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Airbus A320 · Flight Controls 题库（145 题）

Airbus A320 机型「Flight Controls」相关知识共 145 道题。想练习或模拟考试，请到 题库 · 模拟考试。
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1.The ailerons, elevators and pitch trim are powered by three independent actuators, each powered by a separate hydraulic source.

  1. True.
  2. False. ✓
正确答案：False.　·　A320　·　来源 smartcockpit.com

2.In direct law, there is a direct relationship between side stick and con troll surface positions.

  1. There are no protections available.
  2. There are no protections available, although stall and overspeed warnings are still available. ✓
  3. There are no protections available, although stall warning is still available.
正确答案：There are no protections available, although stall and overspeed warnings are still available.　·　A320　·　来源 smartcockpit.com

3.FAC generated slat and flap extension, retraction, and limiting speeds are visually displayed on which of the following?

  1. The MCDU perf page.
  2. The lower ECAM F/CTL page.
  3. Both pilot’s PFD airspeed displays. ✓
  4. All statements are correct.
正确答案：Both pilot’s PFD airspeed displays.　·　A320　·　来源 smartcockpit.com

4.The flight control surfaces are _____ controlled and _____ actuated.

  1. Electrically / hydraulically. ✓
  2. Mechanically / hydraulically.
  3. Electrically / electrically.
  4. Hydraulically / mechanically.
正确答案：Electrically / hydraulically.　·　A320　·　来源 smartcockpit.com

5.Should both FACs fail, maximum rudder deflection can be obtained after the _____ are extended.

  1. Flaps.
  2. Slats. ✓
  3. Gear.
正确答案：Slats.　·　A320　·　来源 smartcockpit.com

6.What happens to the rudder limits if both FAC’s fault?

  1. The limit freezes at the fault condition until Flaps 1 is selected.
  2. The limit freezes at the fault condition until Flaps 5 is selected.
  3. The limit freezes at the fault condition until Flaps 1 is selected. Then it resets to the low speed limits for increased control. ✓
  4. The limit freezes at the fault condition until landing gear is selected down.
正确答案：The limit freezes at the fault condition until Flaps 1 is selected. Then it resets to the low speed limits for increased control.　·　A320　·　来源 smartcockpit.com

7.What condition will cause auto flap retraction?

  1. Exceed 210 kts at Flaps 1. ✓
  2. Exceed 190 kt at Flaps 1.
  3. Exceed 195 kt at Flaps 1
  4. Exceed 190 kt with Flaps 1 while extending the speedbrake lever.
正确答案：Exceed 210 kts at Flaps 1.　·　A320　·　来源 smartcockpit.com

8.With the aircraft in Pitch Alternate Law, roll is in _____ Law.

  1. Direct. ✓
  2. Normal.
  3. Alternate.
正确答案：Direct.　·　A320　·　来源 smartcockpit.com

9.Failure to retract the flaps after takeoff will:

  1. Activate the wing tip brakes.
  2. Result in automatic flap and slat retraction at 210 kt.
  3. Result in automatic flap and slat retraction at 220 kt.
  4. Result in automatic flap retraction at 210 kt. ✓
正确答案：Result in automatic flap retraction at 210 kt.　·　A320　·　来源 smartcockpit.com

10.When the landing gear is extended, pitch alternate law:

  1. Remains the same.
  2. Degrades to pitch direct law. ✓
  3. Degrades to pitch backup law.
正确答案：Degrades to pitch direct law.　·　A320　·　来源 smartcockpit.com

11.Which of the following will automatically reset after landing?

  1. THS. ✓
  2. Rudder trim.
  3. THS and rudder trim.
  4. Ailerons trim.
正确答案：THS.　·　A320　·　来源 smartcockpit.com

12.Mechanical control of the THS is available from the pitch trim wheel at any time if:

  1. Either the green or yellow hydraulic system is functioning. ✓
  2. Both the green and yellow hydraulic system are functioning.
  3. The ELAC2 is operative.
正确答案：Either the green or yellow hydraulic system is functioning.　·　A320　·　来源 smartcockpit.com

13.Flight Control Data Concentrators (FCDC) acquire data from the ELACs and SECs and send it to the electronic instrument system (EIS) and the centralized fault display system (CFDS).

