How many hydraulic systems are on the airplane?
3 independent systems
HYD 1, 2 and 3
What systems use hydraulic power?
Can hydraulic fluid be transferred between systems?
No
How many hydraulic pumps are on the airplane?
Six:
What are the basic components of the hydraulic systems?
What do accumulators do?
Maintain constant pressure and prevent pump cavitation
When will ACMP 1 or 2 activate automatically on the ground?
When flaps are > 0 and:
When will ACMP 1 or 2 automatically activate when in the air?
- flaps > 0
Name some important systems controlled by HYD 2
What is the PTU?
- mechanical pump that uses HYD 1 power to provide HYD 2 pressure
What is the primary purpose of the PTU?
To allow landing gear retraction in the event of an engine 2 or EDP 2 failure
When will the PTU automatically activate?
When engine 2 or EDP 2 fails and:
With ACMP 1 and 2 in AUTO how is single engine taxi on engine 1 possible if nosewheel steering is on HYD 2?
What is the purpose of HYD 3?
Backup for the primary flight controls
What are HYD ACMP 3A and B pump switches ON and AUTO respectively?
- HYD ACMP is the backup and automatically activates if ACMP 3A fails
What HYD ACMP will function if the RAT is the only power source?
HYD ACMP 3A
In an electrical emergency what provides hydraulic pressure to flight controls until the RAT comes online?
HYD 3 accumulator
- after 8 seconds the RAT will power ACMP 3A
In an electrical emergency can HYD 3 system power requirements overload the RAT?
No. HYD 3 system pressure is unloaded automatically to prevent a RAT stall