Aircraft General Knowledge Flashcards

Practice exam cards to test your AGK knowledge

1
Q

The battery switch in an aircraft electrical system is used to …

A

connect the battery to the electrical system

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2
Q

When the inlet valve is closed after BDC in a 4-stroke engine, the maximum quantity of fuel/air change entering the cylinder is ensured. The modification to the valve timing is know as …

A

valve lag

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3
Q

The function of a restrictor valve in an aircraft hydraulic system is …

A

reduce the speed of operation of a hydraulic unit

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4
Q

An IVSI differs from a conventional VSI in that it has …

A

an inertial accelerometer to assist initial indication of climb or descent

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5
Q

A directional gyro (DG) suffers from the errors of …

A

precession and instrument error

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6
Q

A remote magnetic indicator (RMI) has …

A

a remote sensor to improve accuracy

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7
Q

Connecting aircraft batteries in parallel results in …

A

increased amp/hours

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8
Q

If the gas pressure is too low in a hydraulic accumulator you would expect …

A

reduction in emergency power and slower operation of some units

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9
Q

If the manual clutch in a conventional helicopter rotor/transmission system is disengaged during powered forward flight …

A

the helicopter rotor system will lose power, RRPM will decay, the aircraft nose will yaw left and the engine may over speed.

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10
Q

Fluctuating fuel pressure gauge indications on a normally carburetted engine indicate …

A

vapor lock in the system

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11
Q

Fuel tank vents should be inspected before flight because …

A

a blockage in the vent can interrupt the fuel supply to the engine

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12
Q

The reading of a manifold pressure gauge on an inoperative engine at 2000 ft AMSL would be approximately (assume ISA) …

A

28 inches Hg

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13
Q

An engine with a combustion chamber of 13 cubic inches capacity and a swept volume of 78 cubic inches has a compression ratio of …

A

7 to 1

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14
Q

A pressure relief valve fitted to an aircraft hydraulic system is designed to …

A

protect the system from excessive pressure in the event of a pressure regulator failure

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15
Q

De-icing mats on rotor blades should be activated …

A

after ice has formed

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16
Q

An unusually high CHT in cruise could cause …

A

detonation or pre-ignition

17
Q

The effect of a blocked static vent during a descent would be …

A

over reading ASI

18
Q

The purpose of a freewheeling unit is to disconnect the …

A

rotor system when the engine RPM slows below the equivalent RRPM

19
Q

Operating an engine at idle power with the mixture very rich can cause …

A

high EGT

20
Q

An aircrafts actual heading will be behind the compass indication when turning …

A

onto north in the southern hemisphere