTE: Loading the Jeppesen navigation database as the active database prior to its effective date will result FLIGHT INSTRUMENTS in the expiration date on the power-up screen and the effective date on the AUX-System Status Page being displayed in yellow. 1) With the system OFF, insert the SD card containing the new navigation database version into the top card slot of the display (PFD or MFD) to be updated (label of SD card facing left). 2) Turn the system ON. A prompt similar to the following is displayed in the upper left corner of the display: EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure B-7 Standby Navigation Database Prompt HAZARD AVOIDANCE 3) Press the NO Softkey to proceed to loading the active database. 4) A prompt similar to the following is displayed. Press the YES Softkey to update the active navigation database. AFCS ADDITIONAL FEATURES Figure B-8 Active Navigation Database Prompt 5) After the update completes, the display starts in normal mode. 6) Turn the system OFF and remove the SD card from the top card slot. APPENDICES 7) Repeat steps 1 through 6 for the other display (PFD or MFD). INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 547 SYSTEM OVERVIEW Appendix B 8) Apply power to the system and press the ENT Key to acknowledge the startup screen. 9) Turn the large FMS Knob to select the AUX Page group on the MFD. FLIGHT INSTRUMENTS 10) Turn the small FMS Knob to select the System Status Page. 11) Press the Display Database Selection Softkey to show active navigation database information for each display (MFD1 DB, PFD1 DB). Verify the correct active navigation database cycle information is shown for each display. Figure B-9 shows the active navigation database information for the MFD. HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS NOTE: After the navigation database is loaded or copied, the top SD card may be removed. Figure B-9 Check Database Cycle Number AFCS Loading the Jeppesen navigation database as the standby navigation database: 1) With the system OFF, insert the SD card containing the new navigation database version into the top card slot of the MFD. ADDITIONAL FEATURES 2) Verify that an SD card is inserted in the bottom slot of the PFD and MFD. INDEX APPENDICES 3) Turn the system ON. A prompt similar to Figure B-10 is displayed. Figure B-10 Standby Navigation Database Prompt 548 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix B SYSTEM OVERVIEW 4) Press the YES Softkey. The navigation database is copied to the SD card in the bottom card slot of the MFD. A prompt similar to Figure B-11 is displayed. FLIGHT INSTRUMENTS EIS Figure B-11 Active Navigation Database Prompt AUDIO PANEL & CNS 5) Press the NO Softkey. The display now starts in normal mode. Since the database effective date is not yet valid, it should not be loaded as the active database. 6) Press the ENT Key to acknowledge the startup screen. FLIGHT MANAGEMENT NOTE: During the synchronization process, version differences between standby navigation databases will exist. This will result in the system displaying a ‘DB Mismatch’ alert for the standby navigation databases. This alert will remain until the next power cycle. 7) Turn the large FMS Knob to select the AUX Page group on the MFD. HAZARD AVOIDANCE 8) Turn the small FMS Knob to select the System Status Page. 9) If necessary, press the SYNC DBS Softkey to enable database synchronization (Figure B-2). A confirmation box is displayed as shown in Figure B-12. If Database Synchronization has been enabled prior to this step, proceed to step 11. AFCS ADDITIONAL FEATURES Figure B-12 Enable Database Synchronization Prompt APPENDICES 10) With YES highlighted, press the ENT Key. 11) The new database is copied to the SD card in bottom card slot of the PFD. Progress can be monitored in the SYNC STATUS field as shown in Figure B-13. When copying is finished, ‘Complete’ is displayed as seen in Figure B-14. INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 549 AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Appendix B ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT Figure B-13 Copy Progress Figure B-14 Copy Complete 12) Turn system power OFF. APPENDICES 13) Remove the SD card from the top card slot of the MFD. 14) Turn system power ON. 15) Press the ENT Key to acknowledge the startup screen. 16) Turn the large FMS Knob to select the AUX Page group on the MFD. INDEX 17) Turn the small FMS Knob to select the System Status Page. 550 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix B SYSTEM OVERVIEW 18) Press the Display Database Selection Softkey to show standby navigation database information for each display (MFD1 DB, PFD1 DB). Verify the correct standby navigation database cycle information is shown for each display. Figure B-15 shows the navigation database information for the MFD. FLIGHT INSTRUMENTS NOTE: After the navigation database is loaded or copied, the top SD card may be removed. EIS AUDIO PANEL & CNS FLIGHT MANAGEMENT Figure B-15 MFD Navigation Database Information HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 551 INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Appendix B Blank Page 552 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix C SYSTEM OVERVIEW Glossary APPENDICES INDEX Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T ADDITIONAL FEATURES 190-00820-06 Rev. A barometric altitude AFCS B ALT HAZARD AVOIDANCE ATK AUTOSEQ AUX AWOS FLIGHT MANAGEMENT ATC ATCRBS ATIS barometric setting battery backcourse 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 AUDIO PANEL & CNS AIM AIRMET ALRT ALT ALT, ALTN AMPS ANNUNC ANT AOPA AP AP DISC APR APT ARINC ARSPC ARTCC ARV AS ASB ASOS BARO BATT BC Bearing EIS AF AFCS AFM AFMS AFRM AGL AHRS accuracy active, activate air data computer Automatic Direction Finder Attitude Direction Indicator Automatic Descent Mode Automatic Dependent Surveillance Broadcast Arc to fix Automatic Flight Control System Airplane Flight Manual Airplane Flight Manual Supplement airframe Above Ground Level Attitude and Heading Reference System Aeronautical Information Manual Airman’s Meteorological Information alert altitude alternator amperes annunciation antenna Aircraft Owners & Pilots Association 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 AACC ACT, ACTV ADC ADF ADI ADM ADS-B 553 SYSTEM OVERVIEW Appendix C FLIGHT INSTRUMENTS CRSR CTA CTRL Cumulative CVR CVRG CWS CYL cursor Control Area control 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 APPENDICES 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 E ECU Efficiency INDEX EGNOS EGT EIS 554 empty, east Engine Control Unit A measure of fuel consumption, expressed