PPL » Aircraft Tech Knowledge (A) » Stalling and Spinning
12.68 Stalling and Spinning
12.68.2 Describe the stalling angle of attack, with reference to:
(a) disruption of streamline flow over the upper surface of the aerofoil;
(b) reduction of lift and increase of drag.
12.68.4 Describe the symptoms of a developing stall.
12.68.6 Explain how:
(a) the stall is associated with a particular angle of attack and not a particular airspeed;
(b) a reduction in angle of attack is critical to recovery.
12.68.8 Explain how the stalling IAS is affected by:
(a) load factor;
(b) aircraft weight;
(e) flap extension;
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