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A-320 Chapter № 8. Flight Controls
42問 • 11ヶ月前
  • Popovich
    • 通報

    問題一覧

  • 1

    8.1. Which of the following statements is always true when operating in alternate law?

    A. Extending the landing gear will place the aircraft in direct law

  • 2

    8.2. Can the aircraft be controlled with a loss of all electrics?

    Yes

  • 3

    8.3. The amber SPEED BRK is pulsing on the EWD. What does it mean?

    C. Speed brakes are extended and engines are not at idle

  • 4

    8.4. Which computer normally commands the operation of the elevators and horizontal stabilizer?

    C. ELAC 2

  • 5

    8.5. Sidesticks provide electrical signals to the flight control computers. If both sidesticks are operated:

    B. Both inputs are algebraically added

  • 6

    8.6. When the flaps are extended, the ailerons (A320):

    C. Droop 5 degrees

  • 7

    8.7. When the flaps are extended, the ailerons (A321):

    B. Droop 10 degrees

  • 8

    8.8. Two control surfaces that have mechanical backup are:

    B. THS and rudder

  • 9

    8.9. Horizontal stabilizer trim automatically resets to zero degrees after landing.

    True

  • 10

    8.10. What will happen with flaps or slats in case of asymmetry or overspeed?

    A. Flaps or slats will be locked by wing tip brakes

  • 11

    8.11. In Pitch Normal Law and Flight Mode the Pitch Trim is:

    C. Automatic regardless of autopilot status

  • 12

    8.12. TOGA thrust is provided regardless of thrust levers position when ____ protection is active.

    C. Alpha Floor

  • 13

    8.13. Minimum, maximum and maneuvering speeds indicated on PFD in flight are provided by:

    A. FAC

  • 14

    8.14. Speeds indicated on MCDU PERF pages in flight and on the ground are calculated by:

    A. FMGC

  • 15

    8.15. The Flight Control Flight Mode changes to Flare Mode when the aircraft passes:

    A. 50 ft RA for A320, 100 ft RA for A321

  • 16

    8.16. How does the flight control Flare Mode operate when the aircraft descends through 30ft RA (A320):

    A. the system begins to reduce the pitch attitude to 2 ° nose down over a period of 8s

  • 17

    8.17. If the pilot maintains sidestick full forward, the aircraft will:

    C. Significantly overshoot VMO/MMO. At approximately VMO+16 / MMO+0.04, the pitch nose-down authority smoothly reduces to zero

  • 18

    8.18. When does the Flight Control Flight Mode become active?

    B. From liftoff during takeoff until Flare Mode engages at landing

  • 19

    8.19. Roll control in NORMAL LAW is achieved by:

    C. Ailerons and spoilers 2,3,4,5 on each wing

  • 20

    8.20. In normal law, what is the maximum bank angle you can reach with the side stick fully deflected?

    B. 67°

  • 21

    8.21. Rudder deflection will depend on speed

    True

  • 22

    8.22. Maximum rudder deflection is reached at:

    B. LO SPEED

  • 23

    8.23. How many slat surfaces per wing are available?

    5

  • 24

    8.24. How many flap surfaces per wing are available?

    2

  • 25

    8.25 Each wing of A321 NEO has the following lift augmentation devices:

    A. two double-slotted flap surfaces

  • 26

    8.26. How many speed brake surfaces available per wing?

    B. 3 (spoilers 2, 3 and 4)

  • 27

    8.27. What will be speedbrakes surface deflection with autopilot engaged and speedbrake lever in full back position?

    A. ½ for A320, full for A321

  • 28

    8.29. When both main landing gear is compressed:

    B. All ground spoilers will fully deploy

  • 29

    8.30. How many ground spoiler surfaces available per wing?

    5

  • 30

    8.31. MAN PITCH TRIM ONLY red message on PFD indicates that aircraft is in:

    B. Mechanical Back-up

  • 31

    8.32. USE MAN PITCH TRIM amber message on PFD indicates that aircraft is in:

    C. Direct law

  • 32

    8.33. How can you recognize that the aircraft is in Alternate law by inspecting PFD indications:

    A. Amber crosses (X) will replace green double bars “=” on the PFD. Va prot and Va max indications are replaced by Stall Warning Speed (Vsw), which is defined by the top of a red and black strip along the speed scale

