Garmin GTN 650 STC GTN 6XX/7XX AFMS - Page 25

GARMIN Ltd. or its Subsidiaries, c/o Garmin International 1200 E. 151st Street Olathe, KS 66062 USA AIRPLANE FLIGHT MANUAL SUPPLEMENT or SUPPLEMENTAL AIRPLANE FLIGHT MANUAL for STC SA02019SE-D GARMIN GTN NAVIGATION SYSTEM Section 4. NORMAL PROCEDURES Refer to the Cockpit Reference Guide defined in Section 2.1 of this document or the Pilot's Guide defined in Section 7.1 for normal operating procedures and a complete list of system messages and associated pilot actions. This includes all GPS operations, VHF communication and navigation, traffic, data linked weather, StormScope®, TAWS, and Multi-Function Display information. The GTN requires a reasonable degree of familiarity to prevent operations without becoming too engrossed at the expense of basic instrument flying in IMC and basic see-and-avoid in VMC. Garmin provides training tools with the Pilot's Guide and PC based simulator. Pilots should take full advantage of these training tools to enhance system familiarization. 4.1 Unit Power On Database REVIEW EFFECTIVE DATES Self Test VERIFY OUTPUTS TO NAV INDICATORS Self Test - TAWS Remote Annunciator: PULL UP ILLUMINATED TERR ILLUMINATED TERR N/A ILLUMINATED TERR INHB ILLUMINATED Self Test - GPS Remote Annunciator: VLOC ILLUMINATED GPS ILLUMINATED LOI or INTG ILLUMINATED TERM ILLUMINATED WPT ILLUMINATED APR ILLUMINATED MSG ILLUMINATED SUSP or OBS ILLUMINATED 4.2 Before Takeoff System Messages and Annunciators CONSIDERED 4.3 HSI and EHSI Operation If an HSI is used to display navigation data from the GTN the pilot should rotate the course pointer as prompted on the GTN. If an EHSI is used to display navigation data from the GTN the course pointer may autoslew to the correct course when using GPS navigation. When using 190-01007-A2 Rev. 1 FAA APPROVED DATE: _M__A_R_C_H__1_8__,_2_0_1_1__ Page 25 of 31