SV Hydraulics

Question 1

The center hydraulic system has an isolation function which: [8.130.10]

Answer 1

A. Ensures the pilots can lower the landing gear.
B. Allows nose gear steering to be operational for landing, rollout and taxi.
D. A and B are correct

Question 2

Normal brakes are powered: [8.140.10]

Answer 2

C. Electrically

Question 3

The Center Demand pump operates: [8.130.10]

Answer 3

A. On the ground for the first three minutes after the second engine is started. B. During takeoff roll and gear retraction.
C. When flaps and slats are in motion. D. All the above

Question 4

The left hydraulic system powers which systems? [8.130.10]

Answer 4

C. Some flight controls and left engine thrust reverser

Question 5

T or F
One hydraulic system provides adequate airplane control. [8.130.10]

Answer 5

A. True

Question 6

With the left or right hydraulic demand pump selectors in the AUTO position, which of the following is true? [8.130.10]

Answer 6

A. Pumps operate from takeoff thrust set to flaps retracted.
B. Pumps operate for three minutes after second engine is started.
C. Pumps operate during thrust reverser operation.
D. All the above

Question 7

Which hydraulic pump(s) may be shed to allow the electrical system to provide power to other systems? [8.130.10]

Answer 7

A. Center Demand Pump.
B. Left Demand Pump.
C. Right Demand Pump.
D. All of the above

Question 8

The hydraulic isolation system ensures: [8.130.10]

Answer 8

C. Landing gear can be lowered and nose wheel steering operates

Question 9

Which of the following will cause the RAT to deploy automatically in flight? [8.130.10]

Answer 9

D. Left, Center, and Right Hydraulic pressure low

Question 10

What component(s) does the RAT hydraulically power? [8.130.10]

Answer 10

C. Primary flight control components normally powered by the center hydraulic system.

Question 11

T or F
All 3 hydraulic systems will provide up to 4000 psi per system, L,C,R.? [8.130.10]

Question 12

T or F
All 3 hydraulic systems will provide up to 4000 psi per system, L,C,R.? [8.130.10]

Answer 12

B. False

Question 13

What happens if both the C1 and C2 Pump selectors are positioned to ON at the same time? [8.130.20]

Answer 13

A. Both pumps will run continuously

Question 14

Which of the following components are powered by the right hydraulic system? [8.130.10]

Answer 14

B. Some flight controls.
C. Right engine thrust reverser. D. Both B and C are correct

Question 15

T or F
The Ram Air Turbine (RAT) must be manually deployed? [8.130.10]

Answer 15

B. False

Question 16

The primary hydraulic pump FAULT lights illuminate (amber) when the following occurs: [8.130.20]

Answer 16

A. Low primary pump pressure.
B. Excessive primary pump fluid temperature.
C. Pump Selector to OFF.
D. All the above

Question 17

In the AUTO position, the right hydraulic system demand pump: [8.130.10]

Answer 17

A. Operates from takeoff thrust set to flaps retracted.
B. Operates when system, or primary pump pressure is low. C. Operates with right thrust reverser deployment. D. All of the above

Question 18

Where would you find hydraulic quantity indications? [8.130.20]

Answer 18

B. Status Display.
C. Hydraulic Synoptic.
D. Both B and C