Sample Airplane Flight Manual Supplement for the 190-01810-13, Rev. 1

This aircraft is equipped with a GDL 82 with the following interfaces / features: Equipment Installed: GDL 82 Unit:  GDL 82 (external GPS/SBAS source with Time Mark required)  GDL 82 w/ Internal GPS/SBAS Companion Mode A/C Transponder: Make: ______________________________________________________ Model: _____________________________________________________ NOTE The installed and combined GDL 82 and Mode A/C transponder system shall continue to meet the requirements of 14 CFR §91.413(b) and the performance required by 14 CFR §43, Appendix E, pgh. (c) and Appendix F. Interfaced GPS/SBAS Position Source: The GDL 82 requires a GPS/SBAS position source and is noted below.  Internal – or – External GPS/SBAS source (select one):  GTN 6XX/7XX Series  GNS 400W/500W Series  GNS 480 Sample Airplane Flight Manual Supplement for the 190-01810-13, Rev. 1 Garmin GDL 82 FAA APPROVED Page 7 of 12 1.5 Definitions The following terminology is used within this document: ADS-B: Automatic Dependent Surveillance-Broadcast AFM: Airplane Flight Manual AFMS: Airplane Flight Manual Supplement AIM: Aeronautical Information Manual CFR: Code of Federal Regulations GDL: Garmin Data Link GNS: Garmin Navigation System GPS: Global Positioning System GTN: Garmin Touchscreen Navigator ICAO: International Civil Aviation Organization POH: Pilot Operating Handbook SBAS: Satellite-Based Augmentation System SW: Software UAT: Universal Access Transceiver VFR: Visual Flight Rules Sample Airplane Flight Manual Supplement for the 190-01810-13, Rev. 1 Garmin GDL 82 Page 8 of 12 FAA APPROVED Section 2. LIMITATIONS 2.1 Required Equipment The GDL 82 must have the following system interfaces fully functional to be compliant with the requirements for 14 CFR §91.227 ADS-B Out operations: Interfaced Equipment Number Installed Number Required Mode A/C Transponder 1 1 GPS/SBAS Position Source 1 1 Table 1 – Required Equipment 2.2 ADS-B OUT The GDL 82 will only comply with 14 CFR §91.227 for ADS-B OUT when all the above required equipment are operational. If the optional ADS-B OUT FAIL annunciator is installed, it will illuminate when the GDL 82 is not transmitting a valid or complete ADS-B OUT message. 2.3 Maximum Operating Altitude In accordance with 14 CFR §91.225, aircraft with ADS-B Out UAT equipment, operating on 978 MHz and meeting the requirements in TSO-C154c, are limited to operations below 18,000 feet MSL. Aircraft Operational Ceiling:  18,000 feet (UAT Operating Altitude Limit per AC 20-165B)  15,000 feet (Class B Transponder Equipment Operating Altitude Limit per 14 CFR Part 91.413) Sample Airplane Flight Manual Supplement for the 190-01810-13, Rev. 1 Garmin GDL 82 FAA APPROVED Page 9 of 12 2.4 Anonymous Mode Operation (if installed) In the event the GDL 82 is installed with an ADS-B In device (e.g., GDL 39), when the GDL 82 anonymous mode is initially enabled, the ADS-B In receiver may detect the aircraft’s registration number change as a nuisance ownship shadow and report a traffic alert (TA) at the aircraft’s location and altitude. This is due to the aircraft’s identification changing from the known registration number to “VFR” and a temporary address. It is not recommended to enable the anonymous mode during flight. To enable the anonymous mode, it must be activated on-ground to avoid receiving an ownship- shadow TA. Anonymous Mode Switch Installed:  YES (comply with anonymous mode operation limitations in AFMS)  NO Sample Airplane Flight Manual Supplement for the 190-01810-13, Rev. 1 Garmin GDL 82 Page 10 of 12 FAA APPROVED Section 3. EMERGENCY PROCEDURES 3.1 Emergency Procedures No Change. 