APU Flashcards

1
Q

What happens during a normal APU shutdown?

A
  • Pneumatic power is removed immediately

* Electrical power is removed after a 1 minute cool down period

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2
Q

Can the APU shutdown sequence be cancelled?

A

Yes, by turning the APU selector knob back to ON during the shutdown sequence

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3
Q

What happens during an emergency APU shutdown?

A

The APU fuel shutoff valve closes and the APU shuts down without a two minute cool down period

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4
Q

The APU can supply electrical power up to?

A

33,000 feet

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5
Q

The APU can supply bleed air for engine starting up to?

A

21,000 ft

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6
Q

The APU can supply bleed air for air conditioning and pressurization up to?

A

15,000 ft

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7
Q

Where is the APU supplied fuel from?

A

The right wing tank

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8
Q

Is it possible to supply fuel to the APU from the left wing tank?

A

Yes, via a crossfeed valve

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9
Q

What automatically controls and monitors the APU?

A

It’s own dedicated FADEC

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10
Q

To avoid unsuccessful attempt starts it is recommended to wait how long before starting the APU after the EICAS is energized?

A

30 seconds

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11
Q

Max APU starting altitude

A

30,000 ft

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12
Q

What battery is used for the APU start?

A
  • BATT 2 powers the starter

* BATT 1 powers the FADEC and EICAS for monitoring

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13
Q

What will the APU automatically shut down for in flight?

A
  • Overspeed
  • Underspeed
  • FADEC critical fault
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14
Q

How long until the APU is ready to receive electrical and pneumatic loads?

A

3 seconds after APU reaches 95%

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15
Q

Minimum battery voltage for an APU start?

A

22.5 v

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16
Q

Which pump supplies fuel to the APU?

A
  • DC fuel pump with no AC power
  • AC fuel pump with AC power
  • Ejector fuel pump with engine running
17
Q

What will the APU automatically shut down for on the ground?

A
  • Overspeed
  • Underspeed
  • FADEC critical fault
  • APU fire
  • High oil temperature
  • Low oil pressure
  • EGT over temperature