Garmin gnc 300 사용자 설명서
GARMIN International, Inc.
9875 Widmer Road
Lenexa, KS 66215 U.S.A.
FAA APPROVED AIRPLANE FLIGHT MANUAL SUPPLEMENT
GARMIN GNC300 VHF COMMUNICATION TRANSCEIVER / GPS RECEIVER
190-00067-03 Rev. A
FAA APPROVED
Page 16 of 16
DATE: 10/16/95
5. AUTOPILOT / FLIGHT DIRECTOR OPERATION
Coupling of the GNC300 System steering information to the autopilot/flight
director can be accomplished by engaging the autopilot/flight director in the
NAV or APR mode, with the NAV / GPS switch set to GPS.
director can be accomplished by engaging the autopilot/flight director in the
NAV or APR mode, with the NAV / GPS switch set to GPS.
When the autopilot/flight director system is using course information supplied
by the GNC300 System and the course pointer is not automatically driven to the
desired track, the course pointer on the HSI must be manually set to the desired
track (DTK) indicated by the GNC300. For detailed autopilot/flight director
operational instructions, refer to the FAA Approved Flight Manual Supplement
for the autopilot/flight director.
by the GNC300 System and the course pointer is not automatically driven to the
desired track, the course pointer on the HSI must be manually set to the desired
track (DTK) indicated by the GNC300. For detailed autopilot/flight director
operational instructions, refer to the FAA Approved Flight Manual Supplement
for the autopilot/flight director.
NOTE: When the autopilot/flight director is using data
supplied by the GNC300 and the GNC300 is in Route
mode, the course pointer must be reset to the new desired
track (DTK) at each route leg change.
supplied by the GNC300 and the GNC300 is in Route
mode, the course pointer must be reset to the new desired
track (DTK) at each route leg change.
SECTION V
PERFORMANCE
No change.
SECTION VI
WEIGHT AND BALANCE
See current weight and balance data.
SECTION VII
AIRPLANE & SYSTEM DESCRIPTIONS
See GNC300 Pilot’s Guide for a complete description of the GNC300 system.