Explain the relevance of the Critical Angle of Attack.
Explain the effects of the following factors:
Weight variations
Power variations
Flap extension
Recall from memory the airborne HASELL checks.
Recall indications of slow speed flight.
From memory, list the actions that must be taken by the pilot in the event of a stall.
Demonstrate an awareness and eagerness to identify possible threats to the safe outcome of the flight.
In the lift formula, L = Cl * 0.5 * rho * V^2 * S
, the stalling component is 0.5 * rho * V^2
.
A stall is induced by exceeding the Critical Angle of Attack.
Since there is no instrument to measure AoA, manufacturers provide a stall speed (Vs).
Vs assumes the aircraft is configured:
Maximum Take Off Weight (MTOW)
Idle Power
Load Factor = 1
Zero Flap
Most Forward CoG
Sometimes Vs1 is given. Stall speed in landing configuration:
Full flap
Gear down
Bottom of green arc ~ stall speed with no flap.
Bottom of white arc ~ stall speed with flap.
Reduction in weight.
Load Factor change.
Effect of Power.
Effect of Flap.
Use of aileron.
New Stall Speed = Old Stall Speed * (Load Factor ^ 0.5)
60 degree AoB ~ 2g
Therefore, 45 degree AoB ~ 1.41g
Example question
An aircraft with flying stall speed of 62KIAS performs a 60 degree turn.
What is the new stall speed?
Do not use aileron in a stall, approximately < 60KIAS until airspeed recovers.
Causes wingdrop and possible spin.
Factor | Variation | Result on Stall Speed |
---|---|---|
Weight | increase | increase |
Weight | decrease | decrease |
Load Factor | increase | increase |
Power | increase | decrease |
Flap | extension | decrease |
Leading Edge Ice | wing shape change | increase |
Bird Strike | wing damage | increase |
Hoar Frost | boundary layer | increase |
Height: Must recover by 3000AGL
Airframe: Configured (flap up)
Security: No loose objects, hatches and harness secure
Engine: Pressures and temps checked
Location: Not over built-up areas
Lookout: 360 degree clearing turn before commencing and 90 degree between each stall
Slow and decaying airspeed
Nose-high attitude
Less wind noise
Controls less responsive
Stall warning (5-8KIAS above Critical AoA)
Control buffet
Lower nose if warnings of impending stall
loss of height (guaranteed)
nose drop (maybe)
wing drop (maybe)
Lower nose to level
Add full power
Right rudder
After sufficient airspeed, raise nose slightly
Lowering nose too far (do not exceed loss of > 100ft altitude)
Delayed application of full power
Pull up too quickly after recovery -> secondary stall
at lower power setting, carb heat
at stall warning, carb heat off
HASELL check
Symptoms of impending stall
Symptoms of developed stall
Recovery of impending stall
Recovery of developed stall