A B C D E F G H I J K L M N O P Q R S T U V W X Y

Back to: "V"

vortilon
Fonte1
INTERNATIONAL CIVIL AVIATION ORGANIZATION. Aircraft accident digest n.32. Montreal, 1993. (Cir. 232 AN/139).
Contexto
Both angle of attack vanes (stall warning system lift transducers) were recovered but the right vane had separated from the wing and was damaged. A 9-foot piece of the left wing leading edge, from approximately the vortilon 18/ position to the outboard end, was intact.
Subárea
Aircraft Structure
Français
vortillon