ilk 30 Flashcards

1
Q

For a piston engine aeroplane, the speed for maximum range is:

A

that which gives the maximum lift to drag ratio.

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2
Q

Which of the following statements is correct ?

A

A stopway means an area beyond the take-off runway, able to support the aeroplane during an aborted take-off.

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3
Q

During take-off the third segment begins:

A

when acceleration to flap retraction speed is started.

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4
Q

Which of the following is true with regard to VMCA (air minimum control speed)?

A

Straight flight can not be maintained below VMCA, when the critical engine has failed.

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5
Q

Which of the following will decrease V1 ?

A

Inoperative anti-skid.

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6
Q

Which of the following are to be taken into account for the runway in use for take-off ?

A

Airport elevation, runway slope, outside air temperature, pressure altitude and wind components.

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7
Q

Changing the take-off flap setting from flap 15° to flap 5° will normally result in:

A

a longer take-off distance and a better climb.

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8
Q

In accordance with JAR-25, the reference landing speed (VREF) has the following minimum margin above the reference stalling speed in the landing configuration (VSR0):

A

23%

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9
Q

In relation to the net take-off flight path, the required 35 ft vertical distance to clear all obstacles is:

A

the minimum vertical distance between the lowest part of the aeroplane and all obstacles within the obstacle domain.

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10
Q

Considering the take-off decision speed V1 , which of the following is correct?

A

If an engine failure is recognized before reaching V1 , the take-off must be aborted.

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11
Q

What will be the effect on an aeroplane’s performance if aerodrome pressure altitude is decreased?

A

It will decrease the take-off distance required.

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12
Q

If the aerodrome pressure altitude increases it will:

A

increase the take-off distance.

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13
Q

Minimum control speed on the ground, VMCG , is based on directional control being maintained by:

A

primary aerodynamic control only.

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14
Q

Which of the following distances will increase if you increase V1 , but VR remains unchanged?

A

Accelerate Stop Distance

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15
Q

Which of the following answers is true?

A

V1 is lower or equal to VR

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16
Q

The length of a clearway may be included in:

A

the take-off distance available.

17
Q

How does runway slope affect allowable take-off mass, assuming other factors remain constant and not limiting?

A

A downhill slope increases allowable take-off mass.

18
Q

The effect of increasing the flap setting, from zero to the recommended take-off setting, on the length of the Take-off Distance Required (TODR) and the Field-Length-Limited Take-off mass (TOM) is:

A

Decreased TOD required and increased field length limited TOM.

19
Q

How is VMCA influenced by increasing pressure altitude?

A

VMCA decreases with increasing pressure altitude.

20
Q

Which one of the following is not affected by a tail wind?

A

the climb limited take-off mass.

21
Q

Considering VR, which statement is correct?

A

VR is the speed at which rotation should be initiated.

22
Q

Which statement is correct?

A

VR must not be less than 1.05 VMCA and not less than V1.

23
Q

Which of the following represents the minimum for V1 ?

24
Q

In the event of engine failure below V1 , the first action to be taken by the pilot in order to decelerate the aeroplane is to:

A

reduce the engine thrust.

25
Q

If the antiskid system is inoperative, which of the following statements is true?

A

The accelerate stop distance increases.

26
Q

In which of the following distances can the length of a stopway be included?

A

In the accelerate stop distance available.

27
Q

Other factors remaining constant and not limiting, how does increasing pressure altitude affect allowable take-off mass?

A

Allowable take-off mass decreases.

28
Q

If there is a tail wind, the climb limited TOM will:

A

not be affected.

29
Q

Which of the following sets of factors will increase the climb-limited TOM (every factor considered independently)?

A

Low flap setting, low PA, low OAT.

30
Q

The requirements with regard to take-off flight path and the climb segments are only specified for:

A

the failure of the critical engine on a multi-engines aeroplane.