When will the HYD 1 HI TEMP EICAS caution message be displayed?
When the hydraulic fluid temperature increases to 100°C
When will the hydraulic SOV automatically close?
When fluid temperature reaches 125°C
What happens to the hydraulic system during an engine flameout?
FADEC depressurizes the respective EDP to reduce torque loads on the engine and facilitate a windmill start
When will the electric hydraulic pump #1 operate automatically in flight?
* Flaps any position greater than 0°
When will the electric hydraulic pump #1 operate automatically on the ground?
Flaps selected to any position greater than 0° and:
•Thrust levers set to takeoff thrust or
•Ground speed greater than 50 kt
What comprises hydraulic system #1?
Can hydraulic fluid be transferred between each system?
No
What is included in the hydraulic system 2 that is not on system 1?
Power transfer unit (PTU)
What is the PTU?
* Assists the landing gear retraction or extension, should the right engine fail or EDP fail
What does hydraulic system 3 power?
During an electrical emergency what happens to the hydraulic 3 overheat protection system?
It will be inhibited as well as the EICAS messages
What is normal hydraulic pressure?
3000 psi
How many hydraulic pumps are on the airplane?
When will the ACMP 1 or 2 automatically activate?
On ground:
•Flaps > 0 and
•Thrust levers set to T/O
•Groundspeed > 50 kts
In flight:
•Engine failure or EDP failure
•Flaps > 0
When will hydraulic system 2 automatically activate?
* During engine 1 start if parking brake has been applied within the last 6 mins
What happens to the lettering on the hydraulic MFD page in the event of a system failure?
The size of the letters increases
What is the pump unloaded valve?
•Reduces discharge of the ACMP 3A when the RAT deploys
What is the flow limiter valve?
* Prevents the RAT from stalling