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You are here: home->ama->N01->N.8.6.0.6.A.1

8606
The operation of an angle of attack indicating system is based on detection of differential pressure at a point where the airstream flows in a direction
A) not parallel to the true angle of attack of the aircraft.
B) parallel to the longitudinal axis of the aircraft.
C) parallel to the angle of attack of the aircraft.

 

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