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Noor 1
25問 • 5ヶ月前
  • ユーザ名非公開
  • 通報

    問題一覧

  • 1

    1. Main and nose wheel bays are:

    b. unpressurized

  • 2

    2. Normal maximum negative differential pressure is:

    a. when atmospheric pressure exceeds cabin pressure by the amount permitted by the system controls

  • 3

    3. When would the negative differential limit be reached/exceeded?

    a. Rapid descent when AC descends below cabin altitude

  • 4

    4. A/C in level flight: if cabin altitude increases, pressure diff:

    b. decreases

  • 5

    5. In level pressurized flight what does the outflow valve do?

    b. Adjust to provide constant flow, and is normally partially open

  • 6

    6. In a turbo-compressor or bootstrap system the cooling air is:

    a. ram air

  • 7

    7. The rate of change of cabin pressure should be kept to the minimum. This is more important:

    a. in descent

  • 8

    8. A cabin humidifier is used:

    b. at high altitude

  • 9

    9. Fatigue life of the fuselage is based on the:

    a. number of pressurization cycles

  • 10

    10. If the forward oil seal in an axial flow compressor fails, cabin air will be:

    a. contaminated

  • 11

    11. Rate of change of cabin altitude is shown on a:

    a. special gauge

  • 12

    12. Cabin discharge valve (pneumatic) is supplied with:

    b. cabin and static pressure

  • 13

    13. What is the purpose of the duct relief valve?

    c. To prevent damage to the ducts

  • 14

    14. What system is installed to control the air conditioning?

    b. Impingement type dehydrator and humidifier

  • 15

    15. How is the (charge) air cooled in a bootstrap (turbo-compressor) system?

    b. By expanding over turbine driving compressor

  • 16

    16. At the max differential phase, the discharge phase is:

    a. open

  • 17

    17. What is the purpose of inward relief valves?

    a. To prevent negative differential

  • 18

    18. On a ground pressurization test, if the cabin suffers a rapid de-pressurization:

    b. water precipitation will occur

  • 19

    19. A heat exchanger functions by:

    c. passing charge air through ducts and cool air around ducts

  • 20

    20. Maximum differential pressure:

    a. is the maximum authorized pressure difference between the inside of the fuselage and the atmospheric ambient pressure

  • 21

    21. A humidifier is fitted to:

    c. increase the moisture content in the air when operating at high altitude

  • 22

    22. If the discharge or outflow valve closes:

    c. the safety valve would limit the positive pressure difference

  • 23

    23. Air for conditioning and pressurization is taken from:

    a. the engine compressor or cabin compressor

  • 24

    24. Safety valves are biased:

    a. inwards

  • 25

    25. Cabin compressors:

    c. increase their flow in proportion to increases of altitude differential pressure and reduction in engine rpm in order to maintain the mass flow

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    問題一覧

  • 1

    1. Main and nose wheel bays are:

    b. unpressurized

  • 2

    2. Normal maximum negative differential pressure is:

    a. when atmospheric pressure exceeds cabin pressure by the amount permitted by the system controls

  • 3

    3. When would the negative differential limit be reached/exceeded?

    a. Rapid descent when AC descends below cabin altitude

  • 4

    4. A/C in level flight: if cabin altitude increases, pressure diff:

    b. decreases

  • 5

    5. In level pressurized flight what does the outflow valve do?

    b. Adjust to provide constant flow, and is normally partially open

  • 6

    6. In a turbo-compressor or bootstrap system the cooling air is:

    a. ram air

  • 7

    7. The rate of change of cabin pressure should be kept to the minimum. This is more important:

    a. in descent

  • 8

    8. A cabin humidifier is used:

    b. at high altitude

  • 9

    9. Fatigue life of the fuselage is based on the:

    a. number of pressurization cycles

  • 10

    10. If the forward oil seal in an axial flow compressor fails, cabin air will be:

    a. contaminated

  • 11

    11. Rate of change of cabin altitude is shown on a:

    a. special gauge

  • 12

    12. Cabin discharge valve (pneumatic) is supplied with:

    b. cabin and static pressure

  • 13

    13. What is the purpose of the duct relief valve?

    c. To prevent damage to the ducts

  • 14

    14. What system is installed to control the air conditioning?

    b. Impingement type dehydrator and humidifier

  • 15

    15. How is the (charge) air cooled in a bootstrap (turbo-compressor) system?

    b. By expanding over turbine driving compressor

  • 16

    16. At the max differential phase, the discharge phase is:

    a. open

  • 17

    17. What is the purpose of inward relief valves?

    a. To prevent negative differential

  • 18

    18. On a ground pressurization test, if the cabin suffers a rapid de-pressurization:

    b. water precipitation will occur

  • 19

    19. A heat exchanger functions by:

    c. passing charge air through ducts and cool air around ducts

  • 20

    20. Maximum differential pressure:

    a. is the maximum authorized pressure difference between the inside of the fuselage and the atmospheric ambient pressure

  • 21

    21. A humidifier is fitted to:

    c. increase the moisture content in the air when operating at high altitude

  • 22

    22. If the discharge or outflow valve closes:

    c. the safety valve would limit the positive pressure difference

  • 23

    23. Air for conditioning and pressurization is taken from:

    a. the engine compressor or cabin compressor

  • 24

    24. Safety valves are biased:

    a. inwards

  • 25

    25. Cabin compressors:

    c. increase their flow in proportion to increases of altitude differential pressure and reduction in engine rpm in order to maintain the mass flow