Hydraulic

Question 1

The airplane is equipped with two independent hydraulic systems, each powered by

Answer 1

one engine driven pump and one electric motor driven pump

Question 2

Both hydraulic systems are identical, except for the services each system provides and a _ valve installed in the hydraulic system 1

Answer 2

Priority

Question 3

The engine driven hydraulic pump provides continuous fluid flow at _psi

Answer 3

3000

Question 4

The electrical hydraulic pump normally operates in the automatic setting mode, turning on when the associated hydraulic pressure drops below _ psi or the associated engine N2 drops below 56.4%

Answer 4

1600

Question 5

The hydraulic electric pump furnishes continuous fluid flow at _ psi

Answer 5

2900

Question 6

The purpose of hydraulic accumulator system 1 is to keep a _ psi pressure available for operation of the _

Answer 6

3000
Landing gear and Main Door

Question 7

A _ valve is installed between the reservoir and the engine driven pump

Answer 7

shut off