  1. True. ✓
  2. False.
正确答案：True.　·　A320　·　来源 smartcockpit.com

14.Side sticks - If both priority buttons are pushed, the last pressed will give priority. The opposite sidestick can be permanently deactivated by pressing and holding the button for _____.

  1. 10 seconds.
  2. 15 seconds.
  3. 20 seconds.
  4. 40 seconds. ✓
正确答案：40 seconds.　·　A320　·　来源 smartcockpit.com

15.To disable a side-stick, you have to depress the red take-over button on the active stick. Holding the button down for 40 seconds will electrically lock the other stick out until its own red take-over button is pushed again.

  1. True. ✓
  2. False.
正确答案：True.　·　A320　·　来源 smartcockpit.com

16.What control surfaces do the FACs control?

  1. The elevators.
  2. The spoilers.
  3. The rudder. ✓
  4. All statements are correct.
正确答案：The rudder.　·　A320　·　来源 smartcockpit.com

17.Mechanically backed-up control surfaces:

  1. Are mechanically connected to the cockpit controls.
  2. Require hydraulic power for actuation. ✓
  3. All statements are correct.
正确答案：Require hydraulic power for actuation.　·　A320　·　来源 smartcockpit.com

18.The ELAC (Elevator Aileron Computer) are for:

  1. Normal elevator, stabilizer control, and aileron control. ✓
  2. Normal and alternate elevator, and aileron control.
  3. Normal, alternate, and direct elevator and aileron control.
正确答案：Normal elevator, stabilizer control, and aileron control.　·　A320　·　来源 smartcockpit.com

19.What kind of protections are provided if the aircraft is in Alternate Law?

  1. G-load protection with a reduced factor.
  2. Speed Stability
  3. Full G load protection and speed stability
  4. G-load protection and speed stability if the ADIRS and elevators are working. ✓
正确答案：G-load protection and speed stability if the ADIRS and elevators are working.　·　A320　·　来源 smartcockpit.com

20.Where does the SFCCs obtain AOA and air data information from?

  1. SEC.
  2. ELAC.
  3. ADIRU. ✓
  4. ADC.
正确答案：ADIRU.　·　A320　·　来源 smartcockpit.com

21.Which of the following statements is correct concerning the elevator aileron computers (ELACs):

  1. Three computers which achieve normal elevator, stabilizer, and aileron control.
  2. Two computers which achieve normal and standby control of the elevators, ailerons, and trimmable horizontal stabilizer. ✓
  3. Three computers which achieve normal and standby control of the elevators, ailerons, and THS.
  4. Two computers which achieve normal elevator, stabilizer, and aileron control.
正确答案：Two computers which achieve normal and standby control of the elevators, ailerons, and trimmable horizontal stabilizer.　·　A320　·　来源 smartcockpit.com

22.The FLAP lever sends signal to Slat Flap Control Computer (SFCC) to command movement.

  1. True. ✓
  2. False.
正确答案：True.　·　A320　·　来源 smartcockpit.com

23.Which of the following statements best describes the Load Alleviation function (LAF)?

  1. Helps the pilot control the airplane.
  2. Relieves wing structure loads by deflecting the ailerons and spoilers. ✓
  3. Relieves wing structure loads by deflecting only the spoilers.
  4. Relieves wing structure loads by deflecting the ailerons.
正确答案：Relieves wing structure loads by deflecting the ailerons and spoilers.　·　A320　·　来源 smartcockpit.com

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

  1. 33 degrees.
  2. 49 degrees.
  3. 67 degrees. ✓
  4. 70 degrees.
正确答案：67 degrees.　·　A320　·　来源 smartcockpit.com

25.When is the Flight Mode active?

