Navigate / EASA

AMC 25.201(d) Stall demonstration

ED Decision 2018/005/R

1       The behaviour of the aeroplane includes the behaviour as affected by the normal functioning of any systems with which the aeroplane is equipped, including devices intended to alter the stalling characteristics of the aeroplane.

2       Unless the design of the automatic flight control system of the aeroplane protects against such an event, the stalling characteristics and adequacy of stall warning, when the aeroplane is stalled under the control of the automatic flight control system, should be investigated. (See also CS 25.1329(h).)

[Amdt 25/19]

[Amdt 25/21]