Only when the aircraft is using high power settings

Whenever the aircraft is producing lift

Only when the aircraft is heavily loaded

Only when the aircraft is operating at high speeds

41%

100%

None

Slight increase

2.

1.

Dependant on the weight.

Dependant on the airspeed.

70 kt

50 kt

45 kt

60 kt

The stalling speed remains the same in the turn as when the wings are level

The stalling speed increases because the flaps are lowered

The stalling speed decreases in the turn

The stalling speed increases because of the increased load factor in the turn

Angle of attack, weight and air density

Weight, load factor and power

Load factor, angle of attack and power.

Weight, density altitude, power and turbulence

Lift increases but drag remains constant

Lift will increase and drag will increase

Lift and drag will vary depending on speed

Lift will suddenly decrease and drag will increase

Is a function of the altitude

Depends upon the airspeed over the wings

Is greater when flying into wind compared with flying downwind

Remains constant regardless of gross weight

Actual weight to ‘g’ force or gravity

Apparent weight to lift

Lift over weight

Weight over lift