  1. From takeoff until landing.
  2. From liftoff until landing.
  3. From liftoff until flare mode engages at 50 ft RA.
  4. From takeoff until passing 50 kt on landing (main shock absorbers depressed). ✓
正确答案：From takeoff until passing 50 kt on landing (main shock absorbers depressed).　·　A320　·　来源 smartcockpit.com

26.If both pilots deflect their side sticks fully back:

  1. The "pitch up" order is twice as high as with only one stick deflected.
  2. The "pitch up" order is 1.5 times higher as high as with only one stick deflected.
  3. No inputs are sent to the flight control computers unless one pilot presses the takeover pushbutton on his stick.
  4. The "pitch up" order is equal to a single stick deflection. ✓
正确答案：The "pitch up" order is equal to a single stick deflection.　·　A320　·　来源 smartcockpit.com

27.Can the crew make a flight control input that will over-stress the airplane in direct law?

  1. No. The system is designed to avoid such an attempt.
  2. Yes, there are no protections provided in direct law. ✓
正确答案：Yes, there are no protections provided in direct law.　·　A320　·　来源 smartcockpit.com

28.In normal operations, ELAC1 and ELAC2 control the elevators and the horizontal stabilizer, and the green and yellow hydraulic jacks drive the left and right elevator surfaces respectively.

  1. True.
  2. False. ✓
正确答案：False.　·　A320　·　来源 smartcockpit.com

29.Is there any rudder pedal feedback for the yaw damping and turn coordination functions?

  1. Yes.
  2. No. ✓
正确答案：No.　·　A320　·　来源 smartcockpit.com

30.When is alpha floor not available?

  1. Out of normal law.
  2. Below 100 feet RA in landing configuration.
  3. If the A/THR is deactivated or unavailable.
  4. All statements are correct. ✓
正确答案：All statements are correct.　·　A320　·　来源 smartcockpit.com

31.Can the rudders be moved with both FAC’s inoperative?

  1. Yes, if both FACs fail, maximum rudder deflection can be obtained when the slats are extended. ✓
  2. Yes, if both FACs fail, maximum rudder deflection can be obtained.
  3. Yes, if both FACs fail, maximum rudder deflection can be obtained when the gear is extended or flaps extended at 1 minimum.
  4. No.
正确答案：Yes, if both FACs fail, maximum rudder deflection can be obtained when the slats are extended.　·　A320　·　来源 smartcockpit.com

32.What is true concerning the side stick takeover push button?

  1. The last pilot to depress the push button has priority.
  2. If the takeover push button is depressed for more than 40 seconds, the onside system will retain priority after the push button is released.
  3. All statements are correct. ✓
正确答案：All statements are correct.　·　A320　·　来源 smartcockpit.com

33.Automatic rudder trim is provided at the rate of 5 degrees per second while the manual rudder trim rate is _____ up to a maximum of _____.

  1. 1 degree per second - 20 degrees. ✓
  2. 8 degrees per second - 10 degrees.
  3. 3 degrees per second - 15 degrees.
  4. 10 degrees per second - 15 degrees.
正确答案：1 degree per second - 20 degrees.　·　A320　·　来源 smartcockpit.com

34.The 2 FACs (Flight Augmentation Computers) are for:

  1. Normal elevator, stabilizer control, and aileron control.
  2. Spoilers control, standby elevator, and stabilizer control.
  3. Normal and standby elevator, and aileron control.
  4. Electrical rudder control. ✓
正确答案：Electrical rudder control.　·　A320　·　来源 smartcockpit.com

35.What is the maximum flap setting for in-flight use of the spoilers?

