Study Guide Hydraulics Flashcards
How many hydraulic systems 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 systems?
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 system?
- Reservoir
- Pumps
- Accumulator
What is the purpose of the accumulator?
- Helps maintain constant pressure by covering transient loads
- Helps avoid pump cavitations
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 > 0
What are some important items controlled by HYD 2 system?
- Landing gear
- Nosewheel 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 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
- 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 are HYD ACMP 3A & B pump switch positions ON & AUTO respectively?
- HYD ACMP 3A pump is primary and has no automation
- 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