How does the centre of pressure move as the angle of attack is increased?
The centre of pressure moves towards the leading edge with an increase in angle of attack
What is a stall?
When the aerofoil has exceeded its critical angle of attack and can no longer produce enough lift to balance weight
An aircraft can stall regardless of:
Regardless of airspeed and attitude
What are the stall speeds for the C172N? (flaps and clean)
Clean: 47kts
With flaps: 41kts
How does the stagnation point move as the AoA increases?
The stagnation point moves along the bottom of the aerofoil closer to the trailing edge
How does the force of lift change in a stall?
In a stall lift moves aft of the CoG and decreases in magnitude
How does an increase in weight affect stall speed?
Increases stall speed
How does a decrease in weight affect stall speed?
Stall speed decreases
How is stall speed affected as the CoG moves aft?
the stall speed decreases
How does an increase in power affect stall speed?
Reduces stall speed
How does flap extension affect stall speed?
Reduces stall speed
How does an increase in load factor affect stall speed?
Increases stall speed
What is the HASELL check?
MUST BE DONE BEFORE GOING INTO A STALL
Height - make sure you can recover by 3000’ AGL
Airframe configured - clean
Security - no loose articles
Engine T’s and P’s in the green
Location - clear of high traffic areas
Lookout - 180* turn or two 90* turns
What are the symptoms of an incipient stall?
These can occur in any order and may or may not be present
(RSLURP)
Reduced cockpit noise level
Stall warning
Low and decreasing airspeed
Unusually high nose attitude
Reduced control effectiveness
Possible buffeting on the tail
What are the symptoms of a full developed stall?
(HAWN)
High rate of descent
Aircraft highly unstable
Wing drop possibly
Nose drop
How do you recovery from an incipient stall?
Lower the nose attitude
apply power
How do you recover from a fully developed stall?
Carby heat cold
simultaneously release back pressure and introduce power
at 65kt, first stage of flaps up
at 70kt, raise nose to Vy
Once positive rate of climb established, retract another stage of flaps
retain target altitude
How do you enter a stall in approach configuration?
carby heat on
1500RPM
speed checked below 100kt first stage of flaps
below 85kt, second stage of flaps
reduce power to idle
increase back pressure to maintain level
What is the recovery from a spin?
PARE
Power idle
Aileron neutral
Rudder full opposite
Elevator through neutral
Once rotation has stopped:
centralise rudder
dive recovery
power above the horizon