Tecnam P2010 - Stall Warning

AFMS N°D03 FOR ALTERNATIVE AVIONICS CONFIGURATION
Page 7G-21
Section 7 – Airframe and Systems description
ELECTRICAL SYSTEM
Ed. 1, Rev. 0
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.