Bleed Air System Flashcards

1
Q

The bleed air system receives air from 3 main sources, they are ?

A
  1. Engines
  2. APU
  3. Ground pneumatic sources
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2
Q

What (7) components & systems use bleed air?

A
  1. Air driven hydraulic pumps
  2. Wing anti ice
  3. Cargo heating
  4. Engine & APU starting
  5. Air conditioning packs
  6. Hydraulic reservoir pressurisation
  7. Trim air
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3
Q

Uses of APU bleed air on the ground?

A
  1. Air conditioning &,
  2. Engine starting
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4
Q

APU bleed air can be used in flight up to approx ?

A

22,000 ft

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5
Q

Positioning the APU bleed air switch to AUTO with the APU running opens which valves?

A

The APU bleed air valve & all 3 isolation valves (allowing air into the bleed air ducting)

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6
Q

Bleed air from the engine comes from the ……………section?

A

Low pressure or LP section

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7
Q

Air from the LP section is used primarily during ?

A

High thrust settings such as t/o, climb & cruise

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8
Q

Bleed air from the HP section is used to ?

A

Supplement LP air during low thrust settings such as descent

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9
Q

The bleed air system is controlled by the ?

A

ASCPC - the air supply & cabin pressure controller

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10
Q

What’s the job of the ASCPC?

A

To open & close the HP valve, & adjust the Fan Air Modulating Valve to provide cold air for the pre-cooler, which controls the bleed air temperature in the ducts

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11
Q

What does the PRSOV do?

A

The pressure regulating valve (PRSOV), controls the flow & pressure of air to the ducts

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12
Q

If the fan air pre-cooler cannot provide enough cooling for the bleed air, the PRSOV ?

A

Reduces the quantity of bleed air to keep the temperature within limits

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13
Q

Bleed Air Duct Protected Areas

A

Engine struts
Left wing
Right wing
Body duct

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14
Q

Under normal circumstances, what is the source of bleed air to start the second engine?

A

APU

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15
Q

What best describes the leak detection & isolation operation?

A

Automatic leak detection & automatic isolation, crew action is not required

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