AFMS N°D07 FOR GARMIN GFC700 AUTOPILOT AND VARIABLE PITCH PROPELLER EQUIPPED
AEROPLANES
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 located
on the right wing leading edge connected to a warning horn located near the instru-
ment panel.
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