in distance per unit of fuel. European Geostationary Navigation Overlay Service Exhaust Gas Temperature Engine Indication System ELEV ELEV EMERGCY EMI ENDUR Endurance elevation elevator emergency Electromagnetic Interference 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 ES Extended Squitter ESP Electronic Stability and Protection 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 EVS Enhanced Vision System EXPIRD expired ºF FA FAA FADEC FAF FAIL FC FCC FCST FD FD FDE FFLOW 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 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix C INDEX Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T APPENDICES 190-00820-06 Rev. A ADDITIONAL FEATURES Ground Track GRS AFCS Groundspeed HAZARD AVOIDANCE GMA GMT GMU GND gph GPS Grid MORA 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 Hold Terminating at Altitude heading The direction an aircraft is pointed, based upon indications from a magnetic compass or a properly set directional gyro. HF Hold Terminating at Fix HFOM Horizontal Figure of Merit Hg mercury HI high HI SENS High Sensitivity HM Hold with Manual Termination Horizontal Figure of Merit A measure of the uncertainty in the aircraft’s horizontal position. hPa hectopascal HPL Horizontal Protection Level hr hour HSDB High-Speed Data Bus HSI Horizontal Situation Indicator HT heat HUL Horizontal Uncertainty Level Hz Hertz I Inner Marker IAF Initial Approach Fix IAT Indicated Air Temperature ICAO International Civil Aviation Organization ICS Intercom System ID Identification/Morse Code Identifier IDENT, IDNT identification IF Initial Fix IFR Instrument Flight Rules IG Imperial gallon ILS Instrument Landing System IMC Instrument Meteorological Conditions in inch INACTV inactive INC FUEL increase fuel IND indicated Indicated Information provided by properly calibrated and set instrumentation on the aircraft panel. INFO information in HG inches of mercury INT intersection(s) FLIGHT MANAGEMENT G/S, GS GA gal, gl GBOX GDC GDL GDU GEA GEO GFC GIA GLS HA HDG Heading AUDIO PANEL & CNS Fuel On Board Ground speed Garmin Traffic System Garmin Transponder EIS FMS FOB FPL fpm FREQ FRZ FSS ft Fuel Flow GS GTS GTX FLIGHT INSTRUMENTS FISDL FL FLC FM Flight Information ServicesBroadcast Flight Information Service Data Link flight level Flight Level Change Course From Fix to Manual Termination 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 FIS-B 555 FLIGHT INSTRUMENTS SYSTEM OVERVIEW Appendix C INTEG IrDA, IRDA integrity (RAIM unavailable) Infrared Data Association KEYSTK kg kHz km kt key stuck kilogram kilohertz kilometer knot ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS 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 INDEX APPENDICES M m MAG MAG VAR MAHP MAN IN MAN SQ MAP MASQ MAX 556 Middle Marker meter Magnetic Magnetic Variation Missed Approach Hold Point manifold pressure (inches Hg) Manual Squelch Missed Approach Point Master Avionics Squelch maximum MAXSPD MDA maximum speed (overspeed) barometric minimum descent altitude MET manual electric trim METAR Meteorological Aviation Routine MEPT manual electric pitch trim MFD Multi Function Display MGRS Military Grid Reference System MHz megahertz MIC microphone MIN minimum Minimum Safe Altitude Uses Grid MORAs to determine a safe altitude within ten miles of the aircraft present position. MKR marker beacon MOA Military Operations Area MOV movement mpm meters per minute MSA Minimum Safe Altitude MSAS Multi-functional Satellite Augmentation System MSG message 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 pressure altitude Passenger Address Proximity Advisory passenger(s) personal computer Primary Flight Display Procedure Turn to Course Intercept pitch nearest Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix C RAM REF REM REQ RES SCIT 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX SD sec SEL, SLCT south Selective Availability Static Air Temperature Satellite-Based Augmentation System Storm Cell Identification and Tracking Secure Digital second(s) select TCA TCAS TEL TEMP TERM TF TFR T HDG TIS TIT TKE TMA TMR/REF Topo APPENDICES S SA SAT SBAS TAT TAWS true Traffic Advisory Tactical Air Navigation System Terminal Aerodrome Forecast Traffic Advisory System, true airspeed 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 ADDITIONAL FEATURES RT RVRSNRY RX T TA TACAN TAF TAS AFCS REV RF RMI RMT RNG RNWY ROL ROM rpm RST FUEL RSV HAZARD AVOIDANCE right, right runway radial Receiver Autonomous Integrity Monitoring random access memory reference remaining (fuel remaining above Reserve) 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 Sim SLP/SKD SMBL SPD SPI SPKR SQ SRVC, SVC STAL STAR STATS STBY STD SUA SUSP SVS SW SYS AUDIO PANEL & CNS quantity SID SIGMET surface Standard Instrument Approach Procedures Standard Instrument Departure Significant Meteorological Information simulator slip/skid symbol speed Special Position Identification speaker squelch service stall Standard Terminal Arrival Route statistics standby standard Special Use Airspace suspend Synthetic Vision System software system EIS QTY SFC SIAP FLIGHT INSTRUMENTS position parts per million Present Position pressure procedure(s), procedure turn pounds per square inch Procedure Turn parallel track Push-to-Talk power SYSTEM OVERVIEW POSN PPM P. POS PRES, PRESS PROC psi PT PTK PTT PWR 557 SYSTEM OVERVIEW Appendix C Track FLIGHT INSTRUMENTS Track Angle Error EIS TRG TRK TRSA TRUNC TTL TURN TX AUDIO PANEL & CNS UNAVAIL USR UTC UTM/UPS 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 total procedure turn transmit VR VS VSI VSR VTF 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 unavailable user Coordinated Universal Time Universal Transverse Mercator / Universal Polar Stereographic Grid XFER, XFR XPDR XTALK XTK transfer transponder cross-talk cross-track INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT 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 Heading Vector to Manual Termination VMC Visual Meteorological Conditions VNAV, VNV vertical navigation VOL volume VOR VHF Omni-directional Range VORTAC very high frequency omnidirectional range station and tactical air navigation VPL Vertical Protection Level VPROF VNV profile, vertical profile VPTH VNV path, vertical path 558 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix D SYSTEM OVERVIEW Frequently Asked Questions FLIGHT INSTRUMENTS If a particular aspect of the Perspective™ system operational capability is not addressed by these commonly asked questions or in the index, contact Garmin (see the copyright page or back cover for contact information) or a Garmin-authorized dealer. Garmin is