A 320 Sys Autopilot

38 Questions | Total Attempts: 15

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A 320 Sys Autopilot

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Questions and Answers
  • 1. 
    In normal law , pitch and roll attitude limits depicted on each pilots PFD 
    • A. 

      Are displayed as green x´s

    • B. 

      Are displayed as green =´s

    • C. 

      Are never displayed and must be memorized by each pilots PFD

  • 2. 
    In normal law Mmo and Vmo limits depicted on each pilots PFD
    • A. 

      Are displayed as green x´s

    • B. 

      Are displayed as green =´s

    • C. 

      Are never displayed and must be memorized by eachA 320 pilot

  • 3. 
    In normal Law the low speed limits depicted on each pilots PFD
    • A. 

      Are displayed as green x´s

    • B. 

      Are displayed as green =´s

    • C. 

      Are displayed as Alpha port and Alpha max .These limits vary with GW ,CG, altitude and other environment factor.

  • 4. 
    While in flight operating in normal law , movement of the sidesitck and subsequent return to neutral will command.
    • A. 

      The control surface to continue rolling the aircraft until reaching 55 degrees roll angle.

    • B. 

      Control surface movements proportional to stick deflection, disconnected auto trim, and maintain its current attitude.

    • C. 

      A load factor proportional to stick deflection , then maintain one G flight corrected for pitch attitude 

  • 5. 
    Which inflight operating in normal Law in the Alpha port range :
    • A. 

      The flight controls revert in Direct Law

    • B. 

      The side stick controller and flight controls revert to the AOA mode , and side stick deflection is proportional to AOA

    • C. 

      The fight controls remain in the load factor demand law

  • 6. 
    While inflight operating in Normal law , in the Alpha prot range :
    • A. 

      The flight controls revert to Direct Law

    • B. 

      The side stick controller and flight controls revert to the AOA mode , and side stick deflection is proportional to AOA.

    • C. 

      The flight controls remain in the load factor demand law .

  • 7. 
    Which statement best describes protective limit symbols depicted on the pilots PFD while in alternate law ?
    • A. 

      All limit symbols are removed from the pilots PFDs

    • B. 

      Greens =´s are depicted with amber x´s .Alpha prot and Alpha Max are replaced by Vls and Vs

    • C. 

      Are never displayed and must be memorized by each A320 pilot

  • 8. 
    In normal Law all predictions are active , wich of the following lists the most complete list ?
    • A. 

      Protections , Load Factor , Pitch attitude , High AOA , Alpha floor , ange of bank ad high speed.

    • B. 

      Protections , Load factor , Pitch attitude , High AOA and High speed.

    • C. 

      Protections , Load factor , Pitch attitude , high AOA , Vls , alpha floor and High speed.

  • 9. 
    Which protection is not available below 100´AGl
    • A. 

      Alpha speed

    • B. 

      Vls

    • C. 

      Alpha floor

  • 10. 
    When in alternate law , all protections except ,,,,,,,,,,,,,,,,,,,,,, protection will be lost 
    • A. 

      Pitch attitude

    • B. 

      Bank angle

    • C. 

      Load factor

  • 11. 
    High and low speed stabilities maybe available in alternate law stabilities 
    • A. 

      Will not allow the pilot to stall the aircraft

    • B. 

      Prohibit steep bank angles

    • C. 

      Can be overridden by the pilot , and it is posible to exceed Vmo, Mmo and stall the aircraft

  • 12. 
    Which of the following statements is always true when operating in alternate law ?
    • A. 

      Extending the landing gear will place the aircraft in mechanical back up law

    • B. 

      Extending the landing gear will place the aircraft in direct law

    • C. 

      Extending the landing Gear will have not effect on the status of the flight controls 

  • 13. 
    What is the function of the FAC,,s ? 1) Rudder and yaw damping . 2) Flight envelope and Speed computations .  3) Windshear protection
    • A. 

      1 y 2

    • B. 

      1 y 3

    • C. 

      1, 2 y 3

  • 14. 
    What does amber SPEED BREAKS mean on lower ECAM ?
    • A. 

      Speed brakes are extended and flap handle is not at 0

    • B. 

      Speed brake have a fault

    • C. 

      Speed brakes are extended and engines are not at Idle

  • 15. 
    If both ELAC.s fail , what controls the elevator and stabilizer ?
    • A. 

      SEC´s

    • B. 

      FAC,s

    • C. 

      Nothing they revert to mechanical back up.

  • 16. 
    The DDRMI provides the pilot with :
    • A. 

      Bearing and DME information for VOR 1 and  ADF 1

    • B. 

      Bearing and DME information for VOR 2 and ADF 2

    • C. 

      Bearing only for VOR 1 and VOR 2

  • 17. 
    The ATT HDG and AIR DATA selectors on the switching panel in the Norm position indicate that :
    • A. 

      ADIRU 1 is supplying information to PFD 1 and ND2 and ADIRU 2 is supplying power to PFD 2 and ND 1

    • B. 

      ADIRU 1supplying information to PFD 1, ND 1 and the DDRMI, ADIRU 2 is supplying power to PFD 2 and ND 2

    • C. 

      None of the above

  • 18. 
    Placing on of the ADR push buttons OFF will accomplish what ?
    • A. 

      The off light will iluminate and are data output will disconnect 

    • B. 

      The respective ADIRU will become deenergized

    • C. 

      Both AD and IR information will be disconnected

  • 19. 
    What action should be taken if ADR 1 is lost ?
    • A. 

      Nothing

    • B. 

      Move the ATT HDG knob on the switching panel to Cast 3

    • C. 

      Move the AIR DATA knob on the switching panel to Cast 3

  • 20. 
    What information is supplied by the Air data Modules ADM´s and displayed on the PFD´s ?
    • A. 

      Heading , altitude and vertical speed

    • B. 

      Airspeed ,vertical speed and altitude

    • C. 

      Airspeed , altitude ,and back up vertical speed

  • 21. 
    What information is supplied by the IR´s and displayed on the PFD ?
    • A. 

      Heading , altitude and vertical speed.

    • B. 

      Heading , altitude and vertical speed.

    • C. 

      Airspeed , altitude and backup vertical speed.

  • 22. 
    What causes a DU to display a black screen with a white diagonal line ?
    • A. 

      No power

    • B. 

      DMC failure 

    • C. 

      The circuit breaker for that particular DU has popped

  • 23. 
    After a single DMC failure , how could a crew member recover the display unit ?
    • A. 

      Once a DMC has failed the information is unrecoverable

    • B. 

      Rotate  the EIS DMC switch on the switching panel to replace the failed DMC with DMC 3

    • C. 

      No action is needed as recovery is automatic

  • 24. 
    Is the LOWER ECAM DU fails , is there a way to retrieve that information ?
    • A. 

      Pressing and holding the related system page pb on the ECAM control panel , the page will be displayed on the UPPER ECAM .

    • B. 

      Rotating the ECAM/ND XFER switch , the LOWER ECAM page will be transferred to either the Cap or the FO BND

    • C. 

      Both A and B

  • 25. 
    Where is the information displayed by DMC 1 and DMC 2 ?
    • A. 

      ADMC 1 supplies data to PFD 1 ,ND 1 and LOWER ECAM supplies data for PFD 2 ND 2 and UPPER ECAM

    • B. 

      DMC 1 supplies data to PFD 2 ND 2 and LOWER ECAM supplies data for PFD 1 ND 1 and LOWER ECAM

    • C. 

      DMC 1 supplies data to PFD 1 and UPPER ECAM , DMC 2 supplies data for PFD 2 ,ND 2 and LOWER ECAM.

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