APU Flashcards

1
Q

Does APU have self-sealing fuel lines?

A

No

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2
Q

APU system provides what two powers/purpose?

A

Pneumatic (main engine starting and cabin heating) and electrical (ground operations and in flight emergency electrical power).

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3
Q

You can operate the aircraft without the APU but you risk:

A

Not being able to complete certain in flight Eps.

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4
Q

APU accumulator minimum pressure:

A

2800 PSI

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5
Q

Which fuel cell does the APU use?

A

1 fuel cell

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6
Q

APU oil reservoir contains how much oil?

A

3 qts

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7
Q

How is the APU generator cooled?

A

Air cooled

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8
Q

Limitation of APU Generator?

A

Cant power backup hydraulic pump and windshield anti ice at the same time. Backup hydraulic pump takes priority.

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9
Q

If the APU Generator Control Unit (GCU) detects an overload, the APU generator will:

A

Be taken off line and the APU GEN ON advisory light will extinguish.

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10
Q

What action is taken when APU OIL HOT caution appears?

A

APU shutdown immediately. After a 30 minute cooling period and oil level is okay, the APU may be restarted.

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11
Q

Electronic Sequencing Unit (ESU) will shut down the APU and provide a BIT code for any problems detected except:

A

APU OIIL HOT

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12
Q

If APU fails, you must do what before attempting another start?

A

Check APU BIT codes

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13
Q

The accumulator provides hydraulic pressure for driving the:

A

APU hydraulic starter

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14
Q

When AC power is applied to the aircraft, the backup pump will recharge the accumulator in:

A

90 seconds

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15
Q

If AC electrical power is not available, only the reserve fire bottle can be discharged and fire extinguishing capability will be lost to which engine?

A

2 engine

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16
Q

What 3 things occur when the APU Fire T Handle is pulled?

A

Fuel to the APU is shut off, a stop signal is sent to the ESU, the fire extinguishing system arms and the directional control valve is set to the APU compartment.