13 Flashcards

1
Q

Primary control rate of climb is achieved through variations in:

A

Power of thrust

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2
Q

The compressor primarily converts:

A

Kinetic energy to pressure energy

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3
Q

The ‘ram ratio’ in a gas turbine engine is defined as the ratio of -

A

total pressure to static pressure at the air intake

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4
Q

Out of the items listed below, which is NOT an input to a modern Auto-throttle system?

A

ILS LOC

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5
Q

In which way do the “safety valves”, (also known as “Fluid Transfer Valves”) in the nose wheel steering system act in the event of total hydraulic failure?

A

Place the nose wheel into castor mode

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6
Q

An affect of extending slats on approach is to:

A

Increase the co-efficient of lift and re-energise chord-wise flow

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7
Q

The purpose of the water separator in an ACM air-conditioning unit is to:

A

Stop mist coming into cabin

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8
Q

The component of the autopilot system which monitors the gyro sensing signal and ensures that the correct attitude reference is being maintained is -

A

the feedback comparitor

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9
Q

For the B767 featuring 3 autopilot’s conducting a ‘FAIL OPERATIONAL’ auto-land ILS approach, after ‘bus isolation occurs’ the minimum number of separate electrical supply systems
required is:

A

2AC/1DC supply

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10
Q

The hydraulic reservoir in a jet aircraft hydraulic system is pressurised by bleed air to -

A

ensure a positive fluid supply to the pumps at all times

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11
Q

The stall speed of an aircraft at a particular gross weight will be highest with -

A

a forward centre of gravity

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12
Q

In the event of the nose-wheel steering failure, the safety valves will:

A

Allow nose wheel to swivel

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13
Q

The power response of a turbojet engine compared to a turboprop at various RPM settings is

A

slower at low RPM

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14
Q

In order to delay flow separation on an aerofoil at the stall, the characteristics of the boundary layer should ideally be -

A

turbulent due to the higher velocities at the wing surface

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15
Q

With regard to jet transport electrical systems

A

with a parallel bus system the generators are paralleled

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16
Q

With regard to the thrust output of a jet engine, the highest 30% of thrust is produced?

A

Above 90% RPM

17
Q

On a conventional Machmeter/ASI (MASI), a masked Mach speed display indicates that

A

the data from the CADC is unreliable