  • 33

    8.34. Low speed stability. Aural alert “STALL” will NOT be activated in the _____ law

    C. Normal law

  • 34

    8.35. If both ELACs fail, what controls the elevator and stabilizer?

    B. SECs

  • 35

    8.36. When does the sideslip indicator change to a blue Beta target?

    A. CONF1, 2 or 3 is selected, and any engine N1>80%, and the difference between the engines N1’s exceeds 35%

  • 36

    8.37. High and low speed stability may be available in alternate law.

    True

  • 37

    8.38. With autopilot engaged, either sidestick can be moved freely.

    B. False, applying force on either sidestick beyond predetermined threshold will cause the autopilot(s) to disengage

  • 38

    8.39. Flight Control system Rotation Mode is active:

    B. From 70kt during takeoff roll until 10s after liftoff and pitch attitude is above 8°

  • 39

    8.40. Flight Control system Rotation Mode is designed to:

    B. minimize risk of a tailstrike during takeoff

  • 40

    8.41. The load alleviation function (LAF) permits to alleviate:

    A. the wing structure loads

  • 41

    8.42. The LAF is available when the aircraft is:

    A. in Clean configuration and in Normal Law

  • 42

    8.43. The function of LAF is achieved through the upward deflection of:

    A. two ailerons only, or two ailerons associated to the spoilers 4 and 5

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    問題一覧

  • 1

    8.1. Which of the following statements is always true when operating in alternate law?

    A. Extending the landing gear will place the aircraft in direct law

  • 2

    8.2. Can the aircraft be controlled with a loss of all electrics?

    Yes

  • 3

    8.3. The amber SPEED BRK is pulsing on the EWD. What does it mean?

    C. Speed brakes are extended and engines are not at idle

  • 4

    8.4. Which computer normally commands the operation of the elevators and horizontal stabilizer?

    C. ELAC 2

  • 5

    8.5. Sidesticks provide electrical signals to the flight control computers. If both sidesticks are operated:

    B. Both inputs are algebraically added

  • 6

    8.6. When the flaps are extended, the ailerons (A320):

    C. Droop 5 degrees

  • 7

    8.7. When the flaps are extended, the ailerons (A321):

    B. Droop 10 degrees

  • 8

    8.8. Two control surfaces that have mechanical backup are:

    B. THS and rudder

  • 9

    8.9. Horizontal stabilizer trim automatically resets to zero degrees after landing.

    True

  • 10

    8.10. What will happen with flaps or slats in case of asymmetry or overspeed?

    A. Flaps or slats will be locked by wing tip brakes

  • 11

    8.11. In Pitch Normal Law and Flight Mode the Pitch Trim is:

    C. Automatic regardless of autopilot status

  • 12

    8.12. TOGA thrust is provided regardless of thrust levers position when ____ protection is active.

    C. Alpha Floor

  • 13

    8.13. Minimum, maximum and maneuvering speeds indicated on PFD in flight are provided by:

    A. FAC

  • 14

    8.14. Speeds indicated on MCDU PERF pages in flight and on the ground are calculated by:

    A. FMGC

  • 15

    8.15. The Flight Control Flight Mode changes to Flare Mode when the aircraft passes:

    A. 50 ft RA for A320, 100 ft RA for A321

  • 16

    8.16. How does the flight control Flare Mode operate when the aircraft descends through 30ft RA (A320):

    A. the system begins to reduce the pitch attitude to 2 ° nose down over a period of 8s

  • 17

    8.17. If the pilot maintains sidestick full forward, the aircraft will:

    C. Significantly overshoot VMO/MMO. At approximately VMO+16 / MMO+0.04, the pitch nose-down authority smoothly reduces to zero

  • 18

    8.18. When does the Flight Control Flight Mode become active?

    B. From liftoff during takeoff until Flare Mode engages at landing

  • 19

    8.19. Roll control in NORMAL LAW is achieved by:

    C. Ailerons and spoilers 2,3,4,5 on each wing

  • 20

    8.20. In normal law, what is the maximum bank angle you can reach with the side stick fully deflected?

    B. 67°

  • 21

    8.21. Rudder deflection will depend on speed

    True

  • 22

    8.22. Maximum rudder deflection is reached at:

    B. LO SPEED

  • 23

    8.23. How many slat surfaces per wing are available?

    5

  • 24

    8.24. How many flap surfaces per wing are available?

    2

  • 25

    8.25 Each wing of A321 NEO has the following lift augmentation devices:

    A. two double-slotted flap surfaces

  • 26

    8.26. How many speed brake surfaces available per wing?

    B. 3 (spoilers 2, 3 and 4)

  • 27

    8.27. What will be speedbrakes surface deflection with autopilot engaged and speedbrake lever in full back position?

    A. ½ for A320, full for A321

  • 28

    8.29. When both main landing gear is compressed:

    B. All ground spoilers will fully deploy

  • 29

    8.30. How many ground spoiler surfaces available per wing?

    5

  • 30

    8.31. MAN PITCH TRIM ONLY red message on PFD indicates that aircraft is in:

    B. Mechanical Back-up

  • 31

    8.32. USE MAN PITCH TRIM amber message on PFD indicates that aircraft is in:

    C. Direct law

  • 32

    8.33. How can you recognize that the aircraft is in Alternate law by inspecting PFD indications:

    A. Amber crosses (X) will replace green double bars “=” on the PFD. Va prot and Va max indications are replaced by Stall Warning Speed (Vsw), which is defined by the top of a red and black strip along the speed scale

  • 33

    8.34. Low speed stability. Aural alert “STALL” will NOT be activated in the _____ law

    C. Normal law

  • 34

    8.35. If both ELACs fail, what controls the elevator and stabilizer?

    B. SECs

  • 35

    8.36. When does the sideslip indicator change to a blue Beta target?

    A. CONF1, 2 or 3 is selected, and any engine N1>80%, and the difference between the engines N1’s exceeds 35%

  • 36

    8.37. High and low speed stability may be available in alternate law.

    True

  • 37

    8.38. With autopilot engaged, either sidestick can be moved freely.

    B. False, applying force on either sidestick beyond predetermined threshold will cause the autopilot(s) to disengage

  • 38

    8.39. Flight Control system Rotation Mode is active:

    B. From 70kt during takeoff roll until 10s after liftoff and pitch attitude is above 8°

  • 39

    8.40. Flight Control system Rotation Mode is designed to:

    B. minimize risk of a tailstrike during takeoff

  • 40

    8.41. The load alleviation function (LAF) permits to alleviate:

    A. the wing structure loads

  • 41

    8.42. The LAF is available when the aircraft is:

    A. in Clean configuration and in Normal Law

  • 42

    8.43. The function of LAF is achieved through the upward deflection of:

    A. two ailerons only, or two ailerons associated to the spoilers 4 and 5