dedicated to supporting its products and customers. What is SBAS? EIS The Satellite Based Augmentation System (SBAS) uses a system of ground stations to correct any GPS signal errors. These ground stations correct for errors caused by ionospheric disturbances, timing, and satellite orbit errors. It also provides vital integrity information regarding the health of each GPS satellite. The signal correction is then broadcast through geostationary satellites. This correction information can then be received by any SBAS-enabled GPS receiver. AUDIO PANEL & CNS SBAS is designed to provide the additional accuracy, availability, and integrity necessary to enable users to rely on GPS for all phases of flight. FLIGHT MANAGEMENT There are several SBAS systems serving different parts of the world. The Wide Area Augmentation System (WAAS) is currently available in the United States, including Alaska and Hawaii. The European Geostationary Navigation Overlay Service (EGNOS) offers coverage of Europe, parts of the middle east and northern Africa. The Multi-functional Satellite Augmentation System (MSAS) covers mainly Japan and parts of northern Australia. How does SBAS affect approach operations? HAZARD AVOIDANCE Both LNAV/VNAV and LPV approaches use the accuracy of SBAS to include vertical (glide path) guidance capability. The additional accuracy and vertical guidance capability allows improved instrument approaches to an expanded number of airports throughout the U.S. AFCS The implementation of LPV approaches further improves precision approach capabilities. LPV approaches are designed to make full use of the improved GPS signal from the SBAS. This approach combines the LNAV/ VNAV vertical accuracy with lateral guidance similar to the typical Instrument Landing System (ILS). LPV approaches allow lower approach minimums. What is RAIM and how does it affect approach operations? ADDITIONAL FEATURES RAIM is an acronym for Receiver Autonomous Integrity Monitoring. RAIM is a GPS receiver function that performs the following functions: • Monitors and verifies integrity and geometry of tracked GPS satellites • Notifies the pilot when satellite conditions do not provide the necessary coverage to support a certain phase of flight APPENDICES • Predicts satellite coverage of a destination area to determine whether the number of available satellites is sufficient to satisfy requirements NOTE: If RAIM is not predicted to be available for the final approach course, the approach does not become 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX active, as indicated by the “RAIM not available from FAF to MAP” message and the LOI annunciation flagging on the HSI. 559 SYSTEM OVERVIEW Appendix D For RAIM to work correctly, the GPS receiver must track at least five satellites. A minimum of six satellites is required to allow RAIM to eliminate a single corrupt satellite from the navigation solution. FLIGHT INSTRUMENTS RAIM ensures that satellite geometry allows for a navigation solution calculation within a specified protection limit (2.0 nm for oceanic and en route, 1.0 nm for terminal, and 0.3 nm for non-precision approaches). The system monitors RAIM and issues an alert message when RAIM is not available (see Appendix A). Without RAIM, GPS position accuracy cannot be monitored. If RAIM is not available when crossing the FAF, the pilot must fly the missed approach procedure. Why might there be no approaches available for a flight plan? EIS Approaches are available for the final destination airport in a flight plan or as a direct-to (keep in mind that some VOR/VORTAC identifiers are similar to airport identifiers). If a destination airport does not have a published approach, the system indicates “NONE” for the available procedures. AUDIO PANEL & CNS What happens when an approach is selected? Can a flight plan with an approach, a departure, or an arrival be stored? FLIGHT MANAGEMENT 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. HAZARD AVOIDANCE Flight plans can also be stored with an approach, a departure, or an arrival. Note that the active flight plan is erased when the system is turned off. Also, the active flight plan is overwritten when another flight plan is activated. When storing flight plans with an approach, a departure, or an arrival, the system uses the waypoint information from the current database to define the waypoints. If the database is changed or updated, the Perspective™ 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. AFCS Can “slant Golf” (“/G”) be filed using the Perspective™ system? ADDITIONAL FEATURES “/G” may be filed for a flight plan. GPS approaches are not to be flown with an expired database. See the approved Pilot's Operating Handbook (POH) as well as the Aeronautical Information Manual (AIM) for more information. What does the OBS Softkey do? INDEX APPENDICES The OBS Softkey is used to select manual sequencing of waypoints. Activating OBS mode sets the current active-to waypoint as the primary navigation reference and prevents the system from sequencing to the next waypoint in a flight plan. When OBS mode is cancelled, automatic waypoint sequencing is continued, and the system automatically activates the next waypoint in the flight plan once the aircraft has crossed the present active waypoint. 560 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix D • 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 FLIGHT INSTRUMENTS OBS • Manual sequencing - ‘holds’ on selected waypoint SYSTEM OVERVIEW Normal (OBS not activated) • Automatic sequencing of waypoints EIS AUDIO PANEL & CNS When OBS mode is active, the system allows the pilot to set a desired course to/from a waypoint using the CRS/ BARO Knob and HSI (much like a VOR). The most common application for using the OBS Softkey is the missed approach. The system suspends automatic waypoint sequencing (indicated by a ‘SUSP’ annunciation placed on the HSI) when the missed approach point (MAP) is crossed. This prevents the system from automatically sequencing to the missed approach holding point (MAHP). During this time, the OBS Softkey designation changes to SUSP. Selecting the SUSP Softkey reactivates automatic waypoint sequencing. The OBS Softkey then resumes its normal functionality. FLIGHT MANAGEMENT Why might the Perspective™ System not automatically sequence to the next waypoint? HAZARD AVOIDANCE The system 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? AFCS The system allows the pilot to manually select any approach, departure, or arrival leg as the active leg of the flight plan. This procedure is performed on the MFD from the Active Flight Plan Page by highlighting the desired waypoint and selecting the ACT LEG Softkey then the ENT Key to approve the selection. The GPS then provides navigation along the selected flight plan leg. ADDITIONAL FEATURES When does turn anticipation begin? The system smooths adjacent leg transitions based on a normal 15° bank angle (with the ability to roll up to 30°) and provides three pilot cues for turn anticipation: APPENDICES • A waypoint alert (‘Next DTK ###° in # seconds’ or ‘Next HDG ###° in # seconds’) appears on the PFD 10 seconds before the turn point and flashes as it counts down to zero. • A flashing turn advisory (‘Turn [right/left] to ###° in # seconds’) appears on the PFD 10 seconds before the turn and flashes as it counts down to zero. ‘Turn [right/left] to ###° now’ or ‘Next [DTK/HDG] to ###° now’ is displayed when the pilot is to begin the turn and the HSI (GPS mode) automatically sequences to the next DTK or HDG value. 