Hydraulics Questions Flashcards
How many hydraulic systems are on the airplane?
- 3 Independent systems
- HYD 1, HYD 2, and HYD 3
What systems use hydraulic power?
- Flight controls
- Spoilers
- Landing gear
- Nose wheel steering
- Wheel brakes
- Thrust reversers
Can hydraulic fluid be transferred between each system?
- No
How many hydraulic pumps are on the airplane?
- 6 total: 2 EDPs (Engine Driven Pumps)
4 ACMPs (AC Motor Pumps)
What are the basic components of the hydraulic systems?
- Reservoir
- Pumps
- Accumulator
What is the purpose of the accumulator?
- Helps to maintain constant pressure by covering transient demands
- Helps to avoid pump cavitation
When will ACMP 1 or 2 automatically activate?
- Ground
Flaps > 0, and
TL set to T/O, or
Groundspeed > 50 kts - Flight
Engine failure or EDP failure
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 and extension 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 ACMP 2
What is the primary purpose of HYD 3 system?
- Back-up for the Flight controls
Why does HYD ACMP 3A pump switch have an ON position and HYD ACMP 3B have an AUTO position?
- HYD ACMP 3A pump is primary and has no automation
- HYD ACMP 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 ACMP 3A only