  1. Flaps FULL.
  2. Flaps 3. ✓
  3. Spoilers are not approved for in-flight use.
  4. Flaps 10.
正确答案：Flaps 3.　·　A320　·　来源 smartcockpit.com

36.In pitch normal law, the elevator control changes from the normal mode to a protection mode when the angle of attack is greater than:

  1. Alpha Max.
  2. Alpha Prot. ✓
  3. Alpha Floor.
正确答案：Alpha Prot.　·　A320　·　来源 smartcockpit.com

37.While on the ground in Roll Normal Law there is a direct relationship between sidestick deflection and the corresponding aileron and spoiler deflection.

  1. True. ✓
  2. False.
正确答案：True.　·　A320　·　来源 smartcockpit.com

38.Which of the following controls and monitors flaps and slats?

  1. Two Elevator and Ailerons Computers (ELACs).
  2. Wing tip brakes.
  3. One slat flap control computer (SFCC).
  4. Two slat flap control computers (SFCCs). ✓
正确答案：Two slat flap control computers (SFCCs).　·　A320　·　来源 smartcockpit.com

39.Selection of flaps one prior to takeoff will select which of the following?

  1. Slats 1 and flaps 1 (1+F). ✓
  2. Slats 0 and flaps 1 (0+F).
  3. Slats 1 and flaps 0.
  4. Slats 1 and flaps 5.
正确答案：Slats 1 and flaps 1 (1+F).　·　A320　·　来源 smartcockpit.com

40.Four hydraulically-operated wing tip brakes are installed to lock the flaps or slats in case of:

  1. Asymmetry and overspeed.
  2. Asymmetry, overspeed and slow movement.
  3. Asymmetry, overspeed, symmetrical runaway and uncommanded movement. ✓
  4. All statements are correct.
正确答案：Asymmetry, overspeed, symmetrical runaway and uncommanded movement.　·　A320　·　来源 smartcockpit.com

41.Selection of flaps 1 in flight will select which of the following configurations?

  1. Slats 1 and flaps 1 (1+F).
  2. Slats 0 and flaps 1 (0+F).
  3. Slats 1 and flaps 0 (1). ✓
  4. Slats 1 and flaps 5 (1+F).
正确答案：Slats 1 and flaps 0 (1).　·　A320　·　来源 smartcockpit.com

42.There are _____ that control the aircraft in pitch.

  1. One elevator and a Trimmable Horizontal Stabilizer (THS). ✓
  2. Four elevators.
  3. Two elevators and the Trimmable Horizontal Stabilizer (THS).
正确答案：One elevator and a Trimmable Horizontal Stabilizer (THS).　·　A320　·　来源 smartcockpit.com

43.In Normal Law, what are the limits of Pitch Attitude protections with flaps Full.

  1. 30 degrees nose up.
  2. 35 degrees nose up progressively reduced to 20 degrees.
  3. 25 degrees nose up, progressively reduced to 20 degrees at low speed. ✓
  4. There is no limit.
正确答案：25 degrees nose up, progressively reduced to 20 degrees at low speed.　·　A320　·　来源 smartcockpit.com

44.The "SPEED BRK" memo on the E/WD will flash amber if Speed brakes are extended and:

  1. Any engine is above idle. ✓
  2. Both engines are above idle.
  3. Any engine is above idle or TLA (Thrust Lever Angle) is more than 15 degrees.
  4. Both engines are above idle or TLA (Thrust Lever Angle) is more than 15 degrees.
正确答案：Any engine is above idle.　·　A320　·　来源 smartcockpit.com

45.Automatic pitch trim is provided both on ground and in flight.

  1. True.
  2. False. ✓
正确答案：False.　·　A320　·　来源 smartcockpit.com

46.In Direct Law, the yaw damping is lost but turn coordination is still available. The yaw damping and turn coordination functions are lost.

  1. True.
  2. False. ✓
正确答案：False.　·　A320　·　来源 smartcockpit.com

47.The message WING TIP BRK ON appears on the E/WD. What does it mean?

