Air Systems/Pneumatics/Air Conditioning/Pressurization Flashcards
On the Cabin Pressurization Panel, what has occurred if both the amber AUTO FAIL light and the green ALTN light is illuminated?
A single channel controller failure has occurred
The OFF SCHED DESCENT light indicates the aircraft began descent before having reached the planned cruise altitude. What does the controller program the cabin to?
to land at the takeoff field elevation without further pilot inputs
Which stages of the compressor section is bleed air is obtained from (NG aircraft)?
5th; 9th
The ___ high-stage valve modulates open to maintain proper pressure when 5th low-stage pressure is insufficient (NG aircraft).
9th
The engine bleed air valve is normally _____ operated and DC power activated.
Pneumatically
What does the illumination of the BLEED TRIP OFF light indicate?
engine bleed air temperature or pressure exceeds a predetermined limit
When the BLEED TRIP OFF light illuminates, what effect does this have on the engine bleed air system?
The respective engine bleed air valve closes automatically
The isolation valve is _____ when the isolation valve switch in AUTO, both engine bleed air switches ON, and both air conditioning pack switches AUTO or HIGH.
Closed
The isolation valve is _____ when the isolation valve switch in AUTO, if either an engine bleed air switch or an air conditioning pack switch is positioned OFF.
Open
Turning the APU bleed air switch OFF with the PACK switches in AUTO will cause the isolation valve to open.
False
The APU bleed air valve is___ operated and ______ activated.
Pneumatically; DC
Engine thrust must be _______ with the DUAL BLEED light illuminated.
Limited to idle
______causes a WING-BODY OVERHEAT condition.
A bleed air duct leak
Which WING-BODY OVERHEAT light will illuminate if a leak in the bleed duct from the APU occurs?
Left
The isolation valve _________ if either engine BLEED air or air condition PACK switch is positioned OFF with the ISOLOATION VALVE switch in AUTO.
Automatically opens
Conditioned air from which PACK, upstream of the mix manifold, flows directly to the flight deck?
Left pack