14 Flashcards

1
Q

The effect of a VR overspeed on lift off speed and distance and second segment climb gradient is:

A

Increase increase increase.

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2
Q

The C of G is near its forward envelope limit. Which statement is most correct?

A

Greater elevator force is required to change the pitch attitude than with an aft C of G position.

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3
Q

An excessively aft C of G when on approach to land will cause?

A

Light elevator control forces, and decreased pitch stability

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4
Q

A number of swept wing jet transport aircraft have a limitation such that flap extension at high altitudes (typically above FL200) is prohibited. This is because?

A

The high IAS at such altitude can exceed that of the flap restricting Mach number.

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5
Q

As the speed of a large jet aircraft increases from a stall speed up to cruise speed, the power required to fly straight and level will:

A

Decrease and then increase.

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6
Q

You are about to descend through cloud containing heavy freezing rain.
The best descent configuration to minimise the risk of airframe ice in these conditions is -

A

engine RPM up slightly and speedbrakes out

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7
Q

Concerning electrical windshield heating

A

the window may appear tinted when viewed with reflected light

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8
Q

In comparison to an unswept wing, a swept wing will have a -

A

lower MAX CL at subsonic and supersonic speeds

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9
Q

A variable incidence tail-plane with stabiliser trim, as an alternative to a conventional elevator with trim -

A

can produce excessively high control forces if out of trim

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10
Q

The auto pilot depends on devices to measure aircraft attitude changes so that information may be used to achieve controlled flight. Accelerometers assist in a -

A

set rate of climb and descent

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11
Q

The device that controls the direction of movement of a hydraulic actuating unit, is called the

A

Selector valve

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12
Q

Assuming the same degree of trailing edge flap deflection, which answer best describes the primary advantage of slotted flaps, compared to fowler flaps ?

A

Improved boundary layer airflow over flaps.

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