3.2 Abnormal Procedures 3.2.1 LOSS OF AIRCRAFT ELECTRICAL POWER GENERATION When the aircraft electrical charging system becomes inoperative or degraded, avionics will continue to operate for a limited time using aircraft battery power. The pilot should become familiar with electrical load-shedding methods and equipment requirements for the various phases of flight. If an electrical emergency exists or the aircraft’s charging system is compromised, the pilot should consider turning off the GDL 82 to preserve the operation of more essential avionics when using only battery power. Subject to aircraft equipment electrical load-shedding priorities, XPDR UAT Circuit Breaker Position ............................................... CONSIDER NOTE Pulling the XPDR UAT circuit breaker will turn off both the GDL 82 and the companion transponder. ADS-B OUT UAT and transponder functions will no longer be available. Also, without power, the GDL 82’s ADS-B OUT FAIL annunciator will not illuminate. This guidance is supplementary to any guidance provided in the Pilot’s Operating Handbook (POH) for the _______________ aircraft for loss of power generation. 3.2.2 LOSS OF GPS/SBAS POSITION DATA When the configured GPS/SBAS receiver is inoperative or GPS position information is not available or invalid, the GDL 82’s ADS-B OUT FAIL annunciator will illuminate. In this case, though the GDL 82 will continue to transmit ADS-B OUT UAT data without a valid GPS position, the ADS-B OUT message is neither complete nor compliant. ADS-B OUT FAIL Annunciator (if installed)………………ILLUMINATED For GDL 82 installations that use an external GPS position source: Interfaced GPS position source................................................ VERIFY GPS POSITION SOURCE IS ON AND FUNCTIONING PROPERLY WITH A VALID POSITION Sample Airplane Flight Manual Supplement for the 190-01810-13, Rev. 1 Garmin GDL 82 FAA APPROVED Page 11 of 12 Section 4. NORMAL PROCEDURES The GDL 82 requires no pilot intervention or control for normal operation. The GDL 82 is powered on with avionics and will automatically begin to operate once the configured Mode A/C transponder is set to ALT and a GPS/SBAS position is available. The pilot may select the Anonymous Mode if the optional Anonymous Mode switch is installed and the transponder code is set to “1200”. 4.1 GDL 82 Unit Power On Avionics Master ............................................................................................... ON Transponder ................................................................................... Code set, ALT Anonymous mode switch (if installed) ........................................... AS DESIRED ADS-B OUT FAIL annunciation (if installed) ........................ EXTINGUISHED NOTE AIM 4-1-20 a. 3. encourages pilots to operate with the transponder in the altitude reporting mode and ADS-B Out transmissions enabled (if equipped) at all airports, any time the aircraft is positioned on any portion of an airport movement area. If the ADS-B OUT FAIL annunciator is installed, it may illuminate momentarily as the unit powers on and begins to receive input from external systems, including the GPS/SBAS position source. Ensure lamp is operational prior to flight by pressing- to-test. The configured Mode A/C transponder must be set to ALT and the optional ADS-B OUT FAIL annunciation must be EXTINGUISHED for the system to meet the requirements specified in 14 CFR §91.227. This system must be operational in certain airspaces after January 1, 2020 as specified by 14 CFR §91.225. Sample Airplane Flight Manual Supplement for the 190-01810-13, Rev. 1 Garmin GDL 82 Page 12 of 12 FAA APPROVED Section 5. PERFORMANCE No change. Section 6. WEIGHT AND BALANCE See current weight and balance data. Section 7. SYSTEM DESCRIPTION The Garmin GDL 82 Quick Reference Pilot’s Guide, part numbers, and revisions listed below contain additional information regarding GDL 82’s system description, function, and optional control and annunciation. Title Part Number Revision GDL 82 Quick Reference Pilot’s Guide 190-01810-03 Rev. 1 (or later) Pilot’s Guides for interfaced external GPS/SBAS sources, part numbers and revisions listed below, provide additional operating information for the Garmin GPS Navigators. Title Part Number Revision Garmin GTN 725/750 Pilot’s Guide 190-01007-03 Rev. E (or later) Garmin GTN 625/635/650 Pilot’s Guide 190-01004-03 Rev. E (or later) Garmin GNS 400W Pilot’s Guide & Reference 190-00356-00 Rev. K (or later) Garmin GNS 500W Pilot’s Guide & Reference 190-00357-00 Rev. K (or later) GNS 480 Pilot’s Guide 190-00502-00 Rev. D (or later)