Hydraulic & Landing Gear System Flashcards
1
Q
The aircraft hydraulic power supply systems include the 3000 PSI ____ system powered by the left engine and the 3000 PSI _____ system powered by the right engine.
A
utility
flight control
2
Q
Hydraulic caution light illuminate for the following (2)
A
a. Low-pressure condition - Hydraulic pressure approximately 1500 PSI and below detected.
b. Fluid overtemperature - Excessively high fluid temperatures detected.
3
Q
The caution lights go out when hydraulic pressure is restored to approximately ____ PSI or when the hydraulic fluid temperature cools down below overheat threshold conditions. The hydraulic pressure indicators must be observed to determine which condition has caused the lights to illumi- nate.
A
1800
