Chapter 2 - Air Systems Flashcards

1
Q

Does the compartment INOP light illuminate if the temperature control is OFF or trim air is OFF ?

A

Yes.

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2
Q

What is the meaning of the pack INOP light ?

A
  • Pack overheat

- Fault

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3
Q

What is the meaning of the PACK OFF light ?

A

Pack valve is closed.

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4
Q

Does the recirculation INOP light illuminate if the recirculation switch is OFF ?

A

Yes.

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5
Q

How is the air warmed from the should and foot heaters ?

A

Electrically.

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6
Q

When is the equipment cooling NO COOLING light illuminated ?

A

Only in OVRD mode. No reverse air flow is being delivered !

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7
Q

What is the approximate ROC and ROD of the cabin altitude when the auto rate control is set at the index mark ?

A

+500 fpm, -300fpm

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8
Q

When does the cabin pressurization AUTO INOP illuminate ?

A

When both controllers are inop or when MAN has been selected.

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9
Q

When does the CABIN ALT light extinguish again ?

A

When cabin altitude is less than 8,500ft.

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10
Q

When does the APU VALVE light illuminate ?

A

Valve disagreement.

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11
Q

What is the meaning of the engine BLEED light ?

A

Bleed overpressure. The HPSOV or/and PRV are open, and should be closed.

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12
Q

Which has priority: high bleed air demand or high pack output ?

A

high bleed air demand. In this situation, high pack output is not possible.

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13
Q

What does the standby N(ormal) pack control do ?

A

Delivers constant, moderate temperature air.

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14
Q

How is temperature controlled with trim air OFF ?

A

Average air temperature for all zones.

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15
Q

What is the difference in equipment cooling on the ground or in-flight ?

A

On the ground, the supply and exhaust fan are active, hot air is expelled overboard if needed. In-flight it is normally only recirculated using the exhaust fan.

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16
Q

What is the normal cargo temperature when heated ? What about the vented bulk cargo temperature ?

A
  • 7 deg

- 18 deg

17
Q

When does the cargo OVHT light illuminate ?

A

> 32deg, the heating shutoff valve is automatically closed.

18
Q

What happens with cabin pressure during T/O ?

A

Slight positive pressure

19
Q

What happens with cabin pressure shortly before landing ? And at touchdown ?

A

Cabin pressure slightly below landing altitude. At touchdown, the outflow valve opens.

20
Q

When is the outflow valve automatically closed ?

A

When cabin altitude > 11,000ft, in both automatic and manual modes.

21
Q

Do the engine bleed valves close automatically under certain normal operations ?

A

Yes. (low demand on the ground, engine start,..)

22
Q

Is reverse air flow to the APU possible ?

A

No, because of a check valve.

23
Q

Until which altitude is APU bleed available ?

A

17,000 ft.

24
Q

Are the L/R isolation valve normally open ?

A

No, normally closed, except for engine start.

25
Q

Do the HPSOV and PRV normally close when the engine bleed air valves closes ?

A

Yes.

26
Q

Engine bleed air valve is closed, but engine anti-ice is activated. Is EAI available ?

A

Yes, the PRV opens but the engine bleed air valve remains closed.

27
Q

Which side of the bleed air system is ground pneumatic air added ?

A

To the L side, between the L isolation valve and the L pack.

28
Q

Is reverse thrust affected if the respective engine bleed valve is closed ?

A

Yes, it may be affected. The PRV is located before reverse thrust bleed air, and may be closed.