A 320 Sys Fuel // Fight Controls

40 Questions | Total Attempts: 11

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A 320 Sys Fuel // Fight Controls

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Questions and Answers
  • 1. 
    What is the total fuel capacity of the A320n?
    • A. 

      27500 lbs.

    • B. 

      41,285 lbs.

    • C. 

      52,000 lbs.

  • 2. 
    With fuel in the center tank the CTR TK MODE SEL push button selected to AUTO and CTR TK PUMP push button ON (lights out ) which of the following conditions cause the center tank fuel pumps to stop ?
    • A. 

      Extension of the slats (after completion of the test cycle )

    • B. 

      Anytime the slats are extended or an overfill condition is detected in either wing inner cell ,

    • C. 

      Both are correct.

  • 3. 
    Fuel can be transferred from tank to tank ?
    • A. 

      Only on the ground.

    • B. 

      In flight if the fuel X FEED push button is selected OPEN .

    • C. 

      In flight if the fuel XFEED push button is selected OPEN  and center tank MODE SEL push button is selected to MAN.

  • 4. 
    From which tanks will fuel gravity feed ?
    • A. 

      Outer cell of the wing tanks , inner cell of the wing tanks , and / or center tank.

    • B. 

      Inner cell of the wing tanks , and center tank.

    • C. 

      Outer cell of the wing tanks , and inner cell of the wing tanks .

  • 5. 
    What precaution should you observe when gravity feeding fuel ?
    • A. 

      Operate the aircraft bellow 15,000 feet.

    • B. 

      Use center tank first.

    • C. 

      Open the crossfeed when above FL250.

  • 6. 
    Which of the following would cause the fault light to illuminate on the MODE SEL push button ?
    • A. 

      Fuel is being burned out of sequence.

    • B. 

      Crossfeed push button is ON.

    • C. 

      Center tank pumps do not stop after slat extension.

  • 7. 
    During normal operation when should the fuel transfer valves open ?
    • A. 

      When low level is sensed in either inner wing cell .

    • B. 

      When a low level is sensed in either outer wing cell.

    • C. 

      When a low level is sensed in the center tank.

  • 8. 
    The wing fuel transfer valves are :
    • A. 

      Are electrically held closed.

    • B. 

      Manually controlled and open when the MODE SEL push button is selected to MAN.

    • C. 

      Open automatically at the start of the refueling .

  • 9. 
    The APU fuel system :
    • A. 

      Obtains fuel from either center tank pump.

    • B. 

      Uses it´s own dedicated DC powered fuel pump.

    • C. 

      Obtains fuel from the left fuel manifold via the left side fuel pumps or if needed the APU fuel pump.

  • 10. 
    Can the position of the wing fuel transfer valves be checked ?
    • A. 

      Tes , only on the refueling panel .

    • B. 

      It is not possible to determine their position.

    • C. 

      Only on the ECAM fuel page.

  • 11. 
    Which of the following statements is correct concerning the elevator aileron computers (ELAC´S)
    • A. 

      Three computers which achieve normal elevator ,stabilizer and aileron control.

    • B. 

      Two computers which achieve normal and standby control of the elevators ailerons ,and trimmabe horizontal stabilizer.

    • C. 

      Three computers which achieve normal and standby control of the elevators ,ailerons and THS.

  • 12. 
    What happens in the event of an single ELAC failure ?
    • A. 

      ELAC functions are transferred to FAC´s.

    • B. 

      SEC functions are transferred the ELAC´s.

    • C. 

      The functions of the failed ELAC will be assumed by the remaining ELAC.

  • 13. 
    Which of the following statements is correct concerning the spoiler elevator computers (SEC´S) ?
    • A. 

      Two computers which achieve spoiler control and standby elevator and THS control.

    • B. 

      Three computers which achieve spoiler control and normal elevator and THS control.

    • C. 

      Three computers which achieve spoiler control and standby elevator and THS control.

  • 14. 
    The FAC´S primary control which control surface ?
    • A. 

      Elevator.

    • B. 

      Rudder.

    • C. 

      Aileron .

  • 15. 
    If both FAC´S fail ,what happens to the rudder limiter ?
    • A. 

      It immediately assumes the low speed position .

    • B. 

      It freezes at its present position and assumes the low speed position when flaps 1 are selected.

    • C. 

      Maximum rudder deflection can be obtained after slats extended.

  • 16. 
    Which of the following control surfaces can be mechanically controlled ?
    • A. 

      Speed brakes and flaps.

    • B. 

      THS and flaps. 

    • C. 

      THS and rudder .

  • 17. 
    Mechanically backed up control surfaces :
    • A. 

      Are mechanically connected to the cockpit controls.

    • B. 

      Required hydraulic power for actuation .

    • C. 

      Both A and B .

  • 18. 
    Which of the following will automatically reset after landing ?
    • A. 

      Rudder trim.

    • B. 

      THS.

    • C. 

      Both A and B.

  • 19. 
    Which of the following statements are correct concerning the side stick takeover push button ?
    • A. 

      If the takeover push button is depressed for more than 40 seconds , the onside system will retain priority after the push button is realeased.

    • B. 

      The last pilot to depress the push button has priority.

    • C. 

      Both A and B 

  • 20. 
    Which of the following control surfaces can be mechanically controlled ?
    • A. 

      Speed brakes and flaps.

    • B. 

      THS and flaps

    • C. 

      THS and rudder.

  • 21. 
    Mechanically backed up control surfaces ?
    • A. 

      Are mechanically connected to the cockpit controls .

    • B. 

      Require hydraulic power for action.

    • C. 

      Both A and B .

  • 22. 
    Which of the following statements are correct concerning the side stick takeover push button?
    • A. 

      If the takeover push button is depressed for more than 40 seconds . the onside system will retain priority after the push is released.

    • B. 

      The last pilot to depress the push button has priority.

    • C. 

      Both A and B

  • 23. 
    When ground spoilers deploy automatically :
    • A. 

      All ten spoilers panels fully deploy .

    • B. 

      Four spoiler panel on each wing deploy.

    • C. 

      All ten spoiler panels deploy half way.

  • 24. 
    Which of the following controls and monitors flaps and slats ?
    • A. 

      Wing tip brakes.

    • B. 

      One slat flap control computer (SFCC)

    • C. 

      Two slat flap control computers (SFCC´s )

  • 25. 
    The wing tip brakes active :
    • A. 

      For slat and for flap overspeed ,asymmetry or symmetrical runaway.

    • B. 

      For asymmetry or symmetrical runaway.

    • C. 

      For high altitude protection.

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