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Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin

Cirrus SR22T G7 · Flight Manual

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Overview

This Pilot’s Guide is designed for the Cirrus SR2x series, which includes the SR20, SR22, and SR22T models equipped with the Cirrus Perspective Touch+ avionics system by Garmin. The guide provides comprehensive information on the operation, features, and systems of the aircraft, specifically tailored for pilots and operators. It covers system overviews, flight instruments, engine and airframe systems, audio and communication navigation systems (CNS), flight management, hazard avoidance, and automatic flight control systems. The guide is essential for understanding the functionalities and limitations of the avionics system, ensuring safe and efficient operation of the aircraft.

  • The Cirrus SR22T is equipped with the Cirrus Perspective Touch+ avionics system.
  • Pilots must understand the operation of flight instruments such as the airspeed indicator and altimeter for safe navigation.
  • Engine and airframe system indications are critical for monitoring aircraft performance.
  • Effective communication relies on understanding COM and NAV operations, including frequency tuning.
  • Hazard avoidance features are essential for maintaining situational awareness during flight.

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Originally published by static.garmin.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Flight Manual
Year
2023
Pages
750
File size
49 MB
Publisher
static.garmin.com
How rare is it?
3,198Cirrus SR22T G7 registered worldwide · 2,911 active

Common. One of the most common aircraft types we track.

Documentation completeness
4/7

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In this document

System Overview

This section provides a detailed description of the Cirrus Perspective Touch+ system, including its line replaceable units (LRUs) and operational controls. It outlines the initial power application, normal operation, and reversionary display operation, ensuring pilots understand how to effectively manage the avionics system.

Flight Instruments

The flight instruments section details the various indicators available to the pilot, including airspeed, attitude, altimeter, vertical speed, and course deviation indicators. It emphasizes the importance of understanding these instruments for safe flight operations.

Engine and Airframe Systems

This section discusses the indications related to the engine and airframe systems, including engine performance metrics, fuel management, and electrical systems. It is crucial for pilots to monitor these systems for optimal aircraft performance.

Audio and CNS

The audio and communication navigation systems section explains the operation of the COM and NAV radios, including frequency tuning and transponder controls. This knowledge is vital for effective communication and navigation during flight.

Hazard Avoidance

This section covers the various hazard avoidance features integrated into the avionics system, including terrain awareness and traffic information systems. Pilots are advised on how to utilize these features to enhance situational awareness and safety.

Safety notes

  • Do not operate this equipment without first obtaining qualified instruction.
  • Always refer to current aeronautical charts and NOTAMs for verification of displayed information.
  • Do not rely solely on the display of traffic information for collision avoidance.

Full document text

CIRRUS SR2x System Software Version 3956.Q2 or later CIRRUS PERSPECTIVE TOUCH+ Pilot’s Guide SYSTEM OVERVIEW FLIGHT INSTRUMENTS ENGINE AND AIRFRAME SYSTEMS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AUTOMATIC FLIGHT CONTROL SYSTEM ADDITIONAL FEATURES APPENDICES INDEX 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin Copyright © 2022-2023 Garmin® Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of System Software version 3956.Q2 or later for the Cirrus Perspective Touch+ by Garmin Integrated Avionics System. Where used, references to ‘SR2x’ are inclusive of the SR20, SR22, and SR22T. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. Always refer to the approved current pertinent flight manual for a description of systems, limitations, and procedures. Garmin International, Inc. 1200 East 151st Street Olathe, Kansas 66062, U.S.A. Garmin (Europe) Ltd. Liberty House, Hounsdown Business Park Southampton, Hampshire SO40 9LR U.K. Garmin AT, Inc. 2345 Turner Road SE Salem, OR 97302, U.S.A. Garmin Corporation No. 68, Zhangshu 2nd Road Xizhi District, New Taipei City, Taiwan Contact Garmin Product Support or view warranty information at flygarmin.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, G2000, GDL, FliteCharts, Connext, SafeTaxi, flyGarmin, and flyGarmin.com are registered trademarks of Garmin International, Inc. or its subsidiaries. Autonomí, ChartView, GDU, GEA, GFC 700, GMA, GTX, Garmin ESP, Garmin SVT, Garmin Pilot, Flight Stream, Smart Airspace, SurfaceWatch, and WireAware are trademarks of Garmin International, Inc. or its subsidiaries. These trademarks may not be used without the express permission of Garmin. Perspective is a trademark of Cirrus Design Corporation. Stormscope is a registered trademarks of Extant Aerospace. CO Guardian is a trademark of Guardian Avionics, Inc. AC-U-KWIK is a registered trademark of Penton Business Media Inc. NavData is a registered trademark of Jeppesen, Inc.; Wi-Fi is a registered trademark of the Wi-Fi Alliance. Sirius, XM, and all related marks and logos are trademarks of Sirius XM Radio, Inc. and its subsidiaries. The Bluetooth® word mark and logos are owned by the Bluetooth SIG, Inc. and any use of such marks by Garmin is under license. iOS is a registered trademark of Cisco in the US and is used by Apple under license. Android is a trademark of Google LLC. 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. Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A AC-U-KWIK and its related organizations (hereafter collectively “AC-U-KWIK Organizations”) expressly disclaim all warranties with respect to the AC-U-KWIK information included in this data, express or implied, including, but not limited to, the implied warranties of merchantability and fitness for a particular purpose. The information is provided “as is” and AC-U-KWIK Organizations do not warrant or make any representations regarding its accuracy, reliability, or otherwise. Licensee agrees not to sue AC-U-KWIK Organizations and, to the maximum extent allowed by law, to release and hold harmless AC-U-KWIK Organizations from any cause of action, claims or losses related to any actual or alleged inaccuracies in the information arising out of Garmin’s use of the information in the datasets. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations or exclusions may not apply to licensee. Printed in the U.S.A. 22 PAP 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin i WARNINGS, CAUTIONS, AND NOTES WARNING: Do not operate this equipment without first obtaining qualified instruction. WARNING: Always refer to current aeronautical charts and NOTAMs for verification of displayed aeronautical information. Displayed aeronautical data may not incorporate the latest NOTAM information. WARNING: Do not use geometric altitude for compliance with air traffic control altitude requirements. The

