APU Flashcards

1
Q

Where is the APU situated?

A

In a fire proof enclosure at the rear fuselage at of the rear pressure bulkhead.

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2
Q

What tank does the fuel normally come from?

A

Left collector tank.

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3
Q

What electrical power is used for operation?

A

DC

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4
Q

What can the APU supply?

A

Bleed air and AC electrical power on ground

Inflight, electrical power only.

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5
Q

How do you start it?

A

Battery on. Check fire agent. Using Start button and releasing. (on RR place in ON for 15 seconds then start).

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6
Q

What does the AVAIL light tell you?

A

electrical power is available

bleed are is available after 2mins

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7
Q

APU: When is bleed air available after start?

A

2mins after AVAIL light comes on.

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8
Q

What faults will shutdown the APU in flight and what indications do you get?

A

Fire or APU over speed. If start sequence takes more then 90secs

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9
Q

What faults will shutdown the APU on the ground and what indications do you get?

A

Fire or APU over speed, plus low oil pressure, high oil pressure, high exhaust gas temp. and other internal APU failures.

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10
Q

What happens if the APU load becomes excessive?

A

it decreases bleed air.

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11
Q

May the APU operate unattended in the ground and why?

A

Yes, due to continuous self test feature on ground. Plus auto fire system

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12
Q

What can you do to enhance cabin cooling after landing in hot climates?

A

Turn APU on shortly before before landing.

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13
Q

When is it recommended that you leave the APU running for a flight?

A

As per MELed

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14
Q

Where and when is the APU page displayed?

A

can be manually or automatically displayed in some AIRCRAFT MFDU if AC buses are energized. Manual is via APU p/b on MFDS panel. APU page is automatically displayed when start switch is selected from OFF to ON, during APU start or if a APU parameter (EGT or RPM) exceeds its limit.

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