Pneumatics, Air conditioning & Pressurization Flashcards

1
Q

Which engine stages is bleed air taken from?

A

The 9th (low pressure) and 14th (high pressure) stages. AOM 2-14-05 page 2.

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2
Q

When does the 14th stage valve, called the High Stage Valve (HSV), open automatically?

A

During low thrust operations, engine cross bleed start, and anti-ice operation. AOM 2-14-05 page 2.

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3
Q

When does the Cross-Bleed Valve (CBV) open and close automatically?

A

During engine start, depending on the available pneumatic source (APU, ground pneumatic source, or opposite engine). AOM 2-14-05 page 2A.

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4
Q

What causes the APU Bleed Valve (ABV) to automatically close?

A

Whenever any engine is supplying bleed air to the left pneumatic side. AOM 2-14-05 page 4

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5
Q

What causes the APU Bleed Valve (ABV) to automatically close?

A

Whenever any engine is supplying bleed air to the left pneumatic side. AOM 2-14-05 page 4.

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6
Q

What cools the packs?

A

ACM fans on the ground, ram air in flight. AOM 2-14-10 page 2.

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7
Q

When automatic temperature control is used, what are the temperature limits in the cockpit and cabin?

A

Between 18°C and 29°C. AOM 2-14-10 page 5.

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8
Q

How do you activate manual cockpit and cabin temperature control?

A

Pull the temperature knobs. AOM 2-14-10 page 5.

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9
Q

Which pack is the main source of conditioned air to the cockpit?

A

The left pack. AOM 2-14-10 page 6.

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10
Q

Where does the gasper air subsystem provide air to?

A

The individual air outlets (gasper) in the cabin, the rear electronics compartment, the oxygen cylinder compartment, and relay box ventilation. AOM 2-14-10 page 6

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11
Q

What happens when the Cabin Temperature Knob is rotated to the ATTD position?

A

The passenger cabin temperature control is transferred to the attendant’s panel. AOM 2-14-10 page 13.

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12
Q

Will the ATTD selection on the Cabin Temperature Knob on the overhead panel work in manual mode?

A

No. It only works in automatic mode. AOM 2-14-10 page 13.

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13
Q

What is maximum differential pressure?

A

7.8 psi. AOM 1-01-48 page 1.

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14
Q

At what altitude does the Cabin Pressure Acquisition Module (CPAM) alert the crew of high cabin altitude?

A

9,900 +/- 100 ft. AOM 2-14-15 page 1.

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15
Q

What will happen if the landing altitude is not entered in the Digital Controller?

A

The system will automatically consider 8,000 ft as the landing altitude.

AOM 2-14-15 page 2.

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16
Q

What will happen if, while in AUTO mode, the Manual Controller is moved out of the DN position?

A

The pneumatic valve will open, causing inappropriate automatic mode operation. AOM 2-14-15 page 2.

17
Q

What opens the outflow valves?

A

Vacuum, created when bleed air from either or both engines that is ducted through an ejector pump.

AOM 2-14-15 page 3.

18
Q

If the cabin is depressurized by pressing the DUMP button, how high will the cabin altitude rise?

A

14,500 ft.

AOM 2-14-15 page 8.

19
Q

Will the DUMP button work in the manual mode?

A

No.

AOM 2-14-15 page 7.

20
Q

What are the memory items for Rapid Cabin Depressurization?

A

Crew Oxygen Masks…DON
Crew Communication…ESTABLISH, Emergency Descent…AS REQUIRED.

AOM 1-03-24 page 2.

21
Q

What are the memory items for Emergency Descent?

A
Cabin Crew...NOTIFY
Fasten Belts...ON, 
Thrust Levers...IDLE,
Speed Brakes...OPEN, 
Airspeed...250 KIAS, 
Landing Gear...DOWN, 
Altitude...MEA OR 10,000 FT WHICHEVER IS HIGHER. 

AOM 1-03-30 page 1.