ログイン

A-320 Chapter № 9. Fuel
21問 • 11ヶ月前
  • Popovich
  • 通報

    問題一覧

  • 1

    9.1. Refueling is possible if aircraft batteries are the only source of power.

    True

  • 2

    9.2. With the center tank pump mode SEL switch in AUTO; the center tank pumps:

    B. Run for two minutes after both engines are running

  • 3

    9.3. What is the purpose of a Fuel Tank Inerting System (A320 NEO/A321)?

    C. To reduce the flammability in the center tank

  • 4

    9.4. Refueling of aircraft is available from the:

    A. Right wing only

  • 5

    9.5. Refueling can be performed automatically and manually.

    True

  • 6

    9.6. What is the purpose of surge tank?

    A. To protect the system against overpressure and thermal expansion

  • 7

    9.7. How can you monitor amount of fuel in the surge tank?

    B. It is impossible

  • 8

    9.8. Fuel transfer from the outer tank to the inner tank occurs when:

    A. The inner compartment quantity decreases to 750 kg

  • 9

    9.9. The Fuel Used indication on ECAM is reset:

    B. Automatically at engine start on the ground

  • 10

    9.10. The fuel tanks of A320 CEO/NEO are getting empty in the following sequence:

    A. The center tank, the inner tanks, the outer tanks

  • 11

    9.11. The message CTR TK FEEDG appears in the MEMO. What does this mean?

    C. At least one center tank pump is energized

  • 12

    9.12. An amber line appears across the last two digits of the ECAM FOB indication when:

    A. Fuel quantity indication is inaccurate

  • 13

    9.13. Some of the fuel supplied to each engine goes from the high-pressure fuel line in that engine, through the IDG heat exchanger, to the fuel return back to the outer fuel tank.

    True

  • 14

    9.14. Why do the center tank pumps stop automatically when then slats are extended for takeoff?

    C. To ensure that the engines are fed from the wing tanks for takeoff (feeding segregation)

  • 15

    9.15. After engine shutdown, what are your actions to close the fuel transfer valves?

    C. No action is required. The valves will close automatically during the next refueling

  • 16

    9.16. The green message OUTER TK FUEL XFRD appears on the ECAM MEMO display. What does it mean?

    C. Fuel is transferring from the outer tank to the inner tank

  • 17

    9.17. How does the fuel transfer from the outer to the inner tanks?

    C. The transfer valve is opened automatically by the low level sensor in the inner tank

  • 18

    9.18. How does the fuel from Additional Center Tanks (ACT’s) being used?

    A. The fuel transfers automatically or manually to Center Tanks, then to Wing tanks.

  • 19

    9.19. What is the A321 Fuel Feed Sequence in order from first tank to be deployed to the last one?

    A. ACT, Center Tank, Wing tanks

  • 20

    9.20. The wings of A321 NEO have:

    C. wing tanks and vent surge tanks

  • 21

    9.21. The fuel is stored in the (A321NEO):

    A. the center tank, wing tanks and additional center tanks

  • Аэродинамика ВС

    Аэродинамика ВС

    Popovich · 111問 · 1ヶ月前

    Аэродинамика ВС

    Аэродинамика ВС

    111問 • 1ヶ月前
    Popovich

    A-320 Chapter № 22. Performance; “Fly Smart”.

    A-320 Chapter № 22. Performance; “Fly Smart”.

    Popovich · 14問 · 1ヶ月前

    A-320 Chapter № 22. Performance; “Fly Smart”.

    A-320 Chapter № 22. Performance; “Fly Smart”.

