A-320 Chapter № 8. Flight Controls

42問 • 1ヶ月前

Popovich

通報

問題一覧

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

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

Yes

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

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

C. ELAC 2

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

B. Both inputs are algebraically added

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

C. Droop 5 degrees

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

B. Droop 10 degrees

8.8. Two control surfaces that have mechanical backup are:

B. THS and rudder

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

True

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

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

C. Automatic regardless of autopilot status

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

C. Alpha Floor

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

A. FAC

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

A. FMGC

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

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

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

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

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

8.19. Roll control in NORMAL LAW is achieved by:

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

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

B. 67°

8.21. Rudder deflection will depend on speed

True

8.22. Maximum rudder deflection is reached at:

B. LO SPEED

8.23. How many slat surfaces per wing are available?

8.24. How many flap surfaces per wing are available?

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

A. two double-slotted flap surfaces

8.26. How many speed brake surfaces available per wing?

B. 3 (spoilers 2, 3 and 4)

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

8.29. When both main landing gear is compressed:

B. All ground spoilers will fully deploy

8.30. How many ground spoiler surfaces available per wing?

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

B. Mechanical Back-up

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

C. Direct law

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

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

C. Normal law

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

B. SECs

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%

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

True

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

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°

8.40. Flight Control system Rotation Mode is designed to:

B. minimize risk of a tailstrike during takeoff

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

A. the wing structure loads

8.42. The LAF is available when the aircraft is:

A. in Clean configuration and in Normal Law

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

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

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

Yes

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

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

C. ELAC 2

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

B. Both inputs are algebraically added

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

C. Droop 5 degrees

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

B. Droop 10 degrees

8.8. Two control surfaces that have mechanical backup are:

B. THS and rudder

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

True

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

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

C. Automatic regardless of autopilot status

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

C. Alpha Floor

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

A. FAC

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

A. FMGC

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

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

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

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

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

8.19. Roll control in NORMAL LAW is achieved by:

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

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

B. 67°

8.21. Rudder deflection will depend on speed

True

8.22. Maximum rudder deflection is reached at:

B. LO SPEED

8.23. How many slat surfaces per wing are available?

8.24. How many flap surfaces per wing are available?

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

A. two double-slotted flap surfaces

8.26. How many speed brake surfaces available per wing?

B. 3 (spoilers 2, 3 and 4)

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

8.29. When both main landing gear is compressed:

B. All ground spoilers will fully deploy

8.30. How many ground spoiler surfaces available per wing?

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

B. Mechanical Back-up

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

C. Direct law

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

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

C. Normal law

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

B. SECs

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%

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

True

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

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°

8.40. Flight Control system Rotation Mode is designed to:

B. minimize risk of a tailstrike during takeoff

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

A. the wing structure loads

8.42. The LAF is available when the aircraft is:

A. in Clean configuration and in Normal Law

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