Garmin GTN 650 STC GTN 6XX/7XX AFMS - Page 12

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 2.3 Minimum Equipment If the installation of the GTN is not limited to VFR, the GTN must have the following system interfaces fully functional in order to be used for IFR operations: Interfaced Equipment Number installed External HSI/CDI/EHSI 1 or more External GPS Annunciator See Note 1 Table 1 - Required Equipment Number Required for IFR 1 1 Note 1: Certain installations require an external GPS annunciator panel. If installed, this annunciator must be fully functional to use the GTN for IFR operations. Single engine piston aircraft under 6,000 lbs maximum takeoff weight: Required Equipment for IFR operations: Single GTN Navigator Single engine turbine aircraft or multi-engine piston aircraft under 6,000 lbs maximum takeoff weight: Required Equipment for IFR operations: Single GTN Navigator plus a second source of GPS navigation or a separate source of VHF navigation. Operation in remote or oceanic operation requires two sources of GPS navigation. Aircraft over 6,000 lbs maximum takeoff weight: Required Equipment for IFR operations: Single GTN Navigator plus a second source of GPS navigation or a separate source of VHF navigation. Operation in remote or oceanic operation requires two sources of GPS navigation. 190-01007-A2 Rev. 1 FAA APPROVED DATE: _M__A_R_C_H__1_8__,_2_0_1_1__ Page 12 of 31