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T INDEX • The To/From indicator on the HSI flips momentarily to indicate that the midpoint of the turn has been crossed. 561 SYSTEM OVERVIEW Appendix D When does the CDI scale change? FLIGHT INSTRUMENTS Once a departure is activated, the Perspective™ Course Deviation Indicator (CDI) full scale deflection is set to 0.3 nm. The CDI scale changes to 1.0 nm (terminal mode) then ramps up to 2.0 nm (enroute mode) at 30 nm from the departure airport. When 31 nm from the destination, the CDI scale smoothly transition from 2.0 nm back to 1.0 nm (terminal mode). At 2.0 nm before the FAF during an active approach, the CDI scale transitions down further based on the type of approach activated (LNAV, LNAV/VNAV, LPV). When a missed approach is activated, the CDI is set to 0.3 nm. See the Flight Instruments Section for more details on CDI scaling. Why does the HSI not respond like a VOR when OBS mode is active? AUDIO PANEL & CNS EIS 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? FLIGHT MANAGEMENT To comply with TSO specifications, the Perspective™ 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. 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. HAZARD AVOIDANCE 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 AFCS (MAP). If an attempt to do so is made, an alert message “Are you sure you want to discontinue the current approach?” appears. The system directs the pilot back to the transition waypoint and does not take into consideration any missed approach procedures, if the current approach is reactivated. ADDITIONAL FEATURES 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 Perspective™ provides navigation along the desired course to the waypoint and rejoins the approach in sequence from that point. APPENDICES 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 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. 562 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix E 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 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 563 SYSTEM OVERVIEW Appendix E Hazard Avoidance Features FLIGHT INSTRUMENTS Feature Symbol Item Terrain Proximity/TAWS-B display enabled Non-threat Traffic Traffic display enabled Proximity Advisory NEXRAD display enabled Traffic Advisory, Beyond Map Range Cloud Top display enabled EIS Traffic Symbol Traffic Advisory AUDIO PANEL & CNS XM Lightning display enabled FLIGHT MANAGEMENT Echo Top display enabled SIGMETs/AIRMETs display enabled Miscellaneous Item Cell Movement display enabled METARs display enabled HAZARD AVOIDANCE City Forecast display enabled Surface Analysis display enabled ADDITIONAL FEATURES AFCS Freezing Levels display enabled Symbol ARTCC Frequency or FSS Frequency Map Pointer (when panning) Elevation Pointer (on Topography Scale when panning) Measuring Pointer Wind Vector 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 564 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Appendix E SYSTEM OVERVIEW Obstacle Database Unlighted Obstacle Lighted Obstacle < 1000’ AGL > 1000’ AGL < 1000’ AGL > 1000’ AGL Obstacle Location FLIGHT INSTRUMENTS 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 EIS Gray obstacle is more than 1000 ft below aircraft altitude AUDIO PANEL & CNS Table E-1 Obstacle Colors Terrain Avoidance Colors and Symbols FLIGHT MANAGEMENT Terrain Above Aircraft Altitude Aircraft Altitude 100 ft Threshold Red terrain is above or within 100 ft below the aircraft altitude HAZARD AVOIDANCE 1000 ft Yellow terrain is between 100 ft and 1000 ft below the aircraft altitude Black terrain is more than 1000 ft below the aircraft altitude AFCS Figure E-1 Terrain Altitude/Color Correlation ADDITIONAL FEATURES Figure E-2 TAWS-B Potential Impact Points APPENDICES INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 565 INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Appendix E Blank Page 566 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Index EIS AUDIO PANEL & CNS B Backlighting-------------------------------------------------- 48 Barometric altimeter setting---------------------------50, 56 Bearing/distance, measuring------------------------------150 Bearing information--------------------------- 51, 62–63, 63 Bearing source----------------------------------------------- 63 FLIGHT MANAGEMENT C Calibrated Airspeed-----------------------------------------250 CDI---------------------------------- 245, 257, 268, 276, 283 CELL MOV Softkey------------------------------------------303 Chart Not Available---------------------------------- 458, 478 Chart options----------------------------------------- 466, 485 Chart setup box-------------------------------------- 472, 488 ChartView--------------------------------------- 433, 457, 475 ChartView database----------------------------------------475 ChartView functions----------------------------------------457 ChartView plan view---------------------------------------467 ChartView profile view-------------------------------------468 ChartView softkeys-----------------------------------------457 Checklists--------------------------------------------- 502–503 Checklist softkeys-------------------------------------------502 CLD TOP Softkey--------------------------------------------301 Closest Point-------------------------------------------------232 COM channel spacing--------------------------------------113 COM Frequency Box----------------------------------------106 Command Bars----------------------------------------------388 Communication (COM) Frequency Window------------- 50 Comparator Window----------------------------51, 414, 516 COM tuning failure-----------------------------------------137 Controls Softkeys------------------------------------------------ 