DSC Hydraulic Flashcards
What is the normal pressure of the HYD system ?
3000PSI
2500PSI if powered by RAT
What system can pressurizes the Yellow HYD system ?
ENG 2 pump
Can be ELECT Pump or hand pump
What system can pressurizes the Blue HYD system ?
Elect pump
And RAT in an emergency
Can any fluid be transferred with the PTU ? And when will it automatically start ?
No
Diff pressure of 500PSI
When will the RAT automatically deploy ?
when AC BUS 1 & 2 are lost
What system pressurises the HYD reservoirs
HP bleed from ENG 1, if too low can use the pressure from crossbleed duct
It’s avoid cavitation
What are the main systems powered by the green HYD ?
Landing gear
Flaps/slats
Reverser 1
Normal brakes
flight controls
What are the main systems powered by the Blue HYD ?
Emer gen
Slats
flight controls
What are the main systems powered by the Yellow HYD ?
Flaps
Alternate braking
Parking brake
NWS
Flight controls
Reverser 2
Cargo door
What are the main operational consequences of loosing Green HYD ?
-No landing gear retract => Gravity extension
-Loss of autobrakes and normal brakes
-landing distance due to 2 spoilers lost and 1 rev
What are the main operational consequences of loosing Blue HYD ?
- Loss of emer gen if loss of fluid
- loss of redundancy
- slightly longer landing distance
What are the main operational consequences of loosing Yellow HYD ?
- can’t vacate due to no NWS
- landing distance due to 2 spoilers and Rev 2 lost
- loss of alternate braking => Check pressure on stand for park brake
For a dual HYD failure, how would you describe by few words the main consequences of loss of B+Y, G+B, G+Y ?
B+Y => Least detrimental
G+B => controllability
G+Y => Stopping
What are the main operational consequences of dual HYD failure B+Y ?
- Normal law but no AP
- no NWS
- increased landing distance
- Landing gear gravity extension to protect remaining system
- no Speed brakes
What are the commun consequences of any dual HYD failure ?
- CAT 1 landing capability due to AP1&2 Lost
- Landing gear by gravity so no gear retract
- increase landing distance