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primary barometric altimeter must be used for compliance with all air traffic control altitude regulations, requirements, instructions, and clearances. WARNING: Do not use basemap information (land and water data) as the sole means of navigation. Basemap data is intended only to supplement other approved navigation data sources and should be considered only an aid to enhance situational awareness. WARNING: Do not rely solely upon the display of traffic information to accurately depict all of the traffic within range of the aircraft. Due to lack of equipment, poor signal reception, and/or inaccurate information from aircraft or ground stations, traffic may be present that is not represented on the display. WARNING: Do not use data link weather information for maneuvering in, near, or around areas of hazardous weather. Information contained within data link weather products may not accurately depict current weather conditions. WARNING: Do not use the indicated data link weather product age to find the age of the weather information shown by the data link weather product. Due to time delays inherent in gathering and processing weather data for data link transmission, the weather information shown by the data link weather product may be older than the indicated weather product age. WARNING: Do not use terrain avoidance displays as the sole source of information for maintaining separation from terrain and obstacles. Garmin obtains terrain and obstacle data from third party sources and cannot independently verify the accuracy of the information. WARNING: Do not rely on the displayed minimum safe altitude (MSAs) as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical charts for appropriate minimum clearance altitudes. 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. Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A ii WARNINGS, CAUTIONS, AND NOTES WARNING: Do not rely on the autopilot to level the aircraft at the MDA/DH when flying an approach with vertical guidance. The autopilot will not level the aircraft at the MDA/DH even if the MDA/DH is set in the altitude preselect. WARNING: Do not rely on the accuracy of attitude and heading indications in the following geographic areas (due to variations in the earth’s magnetic field): North of 72° North latitude at all longitudes; South of 70° South latitude at all longitudes; North of 65° North latitude between longitude 75° W and 120° W. (Northern Canada); North of 70° North latitude between longitude 70° W and 128° W. (Northern Canada); North of 70° North latitude between longitude 85° E and 114° E. (Northern Russia); South of 55° South latitude between longitude 120° E and 165° E. (Region south of Australia and New Zealand). WARNING: Use appropriate primary systems for navigation, and for terrain, obstacle, and traffic avoidance. Garmin SVT™ is intended as an aid to situational awareness only and may not provide either the accuracy or reliability upon which to solely base decisions and/or plan maneuvers to avoid terrain, obstacles, or traffic. WARNING: Do not use the Garmin SVT runway depiction as the sole means for determining the proximity of the aircraft to the runway or for maintaining the proper approach path angle during landing. WARNING: Do not rely on information from a lightning detection system display as the sole basis for hazardous weather avoidance. Range limitations and interference may cause the system to display inaccurate or incomplete information. Refer to documentation from the lightning detection system manufacturer for detailed information about the system. WARNING: Do not use TAWS information for primary terrain or obstacle avoidance. TAWS is intended only to enhance situational awareness. WARNING: Do not rely solely upon the display of traffic information for collision avoidance maneuvering. The traffic display does not provide collision avoidance resolution advisories and does not under any circumstances or conditions relieve the pilot’s responsibility to see and avoid other aircraft. WARNING: Do not use a QFE altimeter setting with this system. System functions will not operate properly with a QFE altimeter setting. Use only a QNH altimeter setting for height above mean sea level, or the standard pressure setting, as applicable. WARNING: Do not use SurfaceWatch™ information as the primary method of flight guidance during airborne or ground operations. SurfaceWatch does not have NOTAM or ATIS information regarding the current active runway, condition, or information about the position of hold lines. 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin iii WARNINGS, CAUTIONS, AND NOTES CAUTION: Do not clean display surfaces with abrasive cloths or cleaners containing ammonia. They will harm the anti-reflective coating. CAUTION: Do not allow repairs to be made by anyone other than an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and affect the airworthiness of the aircraft. CAUTION: Never disconnect power to the system when loading a database. Power interruption during the database loading process could result in maintenance being required to reboot the system. NOTE: All visual depictions contained within this document, including screen images of the system panel and displays, are subject to change and may not reflect the most current system and aviation databases. Depictions of equipment may differ slightly from the actual equipment. NOTE: Do not rely solely upon data link services to provide Temporary Flight Restriction (TFR) information. Always confirm TFR information through official sources such as Flight Service Stations or Air Traffic Control. NOTE: The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the system utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the system can be misused or misinterpreted and, therefore, become unsafe. 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: Use of polarized eyewear may cause the flight displays to appear dim or blank. NOTE: This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with California’s Proposition 65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/prop65. NOTE: Operating the system in the vicinity of metal buildings, metal structures, or electromagnetic fields can cause sensor differences that may result in nuisance miscompare annunciations during start up, shut down, or while taxiing. If one or more of the sensed values are unavailable, the annunciation indicates no comparison is possible. Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A iv WARNINGS, CAUTIONS, AND NOTES NOTE: The system responds to a terminal procedure based on data coded within that procedure in the Navigation Database. Differences in system operation may be observed among similar types of procedures due to differences in the Navigation Database coding specific to each procedure. NOTE: The FAA has asked Garmin to remind pilots who fly with Garmin database-dependent avionics of the following: ƒ It is the pilot’s responsibility to remain familiar with all FAA regulatory and advisory guidance and information related to the use of databases in the National Airspace System. ƒ Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen. Databases obtained from Garmin or Jeppesen that have a Type 2 Letter of Authorization (LOA) from the FAA are assured compliance with all data quality requirements (DQRs). A copy of the Type 2 LOA is available for each applicable database and can be viewed at flygarmin.com by selecting ‘Aviation Database Declarations.’ ƒ Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with established FAA regulatory guidance, but does not constitute authorization to fly any and all terminal procedures that may be presented by the system. It is the pilot’s responsibility to operate in accordance with established pertinent aircraft documents and regulatory guidance or limitations as applicable to the pilot, the aircraft, and installed equipment. NOTE: The pilot/operator must review and be familiar with Garmin’s database exclusion list as discussed in SAIB CE-14-04 to find what data may be incomplete. The database exclusion list can be viewed at flygarmin.com by selecting ‘Database Exclusions List.’ NOTE: The pilot/operator must have access to Garmin and Jeppesen database alerts and consider their impact on the intended aircraft operation. The database alerts can be viewed at flygarmin.com by selecting ‘Aviation Database Alerts.’ NOTE: If the pilot/operator wants or needs to adjust the database, contact Garmin Product Support. NOTE: Garmin requests the flight crew report any observed discrepancies related to database information. These discrepancies could come in the form of an incorrect procedure; incorrectly identified terrain, obstacles and fixes; or any other displayed item used for navigation or communication in the air or on the ground. Go to flygarmin.com and select ‘Aviation Data Error Report’. NOTE: Electronic aeronautical charts displayed on this system have been shown to meet the guidance in AC 120-76D as a Type B Electronic Flight Bag (EFB) for FliteCharts® and ChartView™. The accuracy of the charts is subject to the chart data provider. Own-ship position on airport surface charts cannot be guaranteed to meet the accuracy specified in AC 120-76D. Possible additional requirements may make a secondary source of aeronautical charts, such as traditional paper charts or an additional electronic display, necessary on the aircraft and available to the pilot. If the secondary source of aeronautical charts is a Portable Electronic Device (PED), its use must be consistent with the guidance in AC 120-76D. 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin v WARNINGS, CAUTIONS, AND NOTES NOTE: The navigation databases used in Garmin navigation systems contain Special Procedures. Before flying these procedures, pilots must have specific FAA authorization, training, and possession of the corresponding current, and legitimately-sourced chart (approach plate, etc.). Inclusion of the Special Procedure in the navigation database DOES NOT imply specific FAA authorization to fly the procedure. NOTE: Terrain and obstacle alerting is not available north of 89º North latitude and south of 89º South latitude. This is due to limitations present within the Terrain database and the system’s ability to process the data representing the affected areas. NOTE: The nose of the ‘own ship’ symbol represents the location of the aircraft. The center of any traffic symbol represents the location of that traffic. The traffic and own ship symbols are an abstract representation and do not reflect the physical extent of the aircraft/traffic, and should not replace other methods for identifying traffic. NOTE: The pilot/operator must review all portions of the flight plan following a flight plan import from any source. 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: Intruder aircraft at or below 500 ft. AGL may not appear on the Garmin SVT display or may appear as a partial symbol. NOTE: When operating the system with the magnetic sensor uncoupled from the AHRS, the displayed heading and heading information used by some system components (e.g. traffic system, AFCS, and weather radar) will be different from the heading calculated by the AHRS. The difference is an amount equal to the difference between the current Magnetic Field Variation Database (MV DB) value, and the MV DB value when the magnetic sensor was uncoupled. Due to the convergence of isogonic lines, this condition is most noticeable at or near the north and south magnetic poles. NOTE: Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground. Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition. NOTE: Operate G2000 system power through at least one cycle in a period of four days of continuous operation to avoid an autonomous system reboot. Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A vi WARNINGS, CAUTIONS, AND NOTES Blank Page 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin SOFTWARE LICENSE AGREEMENT vii SOFTWARE LICENSE AGREEMENT BY USING THE DEVICE, COMPONENT OR SYSTEM MANUFACTURED OR SOLD BY GARMIN (“THE GARMIN PRODUCT”), YOU AGREE TO BE BOUND BY THE TERMS AND CONDITIONS OF THE FOLLOWING SOFTWARE LICENSE AGREEMENT. PLEASE READ THIS AGREEMENT CAREFULLY. Garmin Ltd. and its subsidiaries (“Garmin”) grants you a limited license to use the software embedded in the Garmin Product (the “Software”) in binary executable form in the normal operation of the Garmin Product. Title, ownership rights, and intellectual property rights in and to the Software remain with Garmin and/or its third-party providers. You acknowledge the Software is the property of Garmin and/or its third-party providers and is protected under the United States of America copyright laws and international copyright treaties. You further acknowledge the structure, organization, and code of the Software are valuable trade secrets of Garmin and/or its third-party providers and the Software in source code form remains a valuable trade secret of Garmin and/or its third-party providers. You agree not to reproduce, decompile, disassemble, modify, reverse assemble, reverse engineer, or reduce to human readable form the Software or any part thereof or create any derivative works based on the Software. You agree not to export or re-export the Software to any country in violation of the export control laws of the United States of America. Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A SOFTWARE LICENSE AGREEMENT viii Blank Page 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin ix RECORD OF REVISIONS Record of Revisions Part Number Revision Date Page Range Description 190-02955-00 A Aug, 2022 All Initial Release for GDU 32.01.10 190-02955-01 A Nov, 2023 All Initial Release for GDU 32.01.30 Production Revision - Updated Warnings/Cautions/Advisories - Updated content and images Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A x RECORD OF REVISIONS Blank Page 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin xi TABLE OF CONTENTS SECTION 1 SYSTEM OVERVIEW 1.1 System Description ..............................................1 Line Replaceable Units (LRU) ..............................................1 1.2 System Controls ...................................................4 PFD Controls .......................................................................4 Primary Flight Window (PFW) / Multi-Function Window (MFW) .................................................................................5 Touchscreen Controller........................................................6 Screen Overview ...............................................................11 Controlling Display Panes .................................................24 Softkey Function ...............................................................28 Secure Digital Cards ..........................................................37 1.3 System Operation ..............................................38 System Initial Power Application .......................................38 Normal Operation .............................................................38 Reversionary Display Operation ........................................39 Touchscreen Controller Failure ..........................................40 ADAHRS Operation ...........................................................40 Standby Flight Display.......................................................41 GPS Receiver Operation ....................................................41 Annunciations ...................................................................46 1.4 Initialization .......................................................47 1.5 System Management .........................................50 Avionics Settings ...............................................................50 Avionics Status..................................................................56 Additional Setup Features .................................................57 1.6 Utilities...............................................................58 Trip Planning .....................................................................58 Minimums .........................................................................58 Trip Statistics .....................................................................58 Timers ...............................................................................59 Scheduled Messages .........................................................62 Documents ........................................................................63 Screen Cleaning ................................................................63 Crew Profiles .....................................................................64 SECTION 2 FLIGHT INSTRUMENTS 2.1 Flight Instruments ..............................................70 Airspeed Indicator .............................................................70 Attitude Indicator..............................................................73 Altimeter ...........................................................................74 Vertical Speed Indicator (VSI) ............................................78 Vertical Deviation..............................................................78 Horizontal Situation Indicator (HSI)...................................80 Course Deviation Indicator (CDI).......................................86 Required Navigation Performance and Estimated Position Error ....................................................89 GPS Above Ground Level Altitude .....................................95 Angle of Attack (AOA) Indicator........................................95 2.2 Garmin SVT™ (Synthetic Vision Technology) .....97 SVT Operation ...................................................................98 SVT Features ...................................................................100 WireAware Power Line Obstacles....................................106 Field of View ...................................................................107 2.3 Supplemental Flight Data ................................108 Wind Data .......................................................................108 Timer ...............................................................................109 Vertical Navigation (VNAV) Indications...........................109 2.4 PFD Annunciations and Alerting Functions ......111 Marker Beacon Annunciations ........................................111 Altitude Alerting..............................................................111 Low Altitude Annunciation ..............................................112 Minimum Altitude Alerting ..............................................112 2.5 Abnormal Operations.......................................114 Abnormal GPS Conditions ...............................................114 Comparator Annunciations .............................................115 Reversionary Sensor Annunciations ................................116 Garmin SVT Troubleshooting ...........................................116 Unusual Attitudes ...........................................................117 SVT Unusual Attitudes ....................................................118 Standby Flight Display.....................................................118 SECTION 3 ENGINE AND AIRFRAME SYSTEMS 3.1 Engine/Airframe Systems Indications .............122 3.2 Aircraft Systems ..............................................127 Status & Info ...................................................................128 Engine & Fuel ..................................................................129 Electrical .........................................................................131 Ice Protection ..................................................................133 System Tests ....................................................................134 3.3 Lean Assist Mode .............................................135 3.4 Reversionary Mode ..........................................136 SECTION 4 AUDIO AND CNS 4.1 Overview ..........................................................137 Touchscreen Controller Audio and CNS Controls .............138 COM/NAV Display ...........................................................140 4.2 COM Operation ................................................141 COM Transceiver Selection and Activation ......................141 COM Frequency Tuning ...................................................144 Frequency Spacing ..........................................................156 Automatic Squelch ..........................................................157 Volume............................................................................158 Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A xii TABLE OF CONTENTS 4.3 NAV Operation .................................................159 NAV Radio Selection and Activation................................159 Marker Beacon Receiver .................................................170 ADF/DME Tuning (Optional) ............................................172 4.4 Mode S Transponders .......................................174 Transponder Controls ......................................................174 Transponder Mode Selection ...........................................175 Entering a Transponder Code ..........................................177 IDENT Function ...............................................................179 4.5 Additional Audio Functions..............................180 Mono/Stereo Headsets ....................................................180 Speaker ..........................................................................180 Intercom..........................................................................181 Clearance Recorder and Player .......................................183 3D Audio .........................................................................184 Simultaneous COM Operation ........................................185 Auxiliary Audio................................................................186 Audio Feedback (Clicks) ..................................................188 Telephone .......................................................................189 Bluetooth Audio Controls ................................................190 4.6 Abnormal Operation ........................................191 Stuck Microphone ...........................................................191 COM Failure ....................................................................191 COM Tuning Discrepancy ................................................191 Navigation Failure ...........................................................192 Audio Controller Fail-Safe Operation ..............................192 Touchscreen Controller Failure ........................................192 Transponder Failure .........................................................192 SECTION 5 FLIGHT MANAGEMENT 5.1 Flight Management Navigation Data ..............193 PFW Navigation Status Box / MFW Navigation Data Bar ..195 5.2 Using Map Displays..........................................197 Map Settings Synchronization.........................................197 Map Orientation .............................................................198 Map Range .....................................................................199 Map Panning ...................................................................202 Measuring Bearing and Distance ....................................207 Absolute Terrain ..............................................................209 Map Symbols ..................................................................212 Airways ...........................................................................218 Additional Map Display Items .........................................219 5.3 Waypoints ........................................................224 Waypoint Selection .........................................................224 Airports ...........................................................................225 Non-Airport and User Created Waypoints .......................230 5.4 Airspaces ..........................................................240 Nearest Airspace .............................................................240 Smart Airspace ................................................................243 5.5 Flight Planning .................................................244 General Information........................................................244 Flight Plan Data Fields ....................................................246 Flight Plan Display ..........................................................247 Direct-to Navigation .......................................................250 Flight Plan Keypad Operation..........................................257 Creating a Basic Flight Plan ............................................269 Flight Plan Modification and Navigation.........................273 Flight Plan Operations ....................................................304 Managing Flight Plans ....................................................320 5.6 Procedures .......................................................328 Departures ......................................................................330 Arrivals............................................................................335 Approaches .....................................................................339 5.7 Weight and Balance .........................................355 Weight and Balance Planning .........................................355 Calculations ....................................................................356 Weight and Balance Caution and Warning Conditions....359 5.8 General Performance and Trip Planning ..........360 Datalink Weather for Performance Estimates ..................360 Trip Planning ...................................................................360 5.9 Takeoff and Landing Assistant (TOLA) .............365 Accessing TOLA ...............................................................365 Takeoff Data ....................................................................366 Landing Data ..................................................................374 5.10 Abnormal Operation ........................................380 FMS Degradation ............................................................380 Dead Reckoning Navigation ............................................380 SECTION 6 HAZARD AVOIDANCE 6.1 Data Link Weather............................................384 Activating Data Link Weather Services ............................385 Registering the System for Garmin Connext Services ......386 Accessing FIS-B Weather Information .............................386 Weather Product Age ......................................................388 Displaying Data Link Weather Products ..........................391 Connext Weather Data Requests.....................................401 Weather Product Overview .............................................405 Data Link Weather Product Overlays ...............................418 FIS-B Weather Abnormal Operations ...............................446 CONNEXT Weather Abnormal Operations .......................447 6.2 Stormscope Lightning Detection System .........448 Using the Stormscope Pane.............................................448 Stormscope Information on Navigation Maps ................450 Abnormal Operations ......................................................453 6.3 Vertical Situation Display Terrain .....................454 VSD Inset Window...........................................................454 Track Mode Boundary .....................................................458 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin xiii TABLE OF CONTENTS 6.4 Terrain Displays ................................................459 Relative Terrain Symbology .............................................460 Displaying Relative Terrain Information ..........................462 Terrain Pane ....................................................................462 Relative + Absolute Terrain Map Overlays ......................466 Wire Obstacle Information and Alerting ..........................468 Terrain-SVT and TAWS-B Terrain and Obstacle Alerts ......469 Additional TAWS-B Alerting ............................................474 System Status..................................................................477 TAWS-B Abnormal Operations ........................................479 6.5 TAS Traffic.........................................................480 TAS Theory of Operation .................................................480 Traffic Alerts ....................................................................484 System Test .....................................................................486 Operation ........................................................................487 6.6 ADS-B Traffic ....................................................494 ADS-B System Overview .................................................494 ADS-B With TAS...............................................................496 ADS-B Traffic Advisory System (ATAS) .............................496 Airborne and Surface Applications ..................................498 Airborne and Surface Applications ..................................499 Operation ........................................................................500 ADS-B System Status.......................................................504 SECTION 7 AUTOMATIC FLIGHT CONTROL SYSTEM 7.1 Overview ..........................................................507 Basic Autopilot Operation ...............................................507 AFCS Preflight Test (PFT) .................................................508 7.2 AFCS Controls ..................................................509 AFCS Controller...............................................................509 Additional AFCS Controls ................................................510 7.3 Flight Director Operation.................................511 Activating the Flight Director ..........................................511 AFCS Status Box..............................................................512 Flight Director Modes......................................................513 Command Bars ...............................................................513 7.4 AFCS Modes .....................................................514 Vertical Modes ................................................................514 Lateral Modes .................................................................519 Combination Modes........................................................523 Level Mode .....................................................................542 7.5 Autopilot and (Optional) Yaw Damper Operation ..543 Flight Control ..................................................................543 Engaging the Autopilot and (Optional) Yaw Damper ......544 Disengaging the Autopilot and Yaw Damper...................544 7.6 AFCS Annunciations and Alerts ........................546 AFCS Status Alerts...........................................................546 Underspeed Protection....................................................546 Overspeed Protection ......................................................548 7.7 Abnormal Operation ........................................549 Suspected Autopilot Malfunction ....................................549 Overpowering Autopilot Servos ......................................549 SECTION 8 ADDITIONAL FEATURES 8.1 Overview ..........................................................551 8.2 SafeTaxi ............................................................553 Hot Spots ........................................................................553 3D SafeTaxi .....................................................................553 Operation ........................................................................554 8.3 SurfaceWatch (Optional) ..................................556 Information Display.........................................................557 Alerts ..............................................................................558 SurfaceWatch Setup ........................................................560 Operational States ..........................................................562 8.4 Electronic Charts ..............................................563 ChartView (Optional) ......................................................564 FliteCharts (Optional) ......................................................571 IFR/VFR Charts ................................................................578 8.5 Satellite Telephone & Datalink Services (Optional) ..585 Connext Registration ......................................................585 Bluetooth Enhancements ................................................586 Contacts ..........................................................................587 Telephone Communication..............................................589 Text Messaging (SMS) .....................................................598 8.6 Position Reporting (Optional) ..........................609 8.7 Connext (Optional)...........................................611 Wireless Transceiver/PED Compatibility...........................612 Notifications ...................................................................612 Link Management ...........................................................612 Recording Mode..............................................................617 8.8 SiriusXM Satellite Radio (Optional) .................619 Activating SiriusXM Satellite Services .............................619 Using SiriusXM Radio......................................................620 8.9 Flight Data Logging .........................................624 8.10 Electronic Checklists .......................................626 Checklist Features ...........................................................626 8.11 Electronic Documents ......................................632 Installed Documents .......................................................632 User Documents ..............................................................632 Viewing Electronic Documents ........................................633 8.12 Auxiliary Video (EVS)........................................640 Modes .............................................................................640 Video Settings .................................................................643 Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A xiv TABLE OF CONTENTS 8.13 Stabilized Approach .........................................644 Alert Types ......................................................................645 8.14 Electronic Stability & Protection (ESP) ............648 Roll Engagement.............................................................649 Pitch Engagement ...........................................................651 Angle of Attack Protection ..............................................653 Low Airspeed Protection .................................................653 High Airspeed Protection ................................................653 8.15 Hypoxia Recognition & Automatic Descent Mode.... 654 Determining Pilot Alertness.............................................654 Automatic Descent Mode (ADM) ....................................655 8.16 Database Management ....................................656 Cycle Number and Revision ............................................656 8.17 Abnormal Operation ........................................659 Datalink Troubleshooting ................................................659 APPENDICES Annunciations and Alerts .........................................661 Crew Alerting System (CAS) Messages............................661 Voice Alerts ....................................................................666 System Annunciations .....................................................666 System Messages ............................................................668 Database Management ............................................687 Databases and Cycles .....................................................688 Standby Database Catalog ..............................................689 Database Auto Swap .......................................................690 SD Card Requirements ....................................................691 Seamless Database Activation ........................................691 Updating Databases When the System is Powered On ....694 Updating Databases With Garmin Pilot ..........................696 Deleting Databases .......................................................700 Magnetic Field Variation Database Update .....................702 Aviation Abbreviations, Terms, and Acronyms ..........705 Frequently Asked Questions .....................................719 