14–17 Copy a Flight Plan------------------------------------------218 Course Deviation Indicator (CDI)-----------------50, 64–65 Changing scale-------------------------------------------562 Course To Altitude------------------------------------------249 Cylinder Head Temperature (CHT °F)--------------------- 82 AFCS ADDITIONAL FEATURES APPENDICES INDEX Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T HAZARD AVOIDANCE 190-00820-06 Rev. A Automatic Descent Mode---------------------------------535 Automatic Flight Control System (AFCS)--------- 383–432 Alerts and annunciations------------------------ 429–430 Status Annunciations------------------------------------429 Status Box-------------------------------------------------387 Automatic squelch------------------------------------------114 Autopilot-----------------------------------------------------383 Autopilot Disconnect-------------------------------- 385, 413 Auto-tuning, COM------------------------------------------109 Auto-tuning, NAV------------------------------------ 117, 121 Auto Zoom---------------------------------------------------144 Auxiliary Pages (AUX)--------------------------------------- 37 AUX - system status page-454, 456, 475, 476, 490, 492, 494 Aviation Symbols------------------------------------- 155, 198 Avidyne TAS600---------------------------------------------368 FLIGHT INSTRUMENTS Activate a Flight Plan---------------------------------------218 Active channel-----------------------------------------------497 Active database-------------------------------------- 543, 547 Active frequency------------------------------------- 106, 115 ADS-B---------------------------------------------------------354 AFCS Status Annunciation---------------------------------- 51 AFCS Status Box--------------------------------------- 50, 387 AHRS--------------------------------------------- 530, 531, 532 Air Data Computer-------------------------------------------- 1 Airport Information-----------------------------------------------176 Airspace Alerts--------------------------------- 191, 192, 285 Airspeed Indicator---------------------------------------50, 52 Airways Collapsed--------------------------------------------------232 Expanded--------------------------------------------------232 Alerting system----------------------------------------------515 Alert levels---------------------------------------------------517 Alerts---------------------------------------------------------515 Aircraft-----------------------------------------------------518 Audio voice-----------------------------------------------521 Along Track Offset----------------------------------- 223, 224 ALT------------------------------------------------------------281 Altimeter--------------------------------------------------50, 55 Altitude Constraints----------------------------------------- 235, 268 Altitude alerting---------------------------------------------- 77 Altitude Hold Mode----------------------------------------392 Altitude Reference----------------------------- 391, 392, 399 Annunciations AFCS Status-----------------------------------------------535 Test tone---------------------------------------------- 27, 516 Annunciator lights------------------------------------------130 AOPA airport directory------------------------ 433, 493, 494 AOPA Airport Directory-------------------------------------542 Approach-----------------------------------------------------560 Activating-------------------------------------------------248 ILS----------------------------------------------------------424 Loading--------------------------------------- 215, 245, 247 Missed-----------------------------------------------------427 Removing--------------------------------------------------248 WAAS------------------------------------------------------426 Approach box-----------------------------------------------480 Approach Mode-------------------------------- 409, 424, 426 APR softkey------------------------------------------- 247, 252 Arc HSI--------------------------------------------------------- 60 Arrival procedure------198, 213, 242, 244, 266, 268, 277 Assist, engine leaning---------------------------------- 94–96 Attitude---------------------------------------------------------- 1 Attitude Indicator----------------------------------------50, 54 Audio alerting system------------------------------- 516, 517 Audio panel fail-safe operation---------------------------137 Automatic Dependent Surveillance - Broadcast--------354 SYSTEM OVERVIEW A I-1 AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Index D F Databases----------------------------------------------- 23, 541 Database synchronization--------------- 27, 543, 544, 546 Data link-------------------------------------------------------- 1 Datalink receiver troubleshooting------------------------513 Data Logging----------------------------------------- 433, 505 Date and time------------------------------------------------ 40 Day/Night views-------------------------------------- 472, 488 Day view----------------------------------472, 473, 488, 489 Dead Reckoning---------------------------------------------- 79 Declutter, display--------------------------------------------- 80 Declutter maps-------------------------------------------15, 20 Delete Flight Plans------------------------------------------219 Deleting An entire airway----------------------------------- 220, 221 An entire procedure------------------------------ 220, 221 An individual waypoint--------------------------- 220, 221 Flight Plan Items-----------------------------------------220 Density Altitude---------------------------------------------252 Departure Procedure------------------------------211, 227, 239, 241 Select------------------------------------239, 242, 245, 248 Time--------------------------------------------------------250 Timer-------------------------------------------------------- 47 Digital audio entertainment---------------------------------- 4 Dilution of Precision (DOP)--------------------------------- 30 Direct-to-- 169, 193, 194, 195, 196, 197, 233, 234, 266, 268, 283 Display backup----------------------------------------------- 25 DME HOLD mode-----------------------------------------------123 NAV1 mode-----------------------------------------------123 DME information-----------------------------------------51, 63 DME transceiver pairing-----------------------------------123 DME tuning window---------------------------------------123 DR mode------------------------------------------------------ 79 Fail-safe operation------------------------------------------137 Field of View (SVS)------------------------------------------166 Flight director (FD)------------------------------------------383 Modes, vertical------------------------------------ 389–403 Flight ID------------------------------------------------------124 Flight Level Change Mode-------------------- 394, 420, 422 Flight plan Closest point to reference------------------------------232 Storing-----------------------------------------------------560 Flight timer---------------------------------------------------- 46 FliteCharts-------------------------------------------- 433, 477 FliteCharts®-------------------------------------------------433 FliteCharts cycle---------------------------------------------490 FliteCharts database---------------------------------------491 FliteCharts expiration--------------------------------------491 FliteCharts functions---------------------------------------477 FPA----------------------------------------------------- 235, 273 Frequency Nearest----------------------------------------------------189 Frequency spacing------------------------------------------113 Frequently asked questions--------------------------------559 Fuel Calculations------------------------------------------------ 89 Efficiency--------------------------------------------------252 Endurance-------------------------------------------------252 Flow--------------------------------------------------------- 86 Remaining-------------------------------------------------252 Required---------------------------------------------------252 Statistics---------------------------------------------------251 Fuel calculations--------------------------------------------- 96 Fuel Flow (FFLOW GPH)------------------------------------ 82 Fuel on Board-----------------------------------------------252 ADDITIONAL FEATURES E INDEX APPENDICES ECHO TOP Softkey------------------------------------------300 Electronic checklists---------------------433, 502, 503, 504 Electronic Stability and Protection------------54, 433, 509 Emergency checklist----------------------------------------503 Emergency Frequency--------------------------------------137 Engine Indication System (EIS)------------------------ 81–98 Entering Flight ID-------------------------------------------124 Entertainment inputs---------------------------------------134 ESP------------------------------------------ 54, 509, 510, 511 ESP™-------------------------------------------- 433, 509, 512 Estimated Position Error (EPE)----------------------------- 30 Ethernet------------------------------------------------------- 24 Exhaust Gas Temperature (EGT)---------------------- 94–95 I-2 G GDC 74A-------------------------------------------------------- 1 GDL 69/69A----------------------------------------------1, 287 GDU 1040------------------------------------------------------ 1 GEA 71---------------------------------------------------------- 1 GFC 700------------------------------------------------------383 GIA 63W-------------------------------------------------------- 1 Glidepath-----------------------------------------------------281 Glidepath indicator------------------------------------------ 58 Glidepath Mode (GP)-------------------------- 400, 409, 426 Glideslope----------------------------------------------------281 Glideslope indicator----------------------------------------- 58 Glideslope Mode------------------------------------- 402, 424 Global Positioning System (GPS) Navigation----------------------------------------- 193–286 GMA 347-------------------------------------------------- 1, 23 GMU 44--------------------------------------------------------- 1 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Index Jeppesen aviation database-------------------------------542 Key(s)--------------------------------------------------------- 8, 9 M Mach number------------------------------------------------ 50 Magnetometer------------------------------------------------- 1 Map Panning----------------------------------------------------146 O APPENDICES Land Symbols------------------------------------------------154 LNAV----------------------------------------------------------257 LO SENS------------------------------------------------------122 Low Altitude Annunciation--------------------------------- 77 LPV----------------------------------------------- 257, 283, 415 ADDITIONAL FEATURES L AFCS K National Weather Service----------------------------------311 Navigation Database------------------------------------------- 235, 236 Map--------------------------------------------------------195 Navigation Mode----------------------- 407–408, 418–419 Navigation mode selection--------------------------------115 Navigation (NAV) Frequency Window-------------------- 50 Navigation source-------------------------------------- 64–66 Navigation Status Box-------------------------------------- 50 Nav radio selection-----------------------------------------115 Nearest Airport-------------- 173, 174, 175, 176, 189–192, 247 Airport Minimum Runway Length---------------------176 Airports Page-------------------------------- 174, 175, 176 Airport Surface Matching-------------------------------176 VOR------------------------------------------------- 189–190 Nearest airports, frequency tuning-----------------------109 Nearest Pages (NRST)--------------------------------------- 37 NEXRAD Softkey--------------------------------------------296 Night view--------------------------------472, 473, 488, 489 Non-path descent------------------------------398, 422–423 Normal display operation----------------------------------- 24 HAZARD AVOIDANCE J N FLIGHT MANAGEMENT IDENT function--------------------------------------- 126, 130 ID indicator--------------------------------------------------117 ILS approach-------------------------------------------------424 Indicated airspeed------------------------------------------- 52 Indicated Altitude-------------------------------------------250 INFO box-----------------------------------------------------481 Initialization (system)---------------------------------------- 23 Inset Map----------------------------------------------------- 51 Intercom system (ICS)--------------------------------------134 Intersection Information---------------------------------------- 177–178 Inverting a flight plan--------------------------------------218 IOI----------------------------------- 335, 345, 536, 537, 538 AUDIO PANEL & CNS I EIS Heading------------------------------------------------------- 50 Heading Select Mode--------------------------------------406 HI SENS-------------------------------------------------------122 Horizontal Situation Indicator (HSI)--------------50, 59–70 HSI double green arrow------------------------------------115 HSI magenta arrow-----------------------------------------115 HSI single green arrow-------------------------------------115 Hypoxia------------------------------------------ 433, 507, 508 Map pages---------------------------------------------------- 36 Map symbols------------------------------------------------563 Marker beacon----------------------------------------------122 Marker beacon annunciations----------------------------- 75 MASQ processing-------------------------------------------- 99 Measurement units, changing displayed----------------- 41 Menus--------------------------------------------------------- 34 Message advisories--------------- 517, 525, 530, 531, 532 Messages window------------------------------------------501 Minimum Descent Altitude (MDA)--------------------51, 78 MISCOMP----------------------------------------------------520 Missed Approach----------- 198, 249, 254, 257, 283, 427 MKR/MUTE--------------------------------------------------122 Mode S------------------------------------------------ 124, 125 Mode selection softkeys---------------------------- 124, 125 Morse code identifier---------------------------------------117 Multi Function Display (MFD) Softkeys----------------------------------------------------- 19 FLIGHT INSTRUMENTS H SYSTEM OVERVIEW Go Around Mode------------------------------------ 427–428 GRS 77---------------------------------------------------------- 1 GTS 800------------------------------------------------------532 GTX 33---------------------------------------------------------- 1 GTX 33 Mode S Transponders----------------------------124 OBS Mode----------------------------------------------- 69–70 Obstacles---------------------------------------------- 527, 528 Oil Pressure (OIL PSI)------------------------------------82, 86 Oil Temperature (OIL °F)------------------------------------ 82 Omni Bearing Selector (OBS)----------------------- 560–561 Other Statistics--------------------------------------- 250, 252 INDEX 190-00820-06 Rev. A Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T I-3 SYSTEM OVERVIEW Index P AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS Page groups--------------------------------------------- 35–38 Page menus--------------------------------------------------- 34 Parallel Track------------------------------------------ 225, 227 Passenger address------------------------------------------132 PA system----------------------------------------------------132 Pilot profiles--------------------------------------------- 42–43 PIT-------------------------------------------------------------520 Pitch Hold Mode--------------------------------------------390 Pitch indication----------------------------------------------- 54 Power-up page----------------------------------------------502 Primary Flight Display (PFD) Softkeys------------------------------------------------ 14–16 Procedures GFC 700-------------------------------------------- 415–432 Q Quick tuning 121.500 MHz-------------------------------108 R AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT RAIM---------------------------------------244, 254, 255, 256 Ram Air Temperature (RAT)--------------------------------- 71 Range---------------------------------------------------------164 Receiver Autonomous Integrity Monitoring (RAIM)-31–32, 254, 559 Required Vertical Speed--------------------------------------------274 Vertical Speed Indicator---------------------------------274 Reversionary Mode---------------------------------25–26, 28 Reversionary Sensor Window---------------------- 414, 517 ROC--------------------------------- 335, 345, 536, 537, 538 Roll Hold Mode---------------------------------------------405 RS-232----------------------------------------------------------- 4 RS-485----------------------------------------------------------- 3 RVSI---------------------------------------------------- 274, 275 RX indicator--------------------------------------------------107 ADDITIONAL FEATURES S INDEX APPENDICES SafeTaxi------------------------------------------ 433, 451, 454 SafeTaxi®----------------------------------------------------433 SafeTaxi database-------------------------------------------455 SBAS--------------------------------------------- 254, 256, 559 Scheduler----------------------------------------433–434, 500 Secure Digital (SD) card----------------------------- 502, 541 Selected Altitude-- 50, 77, 390, 391, 393, 394, 395, 399 Selected Altitude Capture Mode-390, 391, 392, 393, 395, 403 Selected Altitude Intercept Arc----------------------------167 Selected Altitude Range Arc----------------------------10, 55 Selected Course----------------------------- 51, 60, 408, 410 Selected Heading--------------------------------- 51, 60, 406 I-4 Selecting a COM radio-------------------------------------106 Sensor--------------------------------------------------------520 Sequencing, automatic-------------------------------------561 Skywatch-----------------------------------------------------375 Slip/Skid Indicator----------------------------------------50, 54 Softkeys LTNG-------------------------------------------------------302 MFD--------------------------------------------------------- 19 PFD-------------------------------------------------14–16, 50 Sort Flight Plans---------------------------------------------218 Speaker-------------------------------------------------------130 Split COM operation----------------------------------------133 Standby database-------------------------------------------543 Standby frequency----------------------------- 106, 109, 115 Standby frequency field------------------------------------106 Stereo headsets---------------------------------------------130 Stormscope--------------------------------------------------317 Stuck microphone-------------------------------------------137 Sunrise--------------------------------------------------------251 Sunset--------------------------------------------------------251 SVS------------------------------------------------------------- 54 SVS troubleshooting----------------------------------------512 Symbols, map------------------------------------------------563 Synthetic vision (SVS)------------------------------- 433, 434 Synthetic Vision System------------------------------------- 54 System annunciations--------------------------------------515 System Page (EIS)-------------------------------------------- 96 System time--------------------------------------------------- 50 T Tachometer (RPM)---------------------------------------82, 86 