A320 Bank

25 Questions

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Bank Quizzes & Trivia

Quiz areas includes:- General questions; Air conditioning and pressurisation; Automatic Flight; Auxiliary Power Unit; Communications; Electrical; Energy Equipment; Fire Protection; Flight Controls; Flight Instruments; Fuel; Hydraulic Power; Ice and Rain Protection; Landing Gear; Navigation; Pneumatics; Power Plant; Limitations; Minimum Equipment List; Emergency Procedures; Low Visibility; EIS and FMS


Questions and Answers
  • 1. 
    Which lights go off when the gear is retracted
    • A. 

      Nose and Turn Off

    • B. 

      Turn Off and Wing

    • C. 

      Nose and Land

    • D. 

      Logo and Land

  • 2. 
    Which colour code is correct for push button switches?
    • A. 

      AMBER - immediate action : BLUE - temporary operation

    • B. 

      GREEN - temporary operation : WHITE - abnormal position

    • C. 

      WHITE - temporary operation : GREEN - normal operation

    • D. 

      RED - immediate action : 2 DOTS "not used" part of switch

  • 3. 
    "Below the passenger door window is a red CABIN PRESSURE light which ...
    • A. 

      ... flashes if there is residual cabin pressure."

    • B. 

      ... is illuminated whenever the cabin pressure is greater than 2.5 mb."

    • C. 

      ... flashes with residual pressure and slides armed."

    • D. 

      ... cannot be seen from outside the aircraft."

  • 4. 
    "Set on LO, the actual pack flow may be ...
    • A. 

      ... HI due to APU bleed supplying."

    • B. 

      ... NORM due to APU bleed supplying."

    • C. 

      ... HI due to air conditioning temperature demands."

    • D. 

      ... NORM or HI due to single ack operation."

  • 5. 
    "The MAN V/S CTL switch is ...
    • A. 

      ...operative at all times, and it controls the outflow valve."

    • B. 

      ... operative in the MAN pressurisation mode: - hold up to OPEN the outflow valve."

    • C. 

      ... operative in the MAN pressurisation mofe: - hold up to OPEN the safety valve."

    • D. 

      ... inoperative if the DITCHING switch is ON."

  • 6. 
    • A. 

      "ALTN MODE"

    • B. 

      "PACK REG"

    • C. 

      Double crosses ( XX )

    • D. 

      "TRIM AIR VALVE FAULT"

  • 7. 
    • A. 

      Initial cooling of air after entering the pack.

    • B. 

      Cooling H.P. air only.

    • C. 

      Cooling bleed air in accordance with pack demands.

    • D. 

      Cooling bleed air to a maximum of 200℃.

  • 8. 
    The Trim Air Valves:
    • A. 

      Are electrically controlled by the zone controller.

    • B. 

      Adjusts temperature by adding cold air.

    • C. 

      Mix fresh air from the packs with recirculated cabin air.

    • D. 

      Regulate pack flow depending on number of passengers.

  • 9. 
    With the PACK FLOW selector to NORM, what will the actual flow be?
    • A. 

      LO or NORM or HI.

    • B. 

      Always NORM.

    • C. 

      NORM or HI.

    • D. 

      NORM or LO.

  • 10. 
    The Avionics Vent System has two "conditions" - GROUND  and FLIGHT.  When does the transition from GROUND to FLIGHT occur?
    • A. 

      After second engine start.

    • B. 

      At lift-off.

    • C. 

      At 100 kts. on the take-off roll.

    • D. 

      When the thrust is set for take-off.

  • 11. 
    Regarding the A/THR indications on the FMA, which is true?
    • A. 

      ATHR in blue - [ ARMED (actual thrust = TLA) ]

    • B. 

      ATHR in white - [ ARMED (actual thrust = TLA) ]

    • C. 

      ATHR in blue - [ ACTIVE (actual thrust is limited by TLA) ]

    • D. 

      ATHR in white - [ ACTIVE (actual thrust is always less than TLA) ]

  • 12. 
    • A. 

      After the APPROACH PHASE is activated on the MCDU.

