Praetor APU Flashcards

1
Q

What services does the APU provide and what are they used for?

A

-An electrical generator supplies 28VDC to the electrical system. The pneumatic power is used for engine starting and to supply bleed air to the air-conditioning pack of the environmental control system (ECS).

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2
Q

How is the APU controlled and monitored?

A

Through a dedicated Full Authority Digital Electronic Control Unit (FADEC).

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3
Q

What does pressing the APU ON/OFF button do?

A

It starts the ECU power-up sequence and initiates the APU built-in test (BIT)

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4
Q

When does the START button on the APU Control Panel flash green?

A

During the ECU bit test

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5
Q

What does the START button on the APU control panel illuminating steady green indicate?

A

The APU is ready to start

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6
Q

If the START button on the APU control panel illuminates amber what does that indicate?

A

The APU start is inhibited

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7
Q

What are the APU starter limitations?

A

Up to three consecutive unsuccessful start attempts are allowed with 30 second intervals between attempts

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8
Q

What MFD page can APU information be seen on?

A

The STATUS synoptic page

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9
Q

Which tank normally supplies fuel to the APU?

A

The right tank

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10
Q

Is it possible to feed the APU from the left-wing tank? If so, how?

A

Yes, via the cross-feed system

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11
Q

Can the APU supply bleed air on the ground or in flight?

A

Yes

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12
Q

If the APU is the only source of electrical power on the ground, what buses can the APU power?

A

All of the airplane electrical loads and can charge both batteries

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13
Q

If the APU is the only source of electrical power in flight, what buses can the APU power?

A

All electrical loads (except for the SHED BUSES) and also charging both batteries

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14
Q

What is the APU operating envelope for starting, operation, and to supply electrical power?

A

Up to 31,000 feet

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15
Q

Up to what altitude is the APU able to supply bleed air for engine starting?

A

Up to 23,000 feet

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16
Q

Where does the APU get its power for starting?

A

The number two battery

17
Q

What should be displayed on the STATUS synoptic page if the APU oil quantity is sufficient?

A

A green “OK”

18
Q

List the 4 conditions that will cause the APU to automatically shut down either in flight or on the ground.

A

-Overspeed
-Underspeed
-ECU internal failure
-APU bleed leak

19
Q

List the conditions that will cause the APU to automatically shut down on the ground only.

A

-APU fire
-APU EGT overtemperature
-APU high oil temperature
-APU low oil pressure
-APU starter not engaged
-APU shut off valve failure