Air Systems (Bleed) Flashcards
Bleed Air is used in which systems? AOM II 2–34
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
Can the APU provide Bleed Air in flight? Up to what altitude? AOM II 7-36
Yes, for one Pack only. Up to 15,000’
Turning an “Engine Bleed” switch OFF does what? AOM II 2-13, 2-34
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.
If the switch is OFF, is NAI still available for that engine? Thrust Reversers?
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
What will illuminate the SYS Fault light? AOM II 2-12
Bleed Air Overheat
Bleed Air Overpressure
HP Bleed Valve and/or
PRV OPEN when commanded closed.
With the SYS FAULT light illuminated, is reversing available upon landing? AOM II 2-35
YES, unless light is on due to an overheat.
Which unit in the Bleed Air system reduces Bleed AIr temperature? AOM II 2-34
Fan Air Pre-Cooler
With a BLD 1,2,3,4, OVHT/PRV what systems are no longer available? AOM II QRH 2-3, 2-39, 2-35
Nacelle Anti-Ice
Reverse Thrust
APU Bleed Air is supplied to which duct? AOM II 2-37
Center Section of the Bleed Air duct
Where is the Duct pressure displayed? AOM II 2-14, 2-16
Primary EICAS
ECS Synoptic