INDEX Index ......................................................................... I-1 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 1 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX SECTION 1 SYSTEM OVERVIEW 1.1 SYSTEM DESCRIPTION The Cirrus Perspective+ Integrated Avionics by Garmin presents flight instrumentation, position, navigation, communication, and identification information to the pilot through large-format displays. The Garmin Automatic Flight Control System (AFCS) provides the Flight Director (FD), Autopilot (AP), Yaw Damper (YD - optional), and manual electric trim (MET) functions. Refer to the AFCS section for more information. LINE REPLACEABLE UNITS (LRU) - GDU 1250W (2) (Standard) or GDU 1450W (2) (Alternate) – The Garmin Display Unit (GDU) features a 14- inch, or optional 12-inch, light emitting diode (LED) Widescreen Ultra Extended Graphics Array (WUXGA) 1920 x 1200 resolution backlit display. In normal operation, the left/pilot side GDU operates as the Primary Flight Display (PFD) and the right/copilot side GDU operates as the Multi Function Display (MFD). The display units communicate with each other, the Touchscreen Controllers, and with the on-side Integrated Avionics Unit (IAU) through a High-Speed Data Bus (HSDB) Ethernet connection. - GTC 585 (2) – The Touchscreen Controllers are centrally located in the cockpit and provide a user interface to the system for data entry and control of the GDU displays and communication equipment.. The unit installed on the left/pilot side is designated as GTC1; the unit installed on the right/copilot side is designated as GTC2. The Touchscreen Controllers communicate with each other and the on-side GDU (PFD / MFD). GTC2 communicates with the Audio Controller. - GIA 64W (2) – The GIA, Integrated Avionics Units (IAU), function as the main communications hub, linking several LRUs with each on-side GDU. Each GIA contains a GPS Satellite-Based Augmentation System (SBAS) receiver, a very high frequency (VHF) communication/navigation/glideslope (COM/NAV/GS) receiver, a Flight Director (FD) and system integration microprocessors. The GIA units communicate directly with each other through HSDB connection. - GEA 71B (1) – Receives and processes signals from the engine and airframe sensors. This unit communicates with both GIAs using an RS-485 digital interface. - GSU 75 (2) – ADAHRS combines air data and altitude/heading data units. Processes data from the pitot/static system as well as the OAT probe to provide pressure altitude, airspeed, vertical speed and OAT information to the system. This unit also provides aircraft attitude and heading information through ARINC 429 to the PFD, MFD, and GIA. The GSU 75 contains advanced sensors (including accelerometers and rate sensors) and interfaces with the GMU to obtain magnetic field information, and with the GIA to obtain GPS information. ADAHRS modes of operation are discussed later in this document. - GMU 44B (2) – The Magnetometer measures local magnetic field and sends the data to the GSU for processing to ascertain aircraft magnetic heading. This unit receives power directly from the GSU and communicates with the it, using an RS-485 digital interface. - GTP 59 (2) – The Temperature Probe provides Outside Air Temperature (OAT) data to the GSU. - GMA™ 36B (1) – The Audio Controller integrates navigation/communication radio (NAV/COM) digital audio, intercom, and marker beacon audio. It is connected to GTC2 and each IAU. - GMC 707 (1) – Provides the controls for the Garmin AFCS through an RS-232 digital interface allowing communication with the PFD and MFD. Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A 2 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX - GTX 335R (1) or GTX 345R (1) (Alternate) – Solid-state transponders that provide Modes A, C, S and ADS-B capability. The optional GTX 345R also provides ADS-B In/Out. The transponder can be controlled from the GTCs. The transponder communicates with the both GIAs through an RS-232 digital interface. - GSA 87 (2) – The Servos are used for automatic control of the pitch, roll, and optional yaw damper. These units interface with each IAU. - GTA 82 (1) – The Pitch Trim Adapter takes input from the trim switches, GIA and GSA to control the DC motor to drive the aircraft trim system. - GTS 800 (1) (Optional) – The 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 Audio Panel. - GDL 69A SXM (1) (Optional) – The Data Link Satellite Radio Receiver provides weather information to the MFD (and, indirectly, to the inset map of the PFD) as well as digital audio entertainment. The unit communicates with the GTC1 through an HSDB connection. A subscription to the SiriusXM Satellite Radio and/or SiriusXM Weather service is required to enable the GDL 69A SXM capabilities. - GSR 56 (1) (Optional) – The Iridium Transceiver provides telephone voice communication by means of pilot and copilot headsets. The unit can also send and receive data over the Iridium satellite network. The GSR 56 is connected the #1 GIA 64W with an RS-232 digital interface, with analog connections to the audio panel. - Flight Stream 510 (1) (Optional) – Provides wireless connectivity between a compatible tablet/mobile device and the avionics system. It is inserted into an MFD Secure Digital (SD) card slot. Figure 1-1 shows interactions between the LRUs. Additional/optional equipment are also shown in Figure 1-1. The system is capable of interfacing with the following optional equipment: - Enhanced Vision System - KN 63 DME - KR 87 ADF - CO Guardian Carbon Monoxide Detector - L3 Stormscope WX 500 Lightning Detection NOTE: For information on non-Garmin equipment, consult the applicable optional interface user’s guide. This document assumes the reader is already familiar with the operation of this additional equipment. 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 3 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX GTX 335R or GSR 56 (Iridium Transceiver) KN-63 (DME) #1 GIA 64W (Integrated Avionics Unit) VHF COM GPS/SBAS VOR/LOC G/S Flight Director AFCS Mode Logic Servo Logic #2 GIA 64W (Integrated Avionics Unit) VHF COM GPS/SBAS VOR/LOC G/S Flight Director AFCS Mode Logic Servo Logic Non-Garmin Equipment CO Guardian Stormscope GEA 71B (Engine & Airframe I/F) GTX 345R (Transponder) #2 GSU 75 (ADAHRS) #1 GSU 75 (ADAHRS) Optional Garmin Equipment Optional Non-Garmin Equipment #1 GMU 44B (Magnetometer) #2 GMU 44B (Magnetometer) Garmin Equipment #1 GSA 87 (Pitch) #3 GSA 87 (Yaw) #2 GSA 87 (Roll) #4 GTA 82 (PTrim) KR-87 (ADF) GMA 36B (Audio Panel) RDM (Data Logger) Standby Flight Instruments #1 GDU 1250W or GDU 1450W (PFD) GDL 69A SXM (XM Weather/ Audio Datalink) #2 GDU 1250W or GDU 1450W (MFD) GMC 707 (AFCS Controller) Enhanced Vision System FS 510 (SD Card Bluetooth Transceiver) GTS 800 (TAS) #1 GTC 585 (Touchscreen Controller) #2 GTC 585 (Touchscreen Controller) Figure 1-1 LRU Block Diagram Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A 4 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 1.2 SYSTEM CONTROLS The system controls are located on the GTCs, PFD, MFD, and AFCS Controller. These controls simplify operation, minimize crew workload, and reduce the time required to access sophisticated functionality. The Touchscreen Controllers are discussed in this section. AFCS controls are described in the AFCS section. See the Audio and Communication/Navigation/Surveillance (CNS) Section for detailed information about NAV/COM controls. Figure 1-2 System Controls AFCS Controller GTC1 GTC2 PFD MFD PFD CONTROLS Figure 1-3 PFD Controls PFD Softkeys 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 5 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Selection softkeys are located along the bottom of the PFDs. The softkeys shown depend on the softkey level previously selected. The bezel keys below the softkey labels can be used to select the appropriate softkey. There are three types of softkeys. One selects a simple on/off state, indicated by an annunciator on the softkey label displayed as green (on) or gray (off). The next type of softkey selects among several options, indicated by the softkey label changing (with the exception of the Map Range keys) to reflect the name of the chosen option. The last type of softkey, when pressed, displays another set of softkeys available for the selected function. Also, these softkeys revert to the top level after 45 seconds of inactivity. When a softkey function is disabled, the softkey label is subdued (dimmed). When the PFD is in Split Mode, an alternate softkey configuration is shown with a reduced number of softkeys displayed on the left pane. Figure 1-4 Top Level PFD Softkeys Softkey Names (GPS Selected for the CDI) Bezel-Mounted Softkeys (Press) Selected Function On Subdued Softkey (Function Unavailable) PFD Softkeys in Full and Reversionary Modes PFD Softkeys in Split Mode PRIMARY FLIGHT WINDOW (PFW) / MULTI-FUNCTION WINDOW (MFW) The PFW and MFW are the graphical content viewed on the PFD and MFD respectively, while the PFD and MFD are the complete display units with screens, bezels and softkeys. Typically, the PFD depicts the PFW display containing primary flight information, while the MFD displays the MFW which depicts the EIS and various selectable MFW panes (e.g., Navigation Map). Figure 1-5 PFW and MFW Displays on PFD and MFD in Normal and Half Mode PFW Display on PFD MFW in Half Mode On MFD with Two MFW Display Panes PFW PFD MFD MFW MFW Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A 6 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX In split-screen mode, the PFD can display one MFW window in addition to PFW content. The MFD can display PFW content, but only in Reversionary mode. See descriptions for the Touchscreen Controller functions and Reversionary mode for more information on the display of the PFW and the MFW. PFD in Split Mode with PFW and MFW Display Pane PFW and MFW on MFD in Reversionary Mode Figure 1-6 PFW and MFW Displays in Reversionary / Split Screen Modes PFW PFD PFD PFW MFW MFW TOUCHSCREEN CONTROLLER The two Touchscreen Controllers, designated as GTC1 and GTC2, are panel-mounted user interfaces allowing for ease of data entry, Display Pane operation, and NAV/COM tuning. Many procedures in this Pilot’s Guide are performed using a Touchscreen Controller. The PFW and MFW softkeys provide buttons for controlling the Primary Flight Window (PFW) and Multi- function Window (MFW) that appear on the displays. The NAV COM softkey provides the control for the ‘NAV/COM Home’ Screen on the Touchscreen Controller. 7 8 5 6 1 2 3 4 Figure 1-7 Touchscreen Controller 1 Screen Title Displays the title of the current screen. 2 Screen Displays set of context sensitive controls and data. 3 Button Bar Displays System level buttons (e.g., Home, MSG, Full/Half/Split, Scroll Up/Down, Back, Enter, Cancel). 4 Label Bar Displays labels to show status and current functions of knobs and softkeys, when functions are available. 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 7 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX 5 Small Upper Knob Provides functions as labeled on the Label Bar (e.g., Display Pane selection, COM Freq/ switching/Hold, data entry/map panning). 6 Large Upper Knob Provides functions as labeled on the Label Bar (e.g., Display Pane selection, COM Freq/ switching/Hold, data entry/map panning). 7 Softkeys Provides functions as labeled on the Label Bar (e.g., PFW, MFW, NAV/COM selection). 