M15.18 APU Flashcards

1
Q

What is the certification achieved by an aircraft possessing and in flight APU?

A

ETOPS (Extended twin operational performance) certification

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2
Q

In flight APU require a lower starting altitude of what?

A

Around 15,000-17,000 feet
Capable of operation up to 40,000 feet

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3
Q

Why are APU started during aircraft’s landing phase?

A

Unloads main engines pneumatic burden and allows the engine to keep compressor air for reverse thrust

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4
Q

Three sections of an APU?

A

The power section
The bleed section
The accessory gearbox section

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5
Q

The power section of the APU drives what?

A

The compressor and gearbox

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6
Q

The gearbox drives what APU accessories?

A

Fuel pump
Oil pump
Cooling fan
A-C generator

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7
Q

On some APU a separate compressor is installed to support the pneumatic system, what is this called?

A

The load compressor

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8
Q

As with all gas turbine engines, what makes up the power section?

A

A compressor
A combustion chamber
A turbine

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9
Q

On modern APU what type of combustion chamber is used? What about old ones?

A

Modern is annular type
Can find can type on older

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10
Q

The APU has what to monitor start sequence, turbine speed, EGT and oil and fuel supply?

A

Electrical control box

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11
Q

An electronic APU control unit controls the APU in what three different modes?

A

The start module controls the APU start activation until it’s reached 100% speed
The normal speed mode keeps APU at 100% speed
The APU shut down mode monitors and controls shut down

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12
Q

APU start sequence

A

Manually operated switches in flight deck to supply electrical power to APU from GPU

A test is then conducted to ensure circuits and sensors function correctly

APU air inlet door opened, APU fuel supply prepared, fuel shut off valve opened, fuel boost pump switched on.

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13
Q

If APU start sequence fails what happens?

A

APU doesn’t start

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14
Q

Throughout acceleration the fuel metering is controlled by what?

A

The APU control unit

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15
Q

What two signals does the APU control unit use for constant speed control?

A

The APU speed signal
The torque motor signal

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16
Q

What factors affect APU operation?

A

APU bleed load
Electrical load
Air inlet temperature
Air inlet pressure

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17
Q

If APU bleed load increases if what?

A

The APU bleed valve is open

18
Q

When the bleed load increases what else increases?

A

APU EGT (Exhaust gas temperature)

19
Q

The APU can only shut down after it has operated for a sufficient time without what?

A

A pneumatic or electric load

20
Q

Cool down period for APU shut down?

A

Varies between 0-120 seconds. Adjusted during maintenance

21
Q

Where is the APU fuel normally taken from?

A

The aircraft’s main engine fuel feed system

22
Q

Main components of APU fuel feed system?

A

APU fuel boost pump
APU fuel shut off valve (known as low pressure fuel shut off valve)
APU fuel feed line
Pressure switches

23
Q

What does the pressure switch do in the APU fuel system?

A

Monitors fuel pressure in fuel feed line directly in front of APU and triggers warning if fuel pressure is too low

24
Q

Having positive fuel pressure in the APU fuel feed line is important why?

A

prevent cavitation at the high pressure fuel pump of the APU

25
Q

APU air system is divided into what two sub systems?

A

Cooling air system
Bleed air system

26
Q

The cooling air system in the APU supplies air to where?

A

Oil cooler and APU compartment ventilation

27
Q

Three main tasks of bleed air system in APU?

A

Bleed supply
Surge protection
The load compressor control (if it has one)

28
Q

The load compressor does what in the APU?

A

Controls the amount of air going over the load compressor to meet the bleed demand of aircraft pneumatic system

29
Q

What two conditions are needed to open APU bleed valve?

A

Bleed stitch in on position
APU start sequence must have been completed

30
Q

Why are APU’s with load compressors more fuel efficient?

A

Airflow across load compressor can be adapted to the aircraft’s bleed air demands

31
Q

As it cannot be turned off, how is the air inlet closed off for the load compressor?

A

Inlet guide vanes

32
Q

Main components of the load compressor system?

A

Variable inlet guide vanes
Inlet guide vane actuator with mechanical transmission assembly
APU control unit

33
Q

When can APU compressors surge?

A

When bleed load changes

34
Q

How can APU compressor surge be prevented?

A

By bleeding off the air that is blocking the compressor discharge

35
Q

What surge protection is used on APU without load compressors?

A

Anti surge system

36
Q

For APU with load compressors what is the method of surge protection?

A

Surge protection system monitors the airflow in load compressor discharge duct and opens a surge control valve if the compressor surges.

37
Q

As a general rule,what is said about the surge control valve?

A

If the airflow behind load compressor decreases or stops the valve opens

38
Q

Automatic APU shutdown is always activated by what?

A

APU control unit

39
Q

Where are the external emergency APU shut down switches?

A

At the nose landing gear
In the main wheel well
On the refuelling station depending on aircraft size and type

40
Q

What is the quickest way to shut down the APU?

A

Activate the fire switch

41
Q

What will cause an automatic APU emergency shut down?

A

A fire condition when aircraft is on the ground

42
Q

Is the APU compartment pressurised?