AFMS N° D08 FOR ALTERNATIVE AVIONICS CONFIGRATION AND
VARIABLE PITCH PROPELLER EQUIPPED AIRPLANES
Page GV 7-21
FIG.7-15. ELECTRICAL SYSTEM ARCHITECTURE
9.1 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.
Section 7 – Airframe and Systems description
ELECTRICAL SYSTEM
Ed. 1, Rev. 0
To Next Page
Loading...