    14問 • 1ヶ月前
    Popovich

    A-320 Chapter № 21. Engines

    A-320 Chapter № 21. Engines

    Popovich · 37問 · 1ヶ月前

    A-320 Chapter № 21. Engines

    A-320 Chapter № 21. Engines

    37問 • 1ヶ月前
    Popovich

    A-320 Chapter № 19. APU

    A-320 Chapter № 19. APU

    Popovich · 17問 · 1ヶ月前

    A-320 Chapter № 19. APU

    A-320 Chapter № 19. APU

    17問 • 1ヶ月前
    Popovich

    A-320 Chapter № 18. Water / Waste

    A-320 Chapter № 18. Water / Waste

    Popovich · 7問 · 1ヶ月前

    A-320 Chapter № 18. Water / Waste

    A-320 Chapter № 18. Water / Waste

    7問 • 1ヶ月前
    Popovich

    A-320 Chapter № 17. Pneumatic

    A-320 Chapter № 17. Pneumatic

    Popovich · 12問 · 1ヶ月前

    A-320 Chapter № 17. Pneumatic

    A-320 Chapter № 17. Pneumatic

    12問 • 1ヶ月前
    Popovich

    A-320 Chapter № 16. Oxygen

    A-320 Chapter № 16. Oxygen

    Popovich · 15問 · 1ヶ月前

    A-320 Chapter № 16. Oxygen

    A-320 Chapter № 16. Oxygen

    15問 • 1ヶ月前
    Popovich

    A-320 Chapter № 15. Navigation and Surveillance

    A-320 Chapter № 15. Navigation and Surveillance

    Popovich · 30問 · 1ヶ月前

    A-320 Chapter № 15. Navigation and Surveillance

    A-320 Chapter № 15. Navigation and Surveillance

    30問 • 1ヶ月前
    Popovich

    A-320 Chapter № 14. Lights

    A-320 Chapter № 14. Lights

    Popovich · 11問 · 1ヶ月前

    A-320 Chapter № 14. Lights

    A-320 Chapter № 14. Lights

    11問 • 1ヶ月前
    Popovich

    A-320 Chapter № 13. Landing gear

    A-320 Chapter № 13. Landing gear

    Popovich · 37問 · 1ヶ月前

    A-320 Chapter № 13. Landing gear

    A-320 Chapter № 13. Landing gear

    37問 • 1ヶ月前
    Popovich

    A-320 Chapter № 12. Indicating / Recording

    A-320 Chapter № 12. Indicating / Recording

    Popovich · 38問 · 1ヶ月前

    A-320 Chapter № 12. Indicating / Recording

    A-320 Chapter № 12. Indicating / Recording

    38問 • 1ヶ月前
    Popovich

    A-320 Chapter № 11. Ice and Rain

    A-320 Chapter № 11. Ice and Rain

    Popovich · 17問 · 1ヶ月前

    A-320 Chapter № 11. Ice and Rain

    A-320 Chapter № 11. Ice and Rain

    17問 • 1ヶ月前
    Popovich

    A-320 Chapter № 10. Hydraulic

    A-320 Chapter № 10. Hydraulic

    Popovich · 17問 · 1ヶ月前

    A-320 Chapter № 10. Hydraulic

    A-320 Chapter № 10. Hydraulic

    17問 • 1ヶ月前
    Popovich

    A-320 Chapter № 9. Fuel

    A-320 Chapter № 9. Fuel

    Popovich · 21問 · 1ヶ月前

    A-320 Chapter № 9. Fuel

    A-320 Chapter № 9. Fuel

    21問 • 1ヶ月前
    Popovich

    A-320 Chapter № 8. Flight Controls

    A-320 Chapter № 8. Flight Controls

    Popovich · 42問 · 1ヶ月前

    A-320 Chapter № 8. Flight Controls

    A-320 Chapter № 8. Flight Controls

    42問 • 1ヶ月前
    Popovich

    A-320 Chapter № 7. Fire protection

    A-320 Chapter № 7. Fire protection

    Popovich · 20問 · 1ヶ月前

    A-320 Chapter № 7. Fire protection

    A-320 Chapter № 7. Fire protection

    20問 • 1ヶ月前
    Popovich

    A-320 Chapter № 6. Equipment

    A-320 Chapter № 6. Equipment

    Popovich · 7問 · 1ヶ月前

    A-320 Chapter № 6. Equipment

    A-320 Chapter № 6. Equipment

    7問 • 1ヶ月前
    Popovich

    A-320 Chapter № 5. Electrical

    A-320 Chapter № 5. Electrical

    Popovich · 26問 · 1ヶ月前

    A-320 Chapter № 5. Electrical

    A-320 Chapter № 5. Electrical

    26問 • 1ヶ月前
    Popovich

    A-320 Chapter № 4. Communication

