Air Systems (Bleed) Flashcards

1
Q

Bleed Air is used in which systems? AOM II 2–34

A

PAWS HAD SALT
Pressurization
Air Conditioning
Water Pressurization (potable)
Smoke Detection (cargo compartment)
Hydraulic Reservoir Pressurization
Aft Cargo Heat
Demand Pumps (Air-Driven Hydraulic; GE 1&4, PW ALL)
Starters (engines)
Anti-Ice (wings and engines)
Leading Edge Flaps
Thrust Reversers

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2
Q

Can the APU provide Bleed Air in flight? Up to what altitude? AOM II 7-36

A

Yes, for one Pack only. Up to 15,000’

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3
Q

Turning an “Engine Bleed” switch OFF does what? AOM II 2-13, 2-34

A

Closes the:
Engine Bleed Air Valve
PRV - Pressure Regulating Valve
(will open for NAI and TR.
HP Valve - High Pressure Valve
(will open for NAI and TR.

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4
Q

If the switch is OFF, is NAI still available for that engine? Thrust Reversers?

A

A: - Yes, is still available unless;
HP valve failed OPEN
PRV failed closed
PRV closed automatically as a result of a Bleed Air Overheat
Engine Starter Valve has NOT closed
B: - Yes, T.R. are still available, unless;
PRV failed closed
PRV closed automatically as a result of Bleed Air Overheat
Engine Starter Valve has NOT closed

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5
Q

What will illuminate the SYS Fault light? AOM II 2-12

A

Bleed Air Overheat
Bleed Air Overpressure
HP Bleed Valve and/or
PRV OPEN when commanded closed.

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6
Q

With the SYS FAULT light illuminated, is reversing available upon landing? AOM II 2-35

A

YES, unless light is on due to an overheat.

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7
Q

Which unit in the Bleed Air system reduces Bleed AIr temperature? AOM II 2-34

A

Fan Air Pre-Cooler

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8
Q

With a BLD 1,2,3,4, OVHT/PRV what systems are no longer available? AOM II QRH 2-3, 2-39, 2-35

A

Nacelle Anti-Ice
Reverse Thrust

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9
Q

APU Bleed Air is supplied to which duct? AOM II 2-37

A

Center Section of the Bleed Air duct

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10
Q

Where is the Duct pressure displayed? AOM II 2-14, 2-16

A

Primary EICAS
ECS Synoptic

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