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 28 of 31FAA APPROVED DATE: _________________Section 5. PERFORMANCENo change.Section 6. WEIGHT AND BALANCESee current weight and balance data.Section 7. SYSTEM DESCRIPTIONS7.1 Pilot’s GuideThe Garmin GTN 6XX or GTN 7XX Pilot’s Guide, part number and revisionlisted below, contain additional information regarding GTN system description,control and function. The Pilot’s Guides do not need to be immediately availableto the flight crew.y GTN 6XX Pilot’s Guide P/N 190-01004-03 Rev A or latery GTN 7XX Pilot’s Guide P/N 190-01007-03 Rev A or later7.2 Leg SequencingThe GTN supports all ARINC 424 leg types. Certain leg types require altitudeinput in order to sequence (course to altitude, for example). If a barometriccorrected altitude source is not interfaced to the GTN, a popup will appearprompting the pilot to manually sequence the leg once the altitude prescribed inthe procedure is reached.
This installation has a barometric corrected altitude source. The GTN willautomatically sequence altitude legs.
This installation does not have a barometric corrected altitude source. Thepilot will be prompted to manually sequence altitude legs.’7.3 Auto ILS CDI CaptureAuto ILS CDI Capture will not automatically switch from GPS to VLOC forLOC-BC or VOR approaches.