    A-320 Chapter № 4. Communication

    Popovich · 18問 · 1ヶ月前

    A-320 Chapter № 4. Communication

    A-320 Chapter № 4. Communication

    18問 • 1ヶ月前
    Popovich

    A-320 Chapter № 3. Autoflight

    A-320 Chapter № 3. Autoflight

    Popovich · 40問 · 1ヶ月前

    A-320 Chapter № 3. Autoflight

    A-320 Chapter № 3. Autoflight

    40問 • 1ヶ月前
    Popovich

    問題一覧

  • 1

    9.1. Refueling is possible if aircraft batteries are the only source of power.

    True

  • 2

    9.2. With the center tank pump mode SEL switch in AUTO; the center tank pumps:

    B. Run for two minutes after both engines are running

  • 3

    9.3. What is the purpose of a Fuel Tank Inerting System (A320 NEO/A321)?

    C. To reduce the flammability in the center tank

  • 4

    9.4. Refueling of aircraft is available from the:

    A. Right wing only

  • 5

    9.5. Refueling can be performed automatically and manually.

    True

  • 6

    9.6. What is the purpose of surge tank?

    A. To protect the system against overpressure and thermal expansion

  • 7

    9.7. How can you monitor amount of fuel in the surge tank?

    B. It is impossible

  • 8

    9.8. Fuel transfer from the outer tank to the inner tank occurs when:

    A. The inner compartment quantity decreases to 750 kg

  • 9

    9.9. The Fuel Used indication on ECAM is reset:

    B. Automatically at engine start on the ground

  • 10

    9.10. The fuel tanks of A320 CEO/NEO are getting empty in the following sequence:

    A. The center tank, the inner tanks, the outer tanks

  • 11

    9.11. The message CTR TK FEEDG appears in the MEMO. What does this mean?

    C. At least one center tank pump is energized

  • 12

    9.12. An amber line appears across the last two digits of the ECAM FOB indication when:

    A. Fuel quantity indication is inaccurate

  • 13

    9.13. Some of the fuel supplied to each engine goes from the high-pressure fuel line in that engine, through the IDG heat exchanger, to the fuel return back to the outer fuel tank.

    True

  • 14

    9.14. Why do the center tank pumps stop automatically when then slats are extended for takeoff?

    C. To ensure that the engines are fed from the wing tanks for takeoff (feeding segregation)

  • 15

    9.15. After engine shutdown, what are your actions to close the fuel transfer valves?

    C. No action is required. The valves will close automatically during the next refueling

  • 16

    9.16. The green message OUTER TK FUEL XFRD appears on the ECAM MEMO display. What does it mean?

    C. Fuel is transferring from the outer tank to the inner tank

  • 17

    9.17. How does the fuel transfer from the outer to the inner tanks?

    C. The transfer valve is opened automatically by the low level sensor in the inner tank

  • 18

    9.18. How does the fuel from Additional Center Tanks (ACT’s) being used?

    A. The fuel transfers automatically or manually to Center Tanks, then to Wing tanks.

  • 19

    9.19. What is the A321 Fuel Feed Sequence in order from first tank to be deployed to the last one?

    A. ACT, Center Tank, Wing tanks

  • 20

    9.20. The wings of A321 NEO have:

    C. wing tanks and vent surge tanks

  • 21

    9.21. The fuel is stored in the (A321NEO):

    A. the center tank, wing tanks and additional center tanks