How many hydraulic systems on the airplane?
- HYD 1, HYD 2, and HYD 3
What systems use hydraulic power?
Can hydraulic fluid be transferred between systems?
No
How many hydraulic pumps are on the airplane?
6 total:
What are the basic components of the hydraulic system?
What is the purpose of the accumulator?
When will ACMP 1 or 2 automatically activate?
Ground:
-Flaps >0, and
-TL set to T/O, or
-Groundspeed > 50kts
Flight
-Engine failure or EDP failure
-Flaps > 0What are some important items controlled by HYD 2 system?
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 the landing gear retraction in the event of an engine 2 or EDP 2 failure?
When will the PTU automatically activate?
During takeoff and landing with flaps >0, if
How is single engine taxi possible if nose wheel steering is on HYD 2?
Releasing the parking brake activates ACMP 2
What is the primary purpose of HYD 3 system?
Back up for the flight controls.
Why are HYD ACMP 3A & B pump switch positions ON & AUTO respectively?
- HYD ACMP 3B pump is a backup and automatically activates if ACMP 3A fails
What, if any, HYD ACMP will function if the RAT is the only power source?
HYD ACMP 3A only
In an electrical emergency what provides hydraulic pressure to flight controls until the RAT come online?
- After 8 seconds the RAT will power ACMP 3A
In an electrical emergency can HYD 3 system power requirements overload the RAT?
No. A flow limiter valve is used to reduce flow and limit pump electrical power draw to prevent a RAT stall.