2 Flashcards

1
Q

The primary purpose of a supercritical wing section is to:

A

Increase the critical drag rise number

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2
Q

Coffin Corner is best described, as the situation where an aircraft is operating at such high altitude that the difference between high and low speed buffet is only a few knots. Is it affected by weight and load factors?

A

It is effected by aircraft weight and load factors

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3
Q

The term ‘Fail Passive’ of the autopilot system is used to describe:

A

An autopilot system comprising 2 autopilots and should one fail both will be disconnected leaving the aircraft in a passive state of trim. The aircraft must then be flown manually.

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4
Q

How would you describe the Diffuser in the exhaust section of a gas turbine engine:

A

It is a divergent duct increasing gas stream pressure and decreasing gas stream velocity

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5
Q

What is the purpose of the Shuttle Valve in the hydraulic system of a transport category aircraft?

A

To allow hydraulic pressure from the alternate system to automatically pressurise the lines in the event of a failure of the normal system

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6
Q

Which of the following components of a hydraulic system in a transport category aircraft acts as a surge suppressor:

A

The accumulator

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7
Q

In a pure turbojet, compared to a high by pass turbofan of the same thrust output, the rear (LP) turbine wheels are -

A

Smaller and rotate faster

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8
Q

Which of the answers listed below best represents the display of active waypoints and active routes?

A

Active waypoints are displayed in magenta and tracks as solid magenta lines

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9
Q

The freezing point of Jet-A1 fuel is closest to:

A

Minus 50 degrees

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10
Q

An aircraft flies above its mach trim speed, the mach trim system will:

A

Deflect the leading edge of the horizontal stabilator downwards

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11
Q

The effect of a centre of gravity (CoG) position on the cruise speed of an aircraft for a given thrust setting and weight in level flight is:

A

A rearward CoG (within limits) results in a higher cruise speed

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12
Q

Gas turbine engine mass air flow is governed primarily by

A

the RPM, the airspeed and the air density

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13
Q

An advantage of NICAD batteries in an aircraft installation compared to lead acid batteries is

A

Faster recharge cycle

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14
Q

The component of the autopilot system which safeguards against a servomotor runaway is

A

the torque limiter

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15
Q

The function of the follow up linkage in the nose wheel landing gear system of a jet transport category aircraft is

A

to hold the nose wheel steering at the correct angle

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