CSYH Practice Cards 4 Flashcards

Random Questions/Statements for Exam Preparation

1
Q

The pressure exerted on the piston during the power stroke increases as the mass of charge induced …

A

increases and combustion temperature increases

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2
Q

As the throttle is moved towards the fully open position …

A

manifold pressure increases and mass flow increases

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3
Q

The volumetric efficiency of an engine depends on …

A

throttle position,
Ambient Temperature,
Ambient Pressure
RPM

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4
Q

The best action to take at the onset of detonation in an engine is …

A

select mixture fully rich and decrease the power

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5
Q

The onset of detonation in an engine is indicated by …

A

vibration,
Rising temperatures and
Reduced indicated air speed

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6
Q

One of the limitations applying to increased RPM for increased power in a piston engine is …

A

excessive rotor tip speed

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7
Q

The warm up period for an engine prior to take off provides …

A

proper oil viscosity and uniform heating of engine components

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8
Q

If the engine is over heating during a long climb, an appropriate pilot action would be …

A

increase indicated airspeed, richen the mixture and if necessary, reduce power

Helicopters fly full rich at all times but this is a generic piston engine question.

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9
Q

If cylinder head temperatures are becoming too low during a long descent, the pilot should …

A

reduce indicated air speed and increase power

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10
Q

The octane rating of a fuel is a measure of …

A

it’s resistance to detonation

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11
Q

A horizontally opposed engine should be held at about 1000 RPM after a cold start rather than idle to avoid …

A

excessive cylinder wear due to poor lubrication at RPM

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12
Q

A radial engine always has an uneven number of cylinders, commonly 5, 7 or 11. This is a necessary design feature to ensure …

A

uniformly spaced power strokes during the cycle

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13
Q

The function of oil in an engine is to …

A

clean,
cool and
lubricate

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14
Q

The viscosity of an oil is a measure of

A

the oil’s resistance to flow

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15
Q

The purpose of an oil cooler bypass is …

A

to prevent oil from passing through the cooler if it is already cold

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16
Q

If airflow to the oil cooler is interrupted by an obstruction in the duct ….

A

oil temperature will rise and oil pressure will fall

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17
Q

One cause of high oil temperature and low oil pressure could be …

A

very low oil level in the sump

18
Q

The purpose of gearing a propeller (rotor) in an aircraft engine is to permit the propeller (rotor) to turn at …

A

lower RPM and higher torque than the engine

19
Q

Operating an engine with too low and oil quantity will produce …

A

rising oil temperature and dropping oil pressure

20
Q

During a long climb, the cylinder head temperature becomes too high. This can be rectified by …

A

richening the mixture to full rich and increasing the climbing indicated air speed

21
Q

With the majority of opposed engines, the left -hand magneto …

A

fires the right top and left bottom plugs

22
Q

In a constant speed engine, the onset of fuel vapor locking would be indicated by …

A

fluctuating oil pressure

23
Q

If fuel vaporisation occurs during flight, the appropriate pilot action would be …

A

operate the fuel boost pump

24
Q

If the take-off manifold pressure exceeds rated boost in a turbo-charged engine …

A

detonation and engine damage could result

25
In a hydraulic system using a constant displacement pump, system pressure is controlled by ...
the pressure regulator
26
The main hydraulic power pump in a helicopter hydraulic system is powered by ...
mechanical drive from the main rotor transmission
27
If a left-hand-zero ammeter indicate zero during flight ...
the alternator has failed
28
A non return valve (check valve) is fitted to a hydraulic circuit to ...
ensure fluid only flows in one direction
29
The purpose of the cooler in an aircraft hydraulic system is to ...
cool the fluid as it returns from the pressure regulator to the reservoir
30
A reservoir may be pressurised to provide ...
positive fluid supply and reduced foaming
31
Hydraulic fluid requires ...
lubricating properties
32
A turbo charger with an exhaust leak upstream of the waste gate causes ...
decreased power output
33
The effect of a blocked pitot tube during a climb would be ...
an increasing nose pitch up attitude required to maintain climb indicated airspeed
34
To find the firing interval of a 4-stroke engine ...
divide 720 by the number of cylinders
35
A hazard associated with nickel/cadmium (NICAD) batteries in an aircraft is ...
thermal runway
36
A circuit breaker in an aircraft electrical system is provided to ...
protect a circuit against overload conditions
37
An airspeed indicator (ASI) will show true airspeed (TAS) in ...
ISA conditions at mean sea level
38
At 6000 ft the pitot becomes blocked, but the static vent is still clear. On descent the VSI will show ...
the correct RDO
39
With a fully articulated rotor head and wheeled undercarriage with unequal tyre pressures, a possible hazard is ...
ground resonance
40
The presence of carburettor icing may be verified by maintaining constant throttle and collective pitch settings, then applying carburettor heat and noting an immediate ...
decrease in MP, then a gradual increase