  1. A hydraulic device locks the flaps in their present position. ✓
  2. To reduce structural stress, the slats movement is being slowed down through the wing tip brakes.
  3. To avoid asymmetry, the outer slats are locked in their present position.
  4. Because of the locked flaps, the wing tip brakes also lock the slats.
正确答案：A hydraulic device locks the flaps in their present position.　·　A320　·　来源 smartcockpit.com

48.Auto ground spoilers are armed by pulling the spoiler lever up to expose a white collar. A memo on the E/WS confirms arming.

  1. True. ✓
  2. False.
正确答案：True.　·　A320　·　来源 smartcockpit.com

49.Should the active elevator actuator fail, elevator control is:

  1. Lost.
  2. Maintained by the other actuator. ✓
  3. Reduced.
正确答案：Maintained by the other actuator.　·　A320　·　来源 smartcockpit.com

50.A screwjack driven by _____ drives the stabilizer.

  1. One hydraulic motor.
  2. Two hydraulic motors. ✓
  3. Three hydraulic motors.
  4. Three hydraulic motors (two active and one standby).
正确答案：Two hydraulic motors.　·　A320　·　来源 smartcockpit.com

51.ALPHA/SPEED LOCK FUNCTION - This function inhibits slat retraction at high angles-of-attack and low speeds or high speeds.

  1. True.
  2. False. ✓
正确答案：False.　·　A320　·　来源 smartcockpit.com

52.Locked flaps or slats may be caused by the Wing Tip Brakes (WTB) locking the affected surface movement if _____ are detected.

  1. Assymmetry, overspeed, or uncommanded movement.
  2. Assymmetry, overspeed, symmetrical runaway or uncommanded movement. ✓
  3. Overspeed or uncommanded movement.
  4. Uncommanded movement.
正确答案：Assymmetry, overspeed, symmetrical runaway or uncommanded movement.　·　A320　·　来源 smartcockpit.com

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

  1. The inputs cancel each other.
  2. Both inputs are algebraically added. ✓
  3. The CM2 input is overridden by the CM1 input.
  4. The CM1 input is overridden by the CM2 input.
正确答案：Both inputs are algebraically added.　·　A320　·　来源 smartcockpit.com

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

  1. True. ✓
  2. False.
正确答案：True.　·　A320　·　来源 smartcockpit.com

55.Once activated the wing tip brakes:

  1. Lock both the slats and flaps in their current position.
  2. Lock only the flaps in their current position.
  3. Lock only the slats in their current position.
  4. Lock only the affected high lift system surfaces in their current position. ✓
正确答案：Lock only the affected high lift system surfaces in their current position.　·　A320　·　来源 smartcockpit.com

56.Aileron droop may best be confirmed by checking which of the following?

  1. The position of the ailerons on the exterior preflight inspection.
  2. The lower ECAM FLT/CTL page. ✓
  3. The position of the flap handle.
正确答案：The lower ECAM FLT/CTL page.　·　A320　·　来源 smartcockpit.com

57.With an elevator fault, the remaining elevator remains operative, but its deflection limits are reduced to prevent excessive torsional loads on the tail. Normal flight is possible in this configuration. If the elevators are lost entirely, they are automatically set to the neutral position.

  1. True. ✓
  2. False.
正确答案：True.　·　A320　·　来源 smartcockpit.com

58.The spoiler panels are the only flight control surfaces with no redundant control.

  1. True. ✓
  2. False.
正确答案：True.　·　A320　·　来源 smartcockpit.com

59.When the flaps are extended, the ailerons:

  1. Go to the centering mode.
  2. Pitch up 5 degrees.
  3. Pitch up 7.5 degrees.
  4. Droop 5 degrees. ✓
正确答案：Droop 5 degrees.　·　A320　·　来源 smartcockpit.com

60.Which controls are used for the mechanical backup?

  1. Ailerons and rudder.
  2. THS and rudder. ✓
  3. Elevators and ailerons.
  4. THS and elevator.
正确答案：THS and rudder.　·　A320　·　来源 smartcockpit.com

61.If the ground spoilers are armed and the speed exceeds 72 kt, the ground spoilers will automatically extend as soon as both thrust levers are reset to idle.

