Flight planning and performance

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The speed V1 is defined as:

The speed V2 is defined for jet aircraft as:

Which of the following is true with regards to VMCA (air minimum cruise speed)?

The minimum value of V2 must exceed VMC by:

VEF= Critical engine failure speed

VMCG= Ground minimum control speed

VMCA= Air minimum control speed

VMU= Minimum unstick speed

V1= Take-off decision speed

VR= Rotation speed

V2 min.= Minimum take-off safety speed

The correct formula is:

The take-off decision speed V1 is:

The induced drag of an aeroplane at constant gross weight and altitude is highest at

The speed VS is defined as

The stalling speed or the minimum steady flight speed at which the aeroplane is controllable in landing configuration is abbreviated as

The speed V1 is defined as

The speed for best rate of climb is called

Which of the following statements is correct?

The speed V2 is

Maximum and minimum values of V1 are limited by :

Which of the following will decrease V1?

In case of an engine failure recognized below V1

In case of an engine failure which is recognized at or above V1

V2 has to be equal to or higher than

The lowest take-off safety speed (V2 min) is:

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