TAF------------------------------------------------------------305 Takeoff Mode------------------------------------------------403 TAS------------------------------------------------------------530 TAWS-------------------------------------------------- 351, 537 Terminal procedures charts------------------------- 458, 478 Terrain--------------------------------------------------------527 Color indications-----------------------------------------565 Terrain Awareness and Warning System (TAWS)-------537 Annunciation---------------------------------------------- 76 Terrain Proximity--------------------------------------------323 Terrain-SVS--------------------------------328, 383, 432, 509 Timer Departure--------------------------------------------------- 47 Flight-------------------------------------------------------- 46 Timer, PFD generic------------------------------------------- 45 TOD---------------------------------------------- 273, 274, 280 TOPO DATA------------------------------------- 151, 152, 161 Top of Descent--------------------------------------- 273, 274 TOPO SCALE-------------------------------------------------153 Track----------------------------------------------------------- 59 Track Vector--------------------------------------------------162 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A Index XM Radio------------------------------------------------ 287, 495 Receiver troubleshooting-------------------------------513 XM Satellite Weather------------------------------------287 XM channel list----------------------------------------------497 XM radio-----------------------------------------------------497 XM radio entertainment-----------------------------------134 XM radio presets--------------------------------------------499 XM radio volume--------------------------------------------499 XM satellite radio------------------------------------ 495, 497 XM Service class--------------------------------------------496 XM weather/radio--------------------------------------------- 4 HAZARD AVOIDANCE Z AFCS Zoom Auto--------------------------------------------------------144 APPENDICES INDEX Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T ADDITIONAL FEATURES 190-00820-06 Rev. A X FLIGHT MANAGEMENT VDI----------------------------------------------------- 274, 275 Vertical deviation-------------------------------------------397 Vertical deviation guidance-------------------------------236 Vertical Deviation Indicator-------------------------------274 Vertical Deviation Indicator (VDI)----------------------51, 58 Vertical navigation------------------------------------------235 Direct-to---------------------------------------------------234 Vertical Navigation flight control------------------ 395–399 Vertical Path Tracking Mode------------------395–396, 421 Vertical speed guidance-----------------------------------236 Vertical Speed Indicator (VSI)--------------------------50, 58 Vertical Speed Mode---------------------------------------393 Vertical Speed Reference----------------------------------393 VFR code-----------------------------------------------------129 VNAV---------------------------------------------------------197 VNAV Target Altitude-------------------------------- 395–398 VNAV Target Altitude Capture Mode--------------------399 VNV----------------------------------------273, 533, 534, 558 VNV guidance Disabling--------------------------------------------------233 Enabling---------------------------------------------------233 VNV indications, PFD---------------------------------------- 74 VNV Target Altitude----------------------------------------- 51 Voice alerts, TIS Traffic--------------------------------------381 VOR WAAS-------------------------------------------- 257, 415, 559 WAAS precision approach---------------------------------426 Waypoint Automatic sequencing----------------------------------561 Skipping---------------------------------------------------561 Waypoint Pages (WPT)-------------------------------------- 36 Waypoint Selection Submenu--- 194, 201, 205, 206, 255 Weather (real-time)-------------------------------------------- 4 Wind--------------------------------------------------- 142, 163 Wind data-------------------------------------------------51, 73 WIND Softkey------------------------------------------------309 AUDIO PANEL & CNS V W EIS Unable to display chart----------------------------- 458, 478 Updating Garmin databases------------------------------455 Updating Jeppesen databases----------------------------475 Nearest--------------------------------------------- 189–190 VOR selection------------------------------------------------115 VSI-------------------------------------------------------------275 Vspeed references------------------------------------------- 53 VS TGT------------------------------------------------- 235, 273 FLIGHT INSTRUMENTS U SYSTEM OVERVIEW Traffic Annunciation------------------------------------------51, 75 Traffic Advisory System-------------------------------------532 Traffic Information Service (TIS) Voice alerts------------------------------------------------- 75 Transponder code entry------------------------------------127 Transponder data box--------------------------------------- 99 Transponder ground mode--------------------------------125 Transponder mode field-------------------------99, 125, 126 Transponder standby mode-------------------------------126 Transponder Status Box------------------------------------- 50 Trend Vector Turn Rate--------------------------------------------------- 62 Trip Planning------------------------------------ 250, 251, 252 Trip statistics-------------------------------------------------251 True Airspeed------------------------------------------- 52, 252 Turn anticipation--------------------------------------------561 Turn Rate Indicator--------------------------------------50, 62 TX indicator--------------------------------------------------107 I-5 INDEX APPENDICES ADDITIONAL FEATURES AFCS HAZARD AVOIDANCE FLIGHT MANAGEMENT AUDIO PANEL & CNS EIS FLIGHT INSTRUMENTS SYSTEM OVERVIEW Index Blank Page I-6 Cirrus Perspective™ by Garmin – Pilot’s Guide for the SR20/SR22/SR22T 190-00820-06 Rev. A ™ Cirrus Perspective by Garmin ® www.garmin.com Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. p:503.391.3411 f:503.364.2138 Garmin (Europe) Ltd. Liberty House, 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 Cirrus SR20/SR22/SR22T Garmin International, Inc. 1200 East 151st Street Olathe, KS 66062, U.S.A. p:913.397.8200 f:913.397.8282 Cirrus SR20/SR22/SR22T Integrated Avionics System Pilot’s Guide
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