  1. True. ✓
  2. False.
正确答案：True.　·　A320　·　来源 smartcockpit.com

62.Elevator actuation - Two electrically controlled hydraulic servojacks drive each elevator.

  1. In normal operation one jack is in active mode. The other jack is in damping mode. Some maneuvers cause the second jack to become active. ✓
  2. One jack is used during normal law and the other jack is used in alternate law.
  3. The two jacks are used simultaneously.
正确答案：In normal operation one jack is in active mode. The other jack is in damping mode. Some maneuvers cause the second jack to become active.　·　A320　·　来源 smartcockpit.com

63.If angle of attack protection is active or flaps are in the configuration Full:

  1. Speed brake extension is inhibited. ✓
  2. Aileron travel is reduced.
  3. Speed brake extension travel is reduced.
正确答案：Speed brake extension is inhibited.　·　A320　·　来源 smartcockpit.com

64.With the autopilot engaged, the FMGC computes the rudder trim orders. The rudder trim rotary switch and the rudder trim reset pushbutton are not active.

  1. True. ✓
  2. False.
正确答案：True.　·　A320　·　来源 smartcockpit.com

65.What are the rudder trim rates?

  1. Autopilot on = 5 degrees per sec and Autopilot off = 1 degree per second. ✓
  2. Autopilot on = 2,5 degrees /second and Autopilot off = 5 degrees /second.
  3. Autopilot on = 3 degrees / second and Autopilot off = 6 degrees / second.
  4. Autopilot on = 5 degrees / second and Autopilot off = 6 degrees / second.
正确答案：Autopilot on = 5 degrees per sec and Autopilot off = 1 degree per second.　·　A320　·　来源 smartcockpit.com

66.The rudder deflection is limited depending on speed by the rudder travel limiter. The current rudder travel limit is shown on the F/CTL ECAM page by white ticks below the rudder scale.

  1. True. ✓
  2. False.
正确答案：True.　·　A320　·　来源 smartcockpit.com

67.What computer normally commands the operation of the elevators and horizontal stabilizer?

  1. SEC 1.
  2. FAC 1.
  3. ELAC 2. ✓
  4. SEC 2.
正确答案：ELAC 2.　·　A320　·　来源 smartcockpit.com

68.How many actuators are provided to control the ailerons and how many hydraulic sources supply these actuators?

  1. Two hydraulic sources with four actuators. ✓
  2. One hydraulic source with two actuators.
  3. Four hydraulic sources with four actuators.
  4. Three hydraulic sources with four actuators.
正确答案：Two hydraulic sources with four actuators.　·　A320　·　来源 smartcockpit.com

69.What happens to high speed (VMO/MMO) when you are in Alternate Law?

  1. VMO is reduced to 320 kt and MMO minus 10 kt.
  2. VMO is reduced to 330 kt and MMO minus 10 kt.
  3. VMO is reduced to 320 kt and MMO does not change. ✓
  4. There is no change.
正确答案：VMO is reduced to 320 kt and MMO does not change.　·　A320　·　来源 smartcockpit.com

70.The ground spoilers retract:

  1. After landing.
  2. After a rejected takeoff, when the ground spoilers are disarmed.
  3. During a touch and go, when at least one thrust lever is advanced above 20 degrees.
  4. All statements are correct. ✓
正确答案：All statements are correct.　·　A320　·　来源 smartcockpit.com

71.Roll control is achieved by:

  1. Ailerons.
  2. Two Ailerons and two spoilers on each wing.
  3. One aileron and four spoilers on each wing. ✓
  4. Ailerons, rudder and spoilers.
正确答案：One aileron and four spoilers on each wing.　·　A320　·　来源 smartcockpit.com

72.A-LOCK pulsing _____ on the E/WD indicates that the slats have been locked due to high angle of attack and/or low speed

