Air/Pneumatic System Flashcards
What sources can supply the pneumatic system with pressurized air?
The 6th or 10th stage compressor sections off the engines, APU or a external ground air source
What is the function of the Air Conditioning System Controller? (ACSC)
Bleed source selection, Valve operation, air distribution
Where is the Engine start external ground air connector?
After left side of the fuselage
Where is the external ground air pressure (high pressure) monitored from the cockpit?
ECS Synoptic Page
What is the function of the Engine Bleed Valve (PRSOV)?
Limits and regulates the discharge pressure from the engine to 45psi ±3 psi
How can the pilot manually close the bleed valves?
By using the manual portion of the Bleed Air Control Panel
What is the function of the high pressure valve (HPV)?
To supply the 10th stage pressure when the system demands are greater than that of the 6th stage bleed air
What is the function of the APU LCV?
It opens to provide bleed air for ECS and engine starts and modulates to control the amount of bleed air taken from the APU
What unit controls the APU LCV?
The APU ECU
What side of the bleed manifold does the APU supply bleed air?
The left side
What is the function of the Isolation Valve?
To connect the left and right sides of the bleed manifold?
When does the Isolation Valve automatically open?
During engine starts, and when the APU LCV is opened
When does the Isolation Valve automatically close?
During transfer of the bleeds from the APU to the engines
How can the pilot manually operate the Isolation Valve?
Using the switches on the Bleed Air Control Panel
What bleed source will supply the bleed air manifold on the ground with the APU and engines running and the bleed valve selector in the auto mode?
APU
When does the ACSC switch from the APU to the engines as a bleed source after departure?
When the thrust levers are retarded from the takeoff detent, flaps up and gear up (20 sec)
When does the ACSC switch from the engines to the APU as a bleed source during approach?
When the flaps are greater than 20° or the gear is down (20 sec)
What will occur if the APU is supplying bleed air to the manifold and either cowl or the wing anti-ice is selected on with both engines operating?
The ACSC will close the APU LCV and transfer the bleeds to the engines