    • B. 

      After APPR is armed on the FCU.

    • C. 

      After LOC capture.

    • D. 

      After G/S capture.

  • 13. 
    The APU has been switched off, but it has not stopped .  Why is this?
    • A. 

      The APU Fuel Pump continuing to run.

    • B. 

      The Air Intake Flap failing to close.

    • C. 

      A cooling period, which occurs on all APU shutdowns.

    • D. 

      A cooling period (following use of APU Bleed).

  • 14. 
    "The  APU may be started ...
    • A. 

      ... at or below 35,000 feet only."

    • B. 

      ... at or below 25,000 feet only."

    • C. 

      ... at or below 300 knots only."

    • D. 

      ...throughout the normal flight envelope."

  • 15. 
    • A. 

      The APU Intake Flap opens and the starter motor engages immediately

    • B. 

      The APU Intake Flap opens and the starter motor engages when the flap is fully open.

    • C. 

      The APU Fuel Pump will operate.

    • D. 

      The APU Intake Flap opens.

  • 16. 
    • A. 

      APU starter disengagement.

    • B. 

      APU electrical power can be used.

    • C. 

      N speed greater than 75%

    • D. 

      ECB power-up check is satisfactory.

  • 17. 
    • A. 

      When the FLAP is fully open and the start switch is pressed on.

    • B. 

      When the Oil Pressure reaches 7 p.s.i.

    • C. 

      When the MASTER SW is pressed on.

    • D. 

      When the START SW is pressed on.

  • 18. 
    On the overhead, when should AUDIO SWITCHING be selected to CAPT 3?
    • A. 

      The Captain is using RMP tuning of the NAVAIDS.

    • B. 

      The Captain's ACP has failed.

    • C. 

      The Captain's loudspeaker has failed.

    • D. 

      Both RMPs have failed.

  • 19. 
    For the ACP, which is true?
    • A. 

      The PA TRANSMISSION key operates like other transmission keys.

    • B. 

      The ON VOICE key enables audio to be heard on the loudspeakers.

    • C. 

      The RESET key transfers associated ACP (1 or 2) operation to ACP3

    • D. 

      The RESET key cancels all CALL lights.

  • 20. 
    On the ACP, what does an amber light on a Transmission Key indicate?
    • A. 

      Failure of the associated transmitter.

    • B. 

      Failure of the associated transmitter and receiver.

    • C. 

      SELCAL operation only.

    • D. 

      SELCAL operation or a call from maintenance or the cabin.

  • 21. 
    • A. 

      Switch it off : use ACP 2

    • B. 

      Switch it off : use RMP 3 only.

    • C. 

      Switch it off : use RMP 3 or RMP 2.

    • D. 

      Use the AUDIO SWITCHING switch (on the overhead panel)

  • 22. 
    Which is true of the AC ESS Bus in the event of an AC BUS 1 FAULT?
    • A. 

      It cannot be powered.

    • B. 

      It can be powered from AC BUS 2, if so selected.

    • C. 

      It will be powered automatically from AC BUS 2.

    • D. 

      It will be powered by the emergency generator.

  • 23. 
    • A. 

      Fuel pump operation is transferred to AC ESS BUS.

    • B. 

      GEN 1 is fed directly onto the AC ESS BUS.

    • C. 

      GEN 1 is de-energised.

    • D. 

      GEN 1 is line contactor opens.

  • 24. 
    • A. 

      The Emergency Generator will be driven by the Blue Hydraulic System.

    • B. 

      The Emergency Generator will be driven directly by the RAT.

    • C. 

      The RAT will not deploy.

    • D. 

      The RAT will extend, but the Emergency Generator will not operate.

  • 25. 
    The aircraft is on the chocks.  All sources (Engine, APU and External Power) are ON. Which of the following is true?
    • A. 

      The External Power is supplying the network.

    • B. 

      If the Engines are shut down, the APU will supply the network.

    • C. 

      If the Engines are shut down, External Power will supply the network.

    • D. 

      If the APU is shut down, the External Power will supply the network.