Hydraulics Flashcards
What systems use hydraulic power?
Flight controls Spoilers Landing gear Nose steering Brakes Thrust reversers
Can hydraulic fluid be transferred between each system?
No
How many hydraulic pumps are on the airplane?
6 total
2 EDP ( engine driven pumps) 4 ACMP (AC Motor Pump)
What are the basic components of the hydraulic systems?
Reservoir
Pumps
Accumulator (2 on HYD 1/2, HYD 3 has 1)
What is the purpose of the accumulator?
Helps to maintain constant pressure by covering transient demands
Helps avoid pump cavitation
When will ACMP 1 or 2 automatically activate on the ground?
Flaps > 0, and
TL set to T/O, or
Ground speed > 50 kts
When will ACMP 1 or 2 automatically activate in flight?
Engine failure or EDP failure OR
Flaps > 0
What are some important items controlled by HYD 2 system?
Landing gear
Nose wheel steering
Inboard brakes
What is the PTU?
Power Transfer Unit
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?
During takeoff and landing with flaps >0, if
Engine 2 fails, or
EDP 2 fails
How is single engine taxi possible if nose wheel steering is on HYD 2?
Releasing the parking brake activates ACMP2
What is the primary purpose of HYD 3 system?
Back-up for the flight controls
Why are HYD ACMP 3A & 3B pump switch positions ON & AUTO respectively?
HYD 3A pump is primary and has no automation
HYD 3B pump is a back-up and automatically activates if ACMP 3A fails
What, if any, HYD ACMP will function if the RAT is the only power source?
HYD 3A only