1. At the first indication
of a stall, the pitch attitude and angle of attack must be decreased
positively and immediately. Since the basic cause of a stall is
always an excessive angle of attack, the cause must first be eliminated
by releasing the back elevator pressure, or by moving the elevator
2. The maximum allowable power should be
applied to increase the airplane's speed and assist in reducing
the wing's angle of attack. Generally, the throttle should be promptly,
but smoothly, advanced to the maximum allowable position. Although
stall recoveries should be practiced withoutas well as withthe
use of power, in most actual stalls, the application of more power
is an integral part of the stall recovery. Usually, the greater
the power applied, the lower the loss of altitude.
3. Regain straight and level flight, with
coordinated use of all controls.