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The stalling speed of an aeroplane is increased by an increase in

IAS

Angle of attack

Lift

Load factor

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If other conditions remain the same, what effect will an increase in surface air temperature have on take-off distance required?

Distance required is unchanged

Distance required is unchanged but take-off roll is increased

Distance required decreases

Distance required increases

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An aeroplane has a straight and level stall speed of 60kt. If the 'apparent' weight is increased by 50% i.e. the load factor is increased by 50%, the new stall speed will be ____kt

58± 2

83± 2

94± 2

72 ± 2

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Consider the turn performance of two aeroplanes with different gross weights. If they both execute turns at the same IAS, altitude, and bank, the heavier aeroplane will have:

A greater turn rate than the lighter aeroplane

A greater turn radius than the lighter aeroplane

A lower turn rate and greater turn radius than the lighter aeroplane

The same turn rate and radius as the lighter aeroplane

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