Section 06 - APU Flashcards

1
Q

Assume all bus switches in AUTO, APU engine running, AUX PWR switch ON, and BATT 1 & 2 switches ON. If the battery switches were selected to OFF, what would happen to the APU?

A

There would be no change in APU operation.

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2
Q

Below what altitude is the APU guaranteed to start no later than the second start attempt?

A

15,000ft

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3
Q

What would happen if APU air is selected on immediately after APU start?

A

The APU air would turn on immediately

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4
Q

Normal shutdown of the APU is accomplished by pushing what switch?

A

The APU OVSP-STOP switch

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5
Q

Selecting what APU switch to the off position will close the APU fuel shutoff valve immediately?

A

The APU Master switch

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6
Q

Prior to starting the APU, how can the position of the right engine lower cowl door be checked?

A

Visually, or using the indicator light on the APU panel (if installed)

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7
Q

What is the minimum fuel temperature required prior to APU start?

A

Above -30ºC

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8
Q

If necessary, how can the batteries be warmed most effectively prior to APU start?

A

Use an external AC power cart to charge and warm the batteries

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9
Q

What is the minimum acceptable battery voltage prior to APU start?

A

22 volts DC

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10
Q

After APU start, when will the APU generator power the electrical buses?

A

When the AUX PWR switch is selected ON

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11
Q

How is an APU start manually terminated?

A

Depress the APU OVSP-STOP switch, which trillers the over speed circuit, resulting in an immediate start abort

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12
Q

Would an APU DIRE message cause the APU to shutdown in-flight or on the ground?

A

Both on the ground and in-flight

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13
Q

Can the APU provide pressurization in flight?

A

No

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14
Q

If an APU start attempt on the battery power fails, how long a wait is required in order to try a second attempt?

A

No waiting is required until it fails a third attempt, then 1 hour

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15
Q

If an APU start attempt on external DC power fails, how long a wait is required in order to try a second attempt?

A

15 minutes

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16
Q

From where does the APU receive its fuel?

A

From the motive flow line to the left fuel ejector

17
Q

How long is the recommended wait for turning on APU air after the APU is started?

A

2 minutes

18
Q

After a normal or automatic shutdown of the APU, what must be done in order to re-start the APU

A

Cycle the APU master switch to OFF, then ON

19
Q

What is indicated by the red “OIL PRESSURE LOW” light on the APU control panel?

A

The APU inlet door is fully open

20
Q

During APU shutdown, when is it acceptable to turn off the APU master switch?

A

After the APU RPM is less than 10%

21
Q

When is a specific APU inspection required in regard to normal operation of the APU?

A

An inspection is required if the APU is operated above 30,000 feet for more than 1 hour per flight, or on more than 5 occasions (not required for aircraft with the 36-150G APU)

22
Q

What is the maximum permissible APU EGT?

A
  • Up to 60% RPM during the start: 988°C
  • 60% to 100% during the start: 821 °C to 732°C (linear decrease)
  • Running: 732°C
23
Q

What is the maximum permissible APU EGT {36-150G)?

A
  • Up to 50% RPM during the start: 973°C
  • 51 % to 87% during the start: 973°C to 732°C (linear decrease)
  • 87% to 100% during the start: 732°C
  • Running: 732°C
24
Q

What are the APU starting limits?

A
  • With aircraft batteries: 30 seconds per start, 3 attempts, then 20 minutes cool down
  • With external DC power: 15 seconds per start, 2 attempts, then 20 minutes cool down
25
Q

The APU has just been started, Five minutes later, a red “APU FIRE” CAS message illuminates. The fire warning bell is also ringing. Describe the emergency procedure associated with this condition.

A
  • APU Overspeed Test Button - PRESS
  • APU Master Switch - OFF
  • APU Fire Extinguisher - PRESS
  • After 1 minute, APU Fire Test - PRESS
26
Q

The APU “HIGH OIL TEMP” light has illuminated. Describe the abnormal procedures associated with this condition.

A

No action is required. The APU will initiate an automatic shutdown