8 Lower Knob Provides functions as labeled on the screen (e.g., COM volume/squelch/map range adjustment/checklist item control). The Touchscreen Controller uses a grid of infrared beams and sensors to detect the location of touch input, even when the operator is wearing gloves. Objects or debris on the glass surface can interfere with these infrared beams and cause unintended activation of buttons. A screen cleaning procedure, described later in this section, is available to temporarily disable the touch recognition capability to facilitate screen cleaning. In normal operation, GTC 1 can control the PFW, MFW and NAV/COM, while GTC 2 can control the PFW and NAV/COM. The crew selects a control mode for a given controller (e.g., PFW, MFW, NAV/COM) by pressing context-sensitive softkeys located on the right portion of each controller bezel. These softkeys are aligned with labels for each control mode currently available on a given controller. A box appears around the selected control mode, and a green arrow points to the currently selected softkey. The Touchscreen Controller functions are arranged by screen. Each screen has a title which appears at the top of the screen area. The contents of each screen change dynamically in response to the selected control mode, and to crew or system input. At the top level of each mode is a corresponding home screen containing mode- specific controls. ‘PFW Home’ is the home screen for PFD / PFW control mode. ‘MFW Home’ is the home screen for MFD / MFW (i.e., Display Pane) control mode. ‘NAV/COM Home’ is the home screen for NAV/COM control mode. The Touchscreen Controller available functions for the selected control mode are accessible from the ‘MFW Home’ Screen. The ‘MFW Home’ Screen may be accessed any time it is not currently displayed by touching the Home Button in the Button Bar, below or to the right of the screen area. Procedures in this Pilot’s Guide generally begin from the ‘MFW Home’ Screen as a reference point. However, it is not necessary to return to the ‘MFW Home’ Screen before performing each procedure if the appropriate screen is already displayed. As the Touchscreen Controller is used, certain selections will cause another screen to be displayed. To return to the previous screen, touch the Back or Cancel Button (as applicable) in the Button Bar, or touch the Home Button to return to the ‘MFW Home’ Screen. If the ‘MFW Home’ Screen was the previous screen, pressing either the Back or Home Button will also return to the ‘MFW Home’ Screen. If the system issues a message, the MSG Button is shown. Touching this button will display the ‘Notifications’ Screen. The Button Bar also contains buttons for controlling the size of MFW Display Panes (Full or Half Mode), and PFW Display Panes (Full or Split Mode), discussed later in this section. The following buttons may be displayed on the Button Bar, depending on current availability and/or settings. Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A 8 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Returns to the Home Screen Selects split display mode on the PFD. Returns to the previous screen Selects half-display mode on the MFD. Displays the ‘Notifications’ Screen on Touchscreen Controller. Flashes when a new system message is issued. The button will display as ‘WARN’ or ‘CAUT’ in red or amber respectively to alert of warning and caution messages. Refer to the Appendices Section for more information about the alerting system. Selects full-display mode when controlling the MFD. Selects full display mode when controlling the PFD. Displays the Telephone ‘Notifications’ Screen on Touchscreen Controller. Flashes when a new telephone call is received. Scrolls up in a list Displays the ‘Initialization’ Screen on Touchscreen Controller. Button appears on the ‘MFW Home’ Screen if initialization tasks have not been completed. Scrolls down in a list During Initialization, selects the next Task in the Initialization process. Cancels data entry and returns to the previous screen Displays the ‘SMS Text Messaging’ Inbox Screen on Touchscreen Controller. Flashes when a new SMS message is received. Accepts entered data into the system. Displays the Connext ‘Notifications’ Screen on the Touchscreen Controller. Flashes when a new Connext message is received. Opens ‘Direct To’ Screen on the Touchscreen Controller The Label Bar, on the right side of the Touchscreen Controller, displays the current function of each control as a reference. These functions include Map Range adjustment, Display Pane selection, radio volume/squelch adjustment, COM radio tuning, and data entry. The labels change based on the context of the options being performed. If a Touchscreen Controller knob cannot be used because of a failure in a system component (COM, NAV, Audio, etc.), the Label Bar also indicates this status; refer to the Audio and CNS Section for more information about radio failures. The Touchscreen Controller recognizes input based on a touch, a gesture (such as sliding a finger), or by pressing or turning the knobs or softkeys. On-screen buttons are selected by momentarily touching them with a finger and then releasing. It is not necessary to apply pressure, as the infrared touchscreen surface detects only the presence and movement of the finger, not pressure. When touched, the button background is highlighted in blue until the finger is released. If enabled, an aural ‘click’ sound is also issued to confirm the button has been touched. When releasing the finger, make sure it is released within the boundary of the button, otherwise the input is considered invalid. If enabled, an aural tone is heard to indicate the touch input was not accepted. 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 9 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Some adjustments are made using horizontal or vertical sliders. To use, simply touch within the slider box and slide the finger in the desired slider bar direction, then release the finger. The finger may move outside of the slider box during adjustment; slider movement stops when either the finger is released or the slider has reached its maximum travel. In some cases, the slider can also be adjusted by touching a + or - Button if it accompanies the slider, such as in the Map Detail Adjustment Slider shown in the following figure. In addition, a slider adjustment may also be accomplished using knobs on the Touchscreen Controller if the Label Bar indicates the selected slider supports this additional control. Volume Adjustment Slider Figure 1-8 Sliders on the Touchscreen Controller Map Detail Adjustment Slider When a window on the Touchscreen Controller screen contains more information than the window can currently show, a scroll bar and scroll buttons appear. To scroll inside of a window, touch the controller while moving the finger up or down accordingly or touch and drag the finger up or down. To scroll more quickly, move the finger up or down rapidly. Scrolling can also be performed by pressing the Up or Down scroll buttons, each touch of the scroll button will display one ‘page’ of information. Press and hold the Up or Down scroll buttons for a continuous scroll. Some screens provide tabs as a means to group multiple categories of information or buttons. Touch the desired tab to display its contents and manage settings or information. The selected tab is highlighted. Selected Tab Highlighted Other Available Tabs Figure 1-9 Touchscreen Controller with Tabs and Scroll Arrows Scroll Bar Scroll Arrows Elements on the Touchscreen Controller screens (such as buttons and sliders) may appear subdued to indicate their functions are currently not available. Generally, pilot-selectable fields appear in cyan. In some cases, the system may highlight the expected button in cyan which completes a data entry process or function. Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A 10 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Touch the highlighted button to activate the Direct-To function Figure 1-10 Subdued Buttons on Touchscreen Controller Button subdued until Direct-To is activated BUTTON TYPES Annunciator Buttons operate in an on/off state. An ‘on’ or enabled button displays a green annunciator; an ‘off’ or disabled button displays a subdued annunciator. Touch the annunciator button to change its state. On or Enabled Off or Disabled Figure 1-11 Touchscreen Controller Annunciator Buttons Datafield Buttons can be modified based on information the pilot can enter or change, and often contain cyan alphanumeric text. Touching datafield buttons will either display a pop-up window from which a selection can be made, or display a keypad to supply the data. See the Data Entry discussion in this section for more information. Options for Selected Datafield Button Datafield Buttons Selected Datafield Button Figure 1-12 Touchscreen Controller Datafield Buttons If a system failure causes a button function to be inaccessible, an amber ‘X’ appears over the button. These buttons will not respond if touched. 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 11 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX SCREEN OVERVIEW The following is a brief overview of the major screens used to access Touchscreen Controller functions. Additional specific screens used to perform functions are shown and discussed in detail throughout this Pilot’s Guide. NOTE: Screen appearance including available buttons may differ based on installed options and equipment. MFW MODE TOUCHSCREEN CONTROLLER SCREENS MFW HoMe or Shows ‘Navigation Map’ Pane in the selected Display Pane. When the ‘Navigation Map’ Pane is displayed, the button becomes the Map Selection Button. Touch the Map Selection Button to access the ‘Map Settings’ Screen on the Touchscreen Controller. or Shows ‘Traffic Map’ Pane in the selected Display Pane. When the ‘Traffic Map’ Pane is displayed, the button becomes the Traffic Settings Button. Touch the Traffic Settings Button to access the ‘Traffic Settings’ Screen on the Touchscreen Controller. or Shows a ‘Weather <SiriusXM, Connext, Stormscope, or FIS-B>’ Pane in the selected Display Pane. When the weather pane is displayed, the button becomes the Weather Selection Button. Touch the Weather Selection Button to access the ‘Weather Selection’ Screen on Touchscreen Controller. Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A 12 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX or Shows the ‘TAWS’ Pane in the selected Display Pane. When the ‘TAWS’ Pane is displayed, the button becomes the TAWS Settings Button. Touch the TAWS Settings Button to access the ‘TAWS Settings’ Screen on Touchscreen Controller. Accesses ‘Flight Plan Information’ Screen on Touchscreen Controller. Accesses ‘Active Flight Plan’ Screen on the Touchscreen Controller. Accesses ‘Procedures’ Screen on Touchscreen Controller. Additional map displays may be shown as procedures are selected. Accesses ‘Charts’ Screen on Touchscreen Controller. Charts are shown on the selected Display Pane. Accesses ‘Systems’ Screen on Touchscreen Controller. Systems data can be selected for display on the Touchscreen Controller, and displayed on a Display Pane. Also provides access to systems controls, systems tests, and optional video controls. Accesses the Checklists for display in the selected Display Pane. Accesses the ‘Services’ Screen on Touchscreen Controller. Includes optional Iridium phone, and text messaging services, Networks and Pairing, Bluetooth Phone, Music, Position Reports, Connext Setup, and Contacts. Accesses the ‘Utilities’ Screen on Touchscreen Controller. Includes Trip Planning functions, Minimums, Trip Statistics, Timer, Scheduled Messages, FMS Sensors, Initialization, Electronic Documents (optional), Screen Cleaning, Crew Profile, and Setup. If SurfaceWatch option is not installed, Weight and Balance functions are also on the ‘Utilities’ Screen. Accesses the ‘PERF’ Screen. Provides controls for entering takeoff, landing, PERF Datalink wind and temperature and weight and balance data and speed bugs. Provides information about Airports, Intersections, VORs, NDBs, VRPs, User Waypoints. Also allows creation of User Waypoints. Provides information about the nearest Airports, Intersections, VORs, NDBs, VRPs, User Waypoints, Airspace, ARTCC facilities, Flight Service Stations, and Weather reporting stations. 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 13 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX ‘Map Selection’ Screen Touching the Map Button on the ‘Map Selection’ Screen displays the ‘Navigation Map’ Pane and the button name will change to Map Settings. Additionally, once touched, the Map Settings Button displays the ‘Navigation Map Settings’ Screen which is discussed in the Flight Management Section. Touching the VFR, IFR Low, or IFR High Buttons will respectively display the ‘VFR’, ‘IFR Low’, or ‘IFR High’ Panes. After touching the IFR Low or IFR High Button, the button name will change to ‘IFR Low Settings’ or ‘IFR High Settings’ respectively. Touching either settings button again opens the ‘IFR/VFR Charts Settings’ Screen which is discussed in the Additional Features Section. Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A 14 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX ‘WeatHer Selection’ Screen Touching a button within the ‘Weather Selection’ Screen (shown above) will display a respective ‘SiriusXM Weather’, ‘Connext Weather’, ‘Stormscope’ or ‘FIS-B Weather’ Pane. Additionally, once touched, the button name will change to a ‘Settings’ syntax. Touching any of these ‘settings’ buttons will open a settings screen discussed in the Hazard Avoidance Section. 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 15 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX ‘aircraFt SySteMS’ Screen Shows the ‘Status & Info’ Pane, with synoptic information about the aircraft doors, brakes, oxygen and oil temperature. Also shows approximate values and parameters for certain performance calculations. Shows the ‘Engine & Fuel’ Pane, with information about fuel quantities, flow, valve, pump states and other engine information (e.g. CHT/EGT, MAP, and MAT). When the Engine & Fuel Button is touched, the Lean Assist Button will be displayed on the ‘Aircraft Systems’ Screen. Shows the ‘Electrical Power’ Pane, with information about the batteries, alternators, and electrical buses. Shows the ‘Video’ Pane in the selected Display Pane. Provides controls for adjusting EVS video on the display (brightness, contrast, saturation). Shows the ‘Ice Protection’ Pane, with synoptic information about the ice protection system, OAT, and pitot and AOA heat. When the Ice Protection Button is touched, the IPS Left, IPS Auto, and IPS Right buttons will be displayed on the ‘Aircraft Systems’ Screen. Displays the ‘System Tests’ Screen. This screen provides controls for testing the following systems: ADS-B and optional TAWS. Provides functions accessible to maintenance personnel with password. Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A 16 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX ‘ServiceS’ Screen The ‘Music’ Screen provides controls for the optional SiriusXM Satellite Radio including channel information, selection, and volume settings. Accesses the optional ‘Connext Position Reports’ Screen. Provides controls for sending automatic or manual position reports. Accesses the optional ‘Contacts’ Screen for management of contact information including phone and email addresses. Also provides quick access to stored contacts using phone, SMS, or email. The ‘Satellite Phone’ Screen (available with the Iridium voice telephone option) shows the status of the Iridium satellite telephone connection and provides telephone controls. Provides controls and settings for networks and for pairing of devices. The ‘Satellite SMS Text Messaging’ Screen (available with the Iridium voice telephone option) provides management of incoming and outgoing SMS (short message service) text messages. The ‘Pilot Bluetooth Phone’ Screen allows for adjustment of Bluetooth phone settings. Provides settings for automated database downloads, Personal Electronic Device (PED), Aircraft Report Intervals, Connext Registration (REG Tab), and time and dates for past and future automated database downloads (Events Tab). 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 17 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX ‘UtilitieS’ Screen Shows the ‘Trip Planning’ Pane in the selected Display Pane, and accesses the ‘Trip Planning’ Screen on the Touchscreen Controller. Accesses the ‘Minimums’ Screen on the Touchscreen Controller. Provides controls for the Minimum Descent Altitude/Decision Height alerting function. Button displays the current minimums altitude and source if provided. Accesses the ‘Trip Statistics’ Screen on the Touchscreen Controller. Shows information regarding Flight Time, Departure/Arrival Time, Odometer, Trip Odometer, Trip Air Odometer, Fuel Used, Average Ground Speed, Maximum Ground Speed, Average Wind Speed, Average Wind Direction, Sunrise, and Sunset. Total Time and Flight Time are displayed in the ‘Trip Statistics’ Window. Also provides settings for resetting trip statistics. Accesses the ‘Timer‘ Screen on the Touchscreen Controller. Controls the timer on the PFD. Used to create custom messages to be displayed one-time or periodically. The Touchscreen Controller displays these System Messages on the ‘Notifications’ Screen. Accesses the ‘Sensors’ Screen to change RNP, update the aircraft position, enable/disable sensors, and check sensor status and RAIM. Displays the ‘GPS1…’ or ‘GPS2 Status’ Pane. Displays the ‘Initialization’ Screen on the Touchscreen Controller. Provides controls for selecting the Crew Profile, checking Database Status, Safety Info, Initial Fuel, Weight and Balance, Flight Plan, and optional Takeoff Data. Shows optional controls for viewing electronic documents on the Touchscreen Controller, and displays documents in the selected Display Pane. Feature temporarily disables touchscreen glass input to allow for manual cleaning. Turn or press any knob or softkey on the Touchscreen Controller to exit Screen Cleaning Mode. Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A 18 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Displays ‘Crew Profile’ Screen, which provides controls for activating and managing crew profiles. Displays the ‘Setup’ Screen, which provides controls for avionics settings and status, SiriusXM Info, ADS-B Status and for displaying the status of avionics databases. ‘SetUp’ Screen Provides controls for changing system avionics settings, such as, time format, units of measure, airspace alert settings, and MFD Data Bar Fields. Displays information on the Touchscreen Controller for installed LRUs, system software, and databases. Shows the ‘SiriusXM Information’ Screen on the Touchscreen Controller. Used to activate audio and data services from SiriusXM Satellite Radio and to verify subscriptions of SiriusXM Weather products. Provides access to the ‘Database Status’ Screen for checking database cycle information. Provides access to the optional ‘ADS-B’ Status Screen for information on the reception of ADS-B services. 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 19 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX ‘perF’ Screen NOTE: SurfaceWatch option required for ‘PERF’ Screen to be shown. Aircraft takeoff, landing, and performance related functions, settings, and processes for the buttons within the ‘PERF’ Screen are discussed in the Flight Management Section. ‘Waypoint inFo’ Screen Functions, settings, and processes for the buttons within the ‘Waypoint Info’ Screen are discussed in the Flight Management Section. Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A 20 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX ‘neareSt’ Screen Functions, settings, and processes for the buttons within the ‘Nearest’ Screen are discussed in the Flight Management Section. PFW MODE TOUCHSCREEN CONTROLLER SCREENS pFW HoMe Cycles through GPS, LOC1/VOR1 and LOC2/VOR2 navigation modes on the CDI 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 21 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX or Selects OBS mode on the CDI when navigating by GPS (only available with active leg). When OBS is active the annunciator is green. Selects SUSP mode on the CDI when navigating by GPS. When SUSP is active the annunciator is green. Displays pop-up window with selection buttons for Bearing 1 Pointer selections Off, NAV1, NAV2, GPS, ADF, BEST GLIDE, and WPT. Displays pop-up window with selection buttons for Bearing 2 Pointer selections Off, NAV1, NAV2, GPS, ADF, BEST GLIDE, and WPT. CAS messages cannot be scrolled. These buttons will remain inactive. Accesses the ‘Speed Bugs’ Screen on Touchscreen Controller, where the speed bugs can be configured. Accesses the ‘Timer’ Screen on the Touchscreen Controller. Controls timer on PFD. Accesses the ‘Minimums’ Screen on the Touchscreen Controller. Set MDA or DH. Shows the Traffic Map on the PFD in inset format when the PFD is in Full Mode and turns the annunciator green. Shows the ‘Traffic Map’ Pane on the PFD when the PFD is in Split Mode, but the green/subdued annunciator is no longer displayed. Accesses the ‘PFD Map Settings’ Screen on the Touchscreen Controller. The Inset Map is not available when in split mode. Accesses the ‘Sensors’ Screen. Allows for manual selection of ADC and AHRS sensors, and access to RNP/EPE settings and Position Sensors settings. Accesses the ‘PFD Settings’ Screen to view or set PFD Mode, Flight Director Active Format, SVT, Flight Path Marker, AOA, Horizon Heading, Wind, Meters Overlay, Baro Select Units, Time Format, Time Offset, COM Channel Spacing, and Screen Cleaning function. Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A 22 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX PFD Settings Deactivates touch input on the Touchscreen Controller to facilitate cleaning. Press or turn a knob on the controller to resume touch input. PFD Tab Synthetic Vision Button selects Synthetic Vision Mode on the PFD. • Auto: Selects SVT Auto Mode. • Flight: Selects SVT Flight Mode. • Off: SVT is off. Shows the type of Flight Director available. Single Cue is the only available format. Enables/disables display of compass heading along the Zero-Pitch line. When Enabled, the annunciator is green. Button is subdued when synthetic terrain is disabled. Option 1: Wind direction arrows with wind direction and speed. Option 2: Wind direction arrows with headwind and crosswind components. Selects the display mode for the Angle of Attack (AOA) indicator on the PFD. • Auto: Automatically displays the Angle of Attack Indicator when the aircraft is in a landing configuration, or when normalized AOA is greater than 0.35. • On: Displays the Angle of Attack (AOA) Indicator on the PFD / PFW. • Off: Removes AOA Indicator from the PFD / PFW. 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 23 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Enables/disables the display of the meter overlay on the Altimeter. Inches (IN): Displays the BARO setting as inches of mercury. Hectopascals (HPA): Displays the BARO setting as hectopascals. General Tab Selects the Time Format: Local 12hr, Local 24hr, or UTC. Displays the Local and UTC time offset. Selects the COM Channel Spacing: 25 kHz or 8.33 kHz. PFD Sensors Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A 24 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX PFD Tab Accesses the ‘ADC Sensor’ Screen where the #1 or #2 Air Data Computer (ADC) can be manually selected. Accesses the ‘AHRS Sensor’ Screen where the #1 or #2 AHRS sensors can be manually selected. RNP/EPE Tab Accesses button to change RNP Setting. Displays GPS current position. Refer to content later in this section for more information. Position Sensors Tab Accesses buttons to select SBAS and SBAS settings, select GPS1 and GPS2 sensors, check sensor status and RAIM. Displays the ‘GPS1...’ or ‘GPS2 Status’ Pane. Refer to content later in this section for more information. CONTROLLING DISPLAY PANES In normal operations, the pilot uses GTC1 to select and control Display Panes in MFD control mode. The system highlights the border of the selected display pane being controlled in cyan (purple in Reversionary Mode). The Label Bar indicates when the upper knobs may be used to select a Display Pane for control by displaying the word ‘Pane’ with three icons below it representing each possible pane location. The configuration of each display determines the number of Display Panes currently available for control (Full, Half, or Split Modes). A cyan (purple in Reversionary Mode) icon represents the selected Display Pane. A black icon represents a Display Pane available for selection, but is not currently selected. A subdued icon represents a Display Pane not currently shown, and therefore cannot be controlled. See the following figures for examples of touchscreen control of Display Panes in MFD Mode. Selectable Display Pane (Black Icon) Selected Display Pane (Cyan/Purple Icon) Display Pane cannot be selected (Gray Icon) Figure 1-13 Touchscreen Controller Display Pane Control Icons MFD FULL AND HALF MODES The MFD provides the capability to show Display Panes in either Full Mode or Half Mode, provided the selected Display Pane is capable of being shown in a Full Mode format. The presence of either the Full or Half Mode Button on the Touchscreen Controller Button Bar indicates the availability of one of these modes for the selected Display Pane. Touch the Full Button to show the selected Display Pane in Full Mode. Touch the Half Button to return to Half Mode. In Full Mode, the MFD shows the EIS Display and a single, enlarged Display Pane. In Half Mode, the MFD shows the EIS Display and two Display Panes (mode selections do not affect the EIS Display formatting). When in Reversionary Mode, MFD Full and Half modes are unavailable, GTC 1 converts to the SFD (standby flight display) and GTC 2 controls the PFW / MFW split screen. See ‘Reversionary Display Operation’ in this section for more information. When system power is applied on the ground, the MFD begins operation in Half Mode. 