AFMS N°D01 FOR GARMIN GFC700 AUTOPILOT INSTALLATION AND
RNAV/RNP NAVIGATION ELIGIBILITY
Section 7 – Airframe and Systems description
ELECTRICAL SYSTEM
FIG.7-15. ELECTRICAL SYSTEM ARCHITECTURE
12.3 STALL WARNING SYSTEM
The aircraft is equipped with a stall warning system consisting of a sensor locat-
ed on the right wing leading edge connected to a warning horn located near the
instrument panel.
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