A-320 Chapter № 10. Hydraulic

17問 • 11ヶ月前

Popovich

通報

問題一覧

10.1. Which hydraulic systems have EDP?

B. Green and Yellow

10.2. Which hydraulic system can be pressurized by RAT?

A. Blue

10.3. The hand pump supplies yellow system pressure to the:

B. Alternate brakes

10.4. The PTU enables:

A. The green and yellow system to pressurize each other automatically

10.5. Which hydraulic system provides power for gear extension/retraction.

C. Green

10.6. The aircraft's three hydraulic systems are normally pressurized by:

A. Two engine driven pumps and one electric pump

10.7. Which hydraulic system is normally pressurized by the electric pump?

C. Blue

10.8. The aircraft has three continuously operating hydraulic systems. Normal system operating pressure is:

C. 3000PSI

10.9. Hydraulic system pressure when powered by the RAT is:

A. 2500PSI

10.10. Hydraulic fluid can be transferred from one system to another.

False

10.11. The PTU runs automatically when ΔP between YELLOW and GREEN hydraulic systems is more than 500 psi:

True

10.12. Normally, air from ______ pressurizes hydraulic reservoirs.

A. engine 1

10.13. The hydraulic reservoirs maintain a high pressure to prevent their pumps from:

A. cavitation

10.14. The RAT is capable of powering a pump which will pressurize:

A. BLUE HYD system

10.15. How can the YELLOW hydraulic system be pressurized?

A. An engine driven pump, an electric pump, the PTU using the green system and a hand pump for the cargo doors

10.16. The flight crew pushes RAT MAN ON switch on hydraulic panel. How can be it stowed?

C. It can be stowed only when the aircraft is on the ground

10.17. Which combination of DUAL HYDRAULIC systems LO PR failure will leave Flight Controls in NORMAL LAW?

C. B+Y

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問題一覧

10.1. Which hydraulic systems have EDP?

B. Green and Yellow

10.2. Which hydraulic system can be pressurized by RAT?

A. Blue

10.3. The hand pump supplies yellow system pressure to the:

B. Alternate brakes

10.4. The PTU enables:

A. The green and yellow system to pressurize each other automatically

10.5. Which hydraulic system provides power for gear extension/retraction.

C. Green

10.6. The aircraft's three hydraulic systems are normally pressurized by:

A. Two engine driven pumps and one electric pump

10.7. Which hydraulic system is normally pressurized by the electric pump?

C. Blue

10.8. The aircraft has three continuously operating hydraulic systems. Normal system operating pressure is:

C. 3000PSI

10.9. Hydraulic system pressure when powered by the RAT is:

A. 2500PSI

10.10. Hydraulic fluid can be transferred from one system to another.

False

10.11. The PTU runs automatically when ΔP between YELLOW and GREEN hydraulic systems is more than 500 psi:

True

10.12. Normally, air from ______ pressurizes hydraulic reservoirs.

A. engine 1

10.13. The hydraulic reservoirs maintain a high pressure to prevent their pumps from:

A. cavitation

10.14. The RAT is capable of powering a pump which will pressurize:

A. BLUE HYD system

10.15. How can the YELLOW hydraulic system be pressurized?

A. An engine driven pump, an electric pump, the PTU using the green system and a hand pump for the cargo doors

10.16. The flight crew pushes RAT MAN ON switch on hydraulic panel. How can be it stowed?

C. It can be stowed only when the aircraft is on the ground

10.17. Which combination of DUAL HYDRAULIC systems LO PR failure will leave Flight Controls in NORMAL LAW?

C. B+Y