Hydraulic Flashcards
Hydraulic system provide power for:
- flight controls
- spoilers
- landing gear
- nose wheel steering
- wheel brakes
- thrust reversers
Normal hydraulic pressure
3,000 psig
Hydraulic System 1 is comprised of:
- one reservoir
- one engine driven pump (EDP 1)
- one electric pump
- one accumulator
Hyd system 1 powers
- elevator (left hand outboard)
- rudder (upper)
- thrust reverser (engine 1)
- multi function spoilers (l and r panels 3 and 4)
- ground spoilers (l and r panel 2)
- outboard brakes
- emergency parking brake
What does the hydraulic accumulator do?
helps maintain constant pressure by covering transient demands during normal operation and keeping residual pressure to avoid pump cavitation
Hydraulic System 2 is comprised of:
- one reservoir
- one engine driven pump (EDP 2)
- one electric pump
- one accumulator
- PTU
Hyd system 2 powers
- elevator (left and right inboard)
- ailerons (right and left inboard)
- thrust reverser (engine 2)
- multi function spoilers (l and r panel 5)
- ground spoilers (l and r panel 1)
- inboard brakes
- nose wheel steering
- landing gear
- emergency parking brake
How are the engine driven pumps powered
engine accessory gear box
In flight the electric pump 1 and 2 activates automatically when:
- EDP or engine fail or
- flaps selected greater than 0
- during landing for 60 seconds to avoid abrupt hyd pressure variations in the event of engine failure
On ground the electric pump 1 and 2 activates automatically when:
- flaps greater than 0 and
- thrust levers set to takeoff thrust or
- groundspeed greater than 50 its
- during takeoff w/ thrust levers at TOGA for 60 seconds to avoid abrupt pressure variations in the event of engine failure
On the ground electric pump 2 automatically activates when
- engine 1 running and parking brake released
- engine 1 running and flaps greater than 0
- during engine 1 start if parking brake has been applied at least 6 mins before
What is the purpose of the PTU
assists landing gear retraction or extension should a right engine or EDP pump fail
the PTU is powered by
a hydraulic motor in hydraulic system 1
the PTU will be automatically started when:
- flaps are not set to 0 or landing gear not up
- EDP 1 not failed
- hydraulic reservoir 2 quantity above 12%
(will not activate on ground)
Hydraulic system 3 is comprised of
- one reservoir
- two electric pumps
- one accumulator