Questions Flashcards

1
Q

What can an impeller either be?

A

Single or double entry

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2
Q

What must the combustion chamber be able to do?

A

Permit safe ignition of the fuel air mixture on ground and in flight

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3
Q

What type of engines are bleed air used on?

A

Ones with high mass airflow

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4
Q

What are the three types of turbine blades?

A

Impulse, impulse-reaction, reaction

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5
Q

What is the first main component of a turbine?

A

Stationary vanes called nozzle guide vanes

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6
Q

What are the blades on stators?

A

Stator vanes that guide and slow the airflow causing an increase in pressure

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7
Q

How is the fuel air mixture ignited?

A

Electrically by an igniter plug

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8
Q

How can fan air be discharged in fan reversers?

A

Through cascade vanes

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9
Q

Why were additives added to type 1 oils?

A

Increase resistance to oxidation and thermal degradation, important for long term engine cleanliness

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10
Q

What is the exhaust system used for in turboprop engines?

A

Safely guide the exhaust gases overboard

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11
Q

Three different types of combustion chambers?

A

Can, can annular, annular

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12
Q

What does any stress crack or deformation on the leading edge of the first stage of the compressor usually mean?

A

Over-temperature conditions

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13
Q

What does SOAP stand for?

A

Spectrometric Oil Analysis Program

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14
Q

How much does the high pressure fuel pump increase fuel pressure to?

A

900 psi

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15
Q

What is the order of oil movement from the oil tank to the oil coolers?

A

From the oil tank to the oil pump. Then to the pressure filter housing. Then the oil filter. Then to the air oil heat exchanger, then to the fuel cooled oil cooler

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16
Q

What is pour point?

A

The lowest temperature oil will visbly move in a 31.75mm test tube held horizontally for 5 seconds

17
Q

What is flash point?

A

The lowest temperature that oil will give enough vapour to flash when a flame is applied

18
Q

What does FADEC stand for?

A

Full Authority Digital Electric Control

19
Q

What is the primary component of FADEC?

A

The EEC (Electronic Engine control) controls the operation of the engine

20
Q

What is used for sealing the engine bearing chambers?

A

Low pressure bleed air

21
Q

What is zone 2 cooled by?

A

Fan air from the upper part of the fan duct and is exhausted at the lower back end into the fan air stream

22
Q

When is continuous ignition used?

A

When there is a possibility of flame out

23
Q

How is the generator turned?

A

By the engine through the accessory gearbox

24
Q

What is one of the reasons for automatic APU shutdown?

A

Low oil pressure

25
Q

What is the drain collector assembly?

A

Also known as the manifold module, it keeps fluid leaks in small tanks

26
Q

What is used for large commercial aircraft for fire protection?

A

Continuous Loop Detector System

27
Q

Where is a low pressure filter installed?

A

Between the supply tanks and engine fuel system to protect the engine fuel pumps

28
Q

What is the level of gas engine vibration?

A

Extremely low vibration levels so any change in level as response to an impeding failure may go unnoticed

29
Q

Is it important to monitor the oil consumption of the engine?

A

Yes, so it should be recorded in the aircrafts technical logbook

30
Q

What are the two fire detection loops?

A

Loop 1 and 2 (continuous loop system)

31
Q

What is the APU?

A

Auxiliary Power Unit, small gas turbine engine (free turbine) turboshaft that provides pneumatic bleed air and electrical power for aircraft systems

32
Q

What is the most common extinguishing agent?

A

Halon 1301

33
Q

What should be used if the wash of an engine is in low temperature conditions?

A

Only isopropyl alcohol as anti freeze, as methanol is damaging to titanium