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The lift force always:
In a descend without power (engine failure) with a heavier aircraft than normal:
Positive directional stability is achieved by:
Positive longitudinal stability is achieved by a:
Vx (best angle of climb) is achieved at the speed of:
Vy (best rate of climb) is achieved at the speed of:
In a climb a headwind will affect:
Positive lateral stability is achieved by:
Service ceiling is when an aircraft:
Flying with a higher airspeed than normal in straight and level flight will give a:
Stability in the rolling plane is called:
Lowering flaps will:
If the Angle of Attack is increased on the elevator, the aircrafts nose will:
The slipstream from the propeller will increase the effectiveness of:
An increase in airspeed will:
To stop adverse aileron yaw:
The further effect of aileron is:
The secondary effect of rudder is:
Lift is generated through:
An aircraft rolls about which axis?