AMC 25.201(a)(2) Stall demonstration

• ED Decision 2003/2/RM found in: CS-25 Amdt 27 - Large Aeroplanes (Jan 2023)

AMC 25.201(a)(2) Stall demonstration ED Decision 2003/2/RM The power for all power-on stall demonstrations is that power necessary to maintain level flight at a speed of 1·5 VSR1 at maximum landing weight, with flaps in the approach position and landing gear retracted, where VSR1 is the reference stall speed in the same conditions (except power). The flap position to be used to determine this power setting is that position in which the reference stall speed does not exceed 110% of the reference stall speed with the flaps in the most extended landing position.