How many hydraulic systems are on the aircraft?
Three: Green, Blue, and Yellow
Which systems power the flight controls?
All three
How is the green system normally pressurized?
By engine 1-driven pump
How is the yellow system normally pressurized?
By engine 2-driven pump
How is the blue system normally pressurized?
By an electric pump
Can the yellow system be pressurized without engine 2?
Yes — via electric pump or hand pump (cargo door)
Can the blue system be activated on the ground with no engines running?
Yes — by selecting BLUE PUMP to AUTO with external power or APU on and pressing the BLUE PUMP OVRD pb in the avionics bay
What happens when PTU is operating?
Power Transfer Unit uses pressure from one system to drive a pump to pressurize the other — no fluid is transferred
When does the PTU automatically operate?
After both engines are running and pressure differential >500 psi between green and yellow systems
What would inhibit PTU from running?
Parking brake on, first engine only, cargo door operation
What does a PTU fault light indicate?
Automatic operation inhibited or pump overheated
What does a reservoir fault light indicate?
Low air pressure, low fluid quantity, or high temperature
What does a pump fault light indicate?
Low pressure (and electric/eng pump selector is ON)
If electrical power is lost, which hydraulic system is available?
Blue — via RAT deployment
What does the RAT supply?
Blue hydraulic pressure and emergency electrical power
What powers the nose wheel steering?
Yellow system (green alternate on some aircraft)
How can nose wheel steering be regained after complete hydraulic loss?
Only if yellow pressure is restored (via engine or hand pump + accumulator)
What is the only hydraulic system that can be pressurized manually on the ground?
Yellow — via hand pump for cargo door operation
What happens if yellow and green systems both fail?
Loss of landing gear, brakes, steering (brake accumulator may retain pressure briefly)