Hydraulic Flashcards
What systems do are the hydraulics responsible for?
Flight controls, landing gear, brakes.
How are hydraulic systems 1 and 2 cooled?
A shared air/fluid heat exchanger. No fluid exchanges occurs within the heat exchanger.
Why doesn’t hydraulic system 3 require any cooling?
The components for system 3 do not pass near any heat sources that would require extra cooling.
Hydraulic SOVs can be closed by selecting the respective ____ switchlight or the ____ switchlights.
ENG FIRE PUSH or HYD 1/2 SOV
Hydraulic pump ____ will continue to operate regardless of switch position following ___ deployment.
3B
ADG deployment
What is the name of the fluid found in the hydraulic lines?
SKYDROL
How many hydraulic pumps are there are the CRJ 900? Describe them:
6 pumps; 3 primary 3 backup.
Systems 1 and 2 A pumps are engine driven, the rest are electric pumps.
Arrange the hydraulic systems in terms of size from largest to smallest.
3 largest
2 med
1 smallest
What components would you lose if you lost hydraulic system 1? (Use synoptic page)
OB Multi function spoiler(spoileron/flt spoiler), OB Ground spoiler, L reverser.
What components would you lose if you lost Hydraulic system 2? (Use synoptic page)
IB Multi function spoiler (spoileron/flt spoiler), LG Alternate Extension, R reverser, OB Brakes.
What components would you lose if you lost hydraulic system 3? (Use synoptic page)
IB Ground spoiler, Landing gear extension, Nosewheel steering, IB Brakes
What would you be concerned about if you were to lose Hydraulic system 2 and 3?
Landing gear deployment would have to be done by manual release handle. Nose gear will not deploy. Braking would only be done by accumulators up to 6 times with no anti skid.
What effects on the braking system would occur with a loss of hydraulic system 3?
50% of braking loss due to IB brake loss.
How many brake applications would be possible following failure of hydraulic systems 2 and 3?
Up to 6 applications from accumulators.
When will hydraulic pumps 1B and 2B turn on in the AUTO position?
During critical phases of flight when flaps are greater than 0 and cross side bus is powered with any AC GEN operating.