  1. Amber.
  2. Blue. ✓
  3. Green.
  4. White.
正确答案：Blue.　·　A320　·　来源 smartcockpit.com

73.The wing tip brakes are:

  1. Electrically actuated.
  2. Electric brakes.
  3. Hydraulically actuated. ✓
  4. Mechanically controlled, hydraulically actuated.
正确答案：Hydraulically actuated.　·　A320　·　来源 smartcockpit.com

74.Two control surfaces that have mechanical backup are:

  1. Elevator and rudder.
  2. Horizontal stabilizer and rudder. ✓
  3. Speed brakes and rudder.
正确答案：Horizontal stabilizer and rudder.　·　A320　·　来源 smartcockpit.com

75.Sideslip target - In the case of an engine failure at takeoff, or at go-around, the sideslip index on the PFD changes from _____.

  1. White to blue.
  2. Yellow to blue. ✓
  3. Blue to white.
  4. White to yellow.
正确答案：Yellow to blue.　·　A320　·　来源 smartcockpit.com

76.Turn coordination is available in Alternate Law.

  1. True.
  2. False. ✓
正确答案：False.　·　A320　·　来源 smartcockpit.com

77.Let’s assume the F/O presses his takeover pushbutton and releases it after more than 40 seconds.

  1. The Captain’s side stick is de-activated unless he presses his takeover pushbutton. ✓
  2. The Captain is unable to re-activate his side-stick for the rest of the flight.
  3. Both sticks are active.
  4. The Captain’s side stick is active as long as the F/O’s side stick is in neutral position.
正确答案：The Captain’s side stick is de-activated unless he presses his takeover pushbutton.　·　A320　·　来源 smartcockpit.com

78.There are ten spoilers (five each side) and they have several functions, each using different surfaces:

  1. Speed brakes use the 3 central surfaces to increase drag.
  2. Roll control use the four outer spoilers to assist in rolling the aircraft.
  3. Ground spoilers deploy all spoilers to dump lift to get weight on the wheels.
  4. All statements are correct. ✓
正确答案：All statements are correct.　·　A320　·　来源 smartcockpit.com

79.What happens if you release the stick at 40 degrees of bank?

  1. The bank stays at 40 degrees.
  2. The aircraft rolls back to 25 degrees.
  3. The aircraft rolls back to 33 degrees and resumes flight path stability. ✓
  4. The aircraft rolls back to a bank angle less than 29 degrees.
正确答案：The aircraft rolls back to 33 degrees and resumes flight path stability.　·　A320　·　来源 smartcockpit.com

80.In Pitch Normal Law Flight Mode, pitch trim is:

  1. Manual without the autopilot engaged.
  2. Automatic as long as the autopilot is engaged.
  3. Automatic with or without the autopilot engaged. ✓
正确答案：Automatic with or without the autopilot engaged.　·　A320　·　来源 smartcockpit.com

81.In flight mode, control surface deflection is not directly proportional to side stick deflection. Instead, side stick input is a rate of roll demand in roll and a load factor demand in pitch.

  1. True. ✓
  2. False.
正确答案：True.　·　A320　·　来源 smartcockpit.com

82.What happens in the event of a single ELAC failure?

  1. ELAC functions are transferred the SECs.
  2. ELAC functions are transferred to FACs.
  3. SEC functions are transferred the ELACs.
  4. The functions of the failed ELAC will be assumed by the remaining ELAC. ✓
正确答案：The functions of the failed ELAC will be assumed by the remaining ELAC.　·　A320　·　来源 smartcockpit.com

83.Which altitude limitation is associated with high lift devices?