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 25 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX PFD FULL AND SPLIT MODES The PFD shows a full PFD display in Full Mode, and a condensed PFD with a Display Pane in Split Mode. The Display Pane on the PFD in Split Mode is the same size as a Display Pane on the MFD in Half Mode. A Full or Split Button in the Button Bar indicates which display mode is available for the PFD. Additionally, a PFD Mode Button is available on the ‘PFD Settings’ Screen, which can be used to select Full or Split Mode on the PFD. Display panes can only be chosen from the ‘MFW Home’ Screen on the GTC 1. PFD in Split Mode with a Display Pane GTC2 in MFD Mode Figure 1-14 GTC2 Display Pane Control from the MFD Home Screen (PFD Split Mode active) MFD in Half Mode with two Display Panes Selected Pane (Cyan/Purple) Display Panes Available for Selection Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A 26 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX PFD in Full Mode (no Display Pane) GTC2 in MFD Mode Figure 1-15 GTC2 Display Pane Control from the MFD Home Screen (MFD Half Mode active) MFD in Half Mode with two Display Panes Display Pane Not Available Selected Display Pane Display Pane Available for Selection PFD in Full Mode (no Display Pane) MFD in Full Mode with one Display Pane Figure 1-16 GTC2 Display Pane Control from the MFD Home Screen (MFD Full Mode active) Display Pane Not Available Selected Display Pane Display Pane Not Available GTC2 in MFD Mode 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 27 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX DATA ENTRY Two methods exist for directly entering alphanumeric data (e.g., waypoint identifiers, barometric minimum descent altitude) into the system: using the Touchscreen Controller alphanumeric keypad, or the large and small upper knob on the Touchscreen Controller. In some instances, such as when entering an identifier, the system anticipates the desired identifier based on the characters being entered. In this case, if the desired identifier appears, use the Enter Button to confirm the entry without entering the rest of the identifier manually. This can save the pilot from entering all the characters of the identifier. Besides character-by-character data entry, the system also provides a shortcut for entering waypoint identifiers. When the cursor is on a field awaiting entry of a waypoint identifier, touching the Find Button accesses four different lists of waypoint identifiers for quick selection: Recent, Nearest, Flight Plan (if active flight plan waypoints are available), and a Favorite waypoints list. In addition, the system provides the ability to search by Facility Name or by City. The system automatically completes the identifier, facility, and city fields with the information for the selected waypoint. Using the Touchscreen Controller keyboard to enter alphanumeric data: 1) Select a Datafield Button on the Touchscreen Controller for which data entry is required (i.e. waypoint, radio frequency, etc.). A keypad will appear, and the Datafield Button will be highlighted in cyan. 2) Touch the desired letters or numbers, one at a time. 3) If an alphabetic keypad is displayed and numbers are desired, touch the 123... Button. 4) If the numeric keypad is displayed and letters are desired, touch the ABC... Button. 5) To accept the entry, touch the Enter Button. Otherwise, touch the Back, Cancel, or Home Button (on the Button Bar) to exit the datafield without saving the entry. Touch to Use Alphabetic Buttons Figure 1-17 Entering Text on the Keypad Touch to Use Numeric Buttons Using the Touchscreen Controller large and small upper knobs to enter data: 1) Select a datafield button on the Touchscreen Controller for which data entry is required (i.e. waypoint, radio frequency, etc.). A keypad will appear, and the data field will be highlighted in cyan. 2) Begin entering data by turning the small upper knob to select a character for the first placeholder. Turning the knob to the right scrolls through the alphabet (where appropriate) toward the letter Z, starting in the middle at K, and the digits zero through nine. Turning the knob to the left scrolls in the opposite direction. 3) Turn the large upper knob to move the cursor to the next placeholder in the field. 4) Repeat, using the small upper knob to select a character and the large upper knob to move the cursor, until the field is complete. 5) Push the upper knob or touch the Enter Button to confirm entry. Otherwise, touch the Back or Home Button to exit the field without saving the entry. Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A 28 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX SOFTKEY FUNCTION Selection softkeys are located along the bottom of the displays. The softkeys shown depend on the softkey level previously selected. The bezel keys below the softkey labels can be used to select the appropriate softkey. There are three types of softkeys. One selects a simple on/off state, indicated by an annunciator on the softkey label displayed as green (on) or gray (off). The next type of softkey selects among several options, indicated by the softkey label changing (with the exception of the Map Range keys) to reflect the name of the chosen option. The last type of softkey, when pressed displays another set of softkeys available for the selected function. Also, these softkeys revert to the top level after 45 seconds of inactivity. When a softkey function is disabled, the softkey label is subdued. Softkey Names (displayed) Figure 1-18 Softkeys (First-Level PFD Configuration) Bezel-Mounted Softkeys (press) Softkey On Softkey Subdued PFD SOFTKEYS The PFD softkeys provide control over the PFW display and some flight management functions, including GPS, NAV, terrain, traffic, and weather (optional). Each softkey sublevel has a Back Softkey which can be pressed to return to the previous level. The following table describes PFD Softkey functions. Softkeys which display another set of softkeys are indicated in the table by showing the given set as an increased level. For example, the Map/HSI softkey is shown in the Level 1 column. When pressed, the PFD Map Settings Softkey will display another set of softkeys and these softkeys are explained in the Level 2 column. If a softkey on Level 2 provides yet another set of softkey functions, those new available softkeys are then explained in the Level 3 column, etc. Level 1 Level 2 Level 3 Level 4 Description Map Range - Decreases the PFD Map display range. Map Range + Increases the PFD Map display range. PFD Map Settings Displays the PFD Map display settings softkeys. Map Layout Displays softkeys used to select map layouts. Map Off Removes the PFD Map from the display. Inset Map Displays the Inset Map. HSI Map Displays the HSI Map. Inset Traffic Overlays a dedicated traffic display on the Inset Map. HSI Traffic Overlays a dedicated traffic display on the HSI. Detail Selects desired amount of map detail; cycles through declutter levels (only available if HSI Map is enabled): All (no declutter): All map features visible. DCLTR 1: Declutters land data. DCLTR 2: Declutters land and SUA data. Least: Removes everything except for the active flight plan. 190-02955-01 Rev. A Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 29 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Level 1 Level 2 Level 3 Level 4 Description Weather Legend Displays or removes the name of the selected data link weather provider (SiriusXM, Connext, FIS-B) and the weather product icon and age box (for enabled weather products). Traffic Adds or removes the display of traffic on the PFD Map. The softkey annunciator is green when the traffic function is on. When the traffic function is off, the annunciator is gray. Storm- scope Adds or removes the display of Stormscope information on the PFD Map (optional). The softkey annunciator is green when the function is on. When the function is off, the annunciator is gray. Terrain Settings Selects the display of terrain information softkeys on the PFD Map: Off Removes terrain information from the PFD Map. Absolute Displays absolute terrain information. Relative Displays relative terrain information. Absolute + Relative Displays absolute and relative terrain information on the HSI Map. Data Link Settings Displays data link settings softkeys based on current installation and configuration options. Data Link Selects the data link source for weather data displayed on the PFD Map (optional): Connext: Selects Garmin Connext as the weather source. SiriusXM: Selects SiriusXM as the weather source. FIS-B: Selects FIS-B as the weather source. NEXRAD Selects type of NEXRAD coverage when FIS-B is the selected data link source: CONUS: Selects coverage for continental U.S. Regional: Selects coverage for a region, which provides a higher resolution. Combined: Combines CONUS and regional coverages. Or: Selects type of NEXRAD coverage when SiriusXM is the selected data link source: COMP: Displays composite reflectivity image. Base: Displays base reflectivity image. Pilot’s Guide for the Cirrus SR2x with Cirrus Perspective Touch+ by Garmin 190-02955-01 Rev. A 30 SYSTEM OVERVIEW SYSTEM OVERVIEW FLIGHT INSTRUMENTS EAS AUDIO & CNS FLIGHT MANAGEMENT HAZARD AVOIDANCE AFCS ADDITIONAL FEATURES APPENDICES INDEX Level 1 Level 2 Level 3 Level 4 Description Storm Cell Movement Adds or removes the display of storm cell movement information on the PFD Map (only available when SiriusXM is selected as the data link weather source). The softkey annunciator is green when the function is on. When the function is off, the annunciator is subdued. NEXRAD Animation Adds or removes the display of NEXRAD animation on the Inset Map (only available when SiriusXM is selected as the data link weather source). NEXRAD animation is not available for display on the HSI Map. The softkey annunciator is green when the function is on. When the function is off, the annunciator is subdued. WX Overlay Selects the display of weather information on the PFD Map based on the installation and configuration options. SiriusXM: Selects SiriusXM as the weather source for the display of weather data when SiriusXM is selected as the weather source using the Data Link Softkey. Connext: Selects Connext as the weather source for the display of weather data when Connext is selected as the weather source using the Data Link Softkey. FIS-B: Selects FIS-B as the weather source for the display of weather data when FIS-B is selected as the weather source using the Data Link Softkey. Off: Removes weather data from the Inset or HSI Map. Datalink Lightning Softkey is available when SiriusXM or Connext is selected as the weather source using the Data Link Softkey. Adds/removes the display of SiriusXM or Connext information on the PFD Map. The softkey annunciator is green when the lightning function is on. When the lightning function is off, the annunciator is gray. METAR Adds or removes the display of SiriusXM, Connext, or FIS-B sourced METAR data on the PFD Map. The softkey annunciator is green when the METAR data is enabled. When the METAR data is off, the annunciator is gray. Traffic Map Replaces the PFD Map with a dedicated traffic display. The softkey annunciator is green when the dedicated traffic display is on. When the PFD Map is on, the softkey annunciator is gray. PFD Settings Displays the PFD settings softkeys. SVT Mode Displays the Synthetic Vision Technology (SVT) settings softkeys

Type certificate, explained

What's in the Cirrus SR22T G7 TCDS

A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.

TCDS A00009CHRev 19· Issued 2013
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