MARCH 18, 2011GARMIN Ltd. or its Subsidiaries, c/oGarmin International 1200 E. 151st StreetOlathe, KS 66062 USAAIRPLANE FLIGHT MANUAL SUPPLEMENT orSUPPLEMENTAL AIRPLANE FLIGHT MANUALfor STC SA02019SE-D GARMIN GTNNAVIGATION SYSTEM190-01007-A2 Rev. 1 Page 8 of 31FAA APPROVED DATE: _________________The Garmin GNSS navigation system, as installed in this aircraft, complies withthe accuracy, integrity, and continuity of function, and contains the minimumsystem functions required for P-RNAV operations in accordance with JAAAdministrative & Guidance Material Section One: General Part 3: TemporaryGuidance Leaflets, Leaflet No 10 (JAA TGL-10 Rev 1). The GNSS navigationsystem has [one or more] TSO-C146c Class 3 approved Garmin GTN NavigationSystems. The Garmin GNSS navigation system as installed in this aircraftcomplies with the equipment requirements for P-RNAV and B-RNAV/RNAV 5operations in accordance with AC 90-96A CHG 1 and JAA TGL-10 Rev 1. Thisdoes not constitute an operational approval.Garmin International holds an FAA Type 2 Letter of Acceptance (LOA) inaccordance with AC 20-153 for database integrity, quality, and databasemanagement practices for the Navigation database. Flight crew and operators canview the LOA status at FlyGarmin.com then select “Type 2 LOA Status.”Navigation information is referenced to WGS-84 reference system.Note that for some types of aircraft operation and for operation in non-U.S.airspace, separate operational approval(s) may be required in addition toequipment installation and airworthiness approval.1.3 Electronic Flight BagThe GTN as installed in this aircraft supports approval of AC 120-76A HardwareClass 3, Software Type C Electronic Flight Bag (EFB) electronic aeronauticalchart applications when using current FliteChart or ChartView data. Additionaloperational approvals may be required. For operations under 14 CFR Part 91,Garmin suggests that a secondary or back up source of aeronautical informationnecessary for the flight be available to the pilot in the airplane. The secondary orbackup information may be either traditional paper-based material or displayedelectronically. If the source of aeronautical information is in electronic format,operators must determine non-interference with the GTN system and existingaircraft systems for all flight phases.