  1. Max altitude for extension is 20, 000 ft. ✓
  2. Max altitude for extension is 22, 000 ft.
  3. Max altitude for extension is 25, 000 ft.
  4. Max altitude for extension is 27, 000 ft.
正确答案：Max altitude for extension is 20, 000 ft.　·　A320　·　来源 smartcockpit.com

84.Lift augmentation devices consist of:

  1. Four slats on each leading edge and two flaps on each trailing edge.
  2. Three slats on each leading edge and three flaps on each trailing edge.
  3. Two slats on each leading edge and two flaps on each trailing edge.
  4. Five slats on each leading edge and two flaps on each trailing edge. ✓
正确答案：Five slats on each leading edge and two flaps on each trailing edge.　·　A320　·　来源 smartcockpit.com

85.In normal law, if one stick is rapidly pulled fully back, can the aircraft’s maximum allowable “G” load be exceeded?

  1. Yes. Rapid side stick deflection must never be made.
  2. Yes, until maximum pitch attitude is reached.
  3. No. At Maximum “G” load, the side sticks are de-activated for 5 seconds.
  4. No. The load factor limitation overrides side stick commands to avoid excessive “G” loads. ✓
正确答案：No. The load factor limitation overrides side stick commands to avoid excessive “G” loads.　·　A320　·　来源 smartcockpit.com

86.The FAC’s primarily control which control surface?

  1. Elevator.
  2. Rudder. ✓
  3. Aileron.
  4. Elevator and aileron.
正确答案：Rudder.　·　A320　·　来源 smartcockpit.com

87.To select speedbrakes inflight, the pilot should:

  1. Push down on the speed brake handle and move it forward.
  2. Push down on the speed brake handle and move it aft. ✓
  3. Pull up on the speed brake handle and move it aft.
正确答案：Push down on the speed brake handle and move it aft.　·　A320　·　来源 smartcockpit.com

88.In the case of an extraordinary unpredictable external event (e.g. mid-air collision) the flight parameters may go far beyond the limits of the protected envelope. In this case, specific control laws are activated to ensure aircraft recovery, and to allow a safe continuation of the flight. This is called “Abnormal Attitude Law”.

  1. True. ✓
  2. False.
正确答案：True.　·　A320　·　来源 smartcockpit.com

89.On the ground, a combined side stick deflection indicator is shown as a white cross on the attitude indicator. This indicates control surface positions.

  1. True.
  2. False. ✓
正确答案：False.　·　A320　·　来源 smartcockpit.com

90.If both FAC’s fail, what happens to the rudder limiter?

  1. It immediately assumes the low speed position.
  2. It freezes at its present position and assumes the low speed position when flaps 1 are selected. ✓
  3. Maximum rudder deflection can be obtained after slats extended.
  4. Maximum rudder deflection can be obtained after flaps extended.
正确答案：It freezes at its present position and assumes the low speed position when flaps 1 are selected.　·　A320　·　来源 smartcockpit.com

91.You can degrade directly from Normal Law to Direct Law with gear down and a dual radio altimeter fault.

  1. True. ✓
  2. False.
正确答案：True.　·　A320　·　来源 smartcockpit.com

92.Can you manually trim the rudder with the autopilot engaged?

  1. Yes.
  2. No. ✓
正确答案：No.　·　A320　·　来源 smartcockpit.com

93.The alpha speed lock function:

  1. Will inhibit flap retraction during an inadvertent movement of the flap selector at high AOA or low speeds.
  2. Will inhibit slat retraction during an inadvertent movement of the flap selector at high AOA or low speeds. ✓
  3. Automatically raises the flaps if retraction has not been accomplished by 210 kt.
正确答案：Will inhibit slat retraction during an inadvertent movement of the flap selector at high AOA or low speeds.　·　A320　·　来源 smartcockpit.com

94.The maximum deflection of the spoilers is:

  1. 90 degrees.
  2. 60 degrees.
  3. 45 degrees.
  4. 35 degrees. ✓
正确答案：35 degrees.　·　A320　·　来源 smartcockpit.com

95.Aileron actuation - Each aileron has two electrically controlled hydraulic servojacks. One of these servojacks per aileron operates at a time. Each servojack has two control modes:

  1. Active: Jack position is controlled hydraulically. Damping: Jack position is controlled electrically