Garmin GTN 650 STC GTN 6XX/7XX AFMS - Page 28
Performance, Weight And Balance, System Descriptions, Pilot's
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GARMIN Ltd. or its Subsidiaries, c/o Garmin International 1200 E. 151st Street Olathe, KS 66062 USA Section 5. PERFORMANCE No change. AIRPLANE FLIGHT MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM Section 6. WEIGHT AND BALANCE See current weight and balance data. Section 7. SYSTEM DESCRIPTIONS 7.1 Pilot's Guide The Garmin GTN 6XX or GTN 7XX Pilot's Guide, part number and revision listed below, contain additional information regarding GTN system description, control and function. The Pilot's Guides do not need to be immediately available to the flight crew. y GTN 6XX Pilot's Guide y GTN 7XX Pilot's Guide P/N 190-01004-03 Rev A or later P/N 190-01007-03 Rev A or later 7.2 Leg Sequencing The GTN supports all ARINC 424 leg types. Certain leg types require altitude input in order to sequence (course to altitude, for example). If a barometric corrected altitude source is not interfaced to the GTN, a popup will appear prompting the pilot to manually sequence the leg once the altitude prescribed in the procedure is reached. This installation has a barometric corrected altitude source. The GTN will automatically sequence altitude legs. This installation does not have a barometric corrected altitude source. The pilot will be prompted to manually sequence altitude legs.' 7.3 Auto ILS CDI Capture Auto ILS CDI Capture will not automatically switch from GPS to VLOC for LOC-BC or VOR approaches. 190-01007-A2 Rev. 1 FAA APPROVED DATE: _M__A_R_C_H__1_8__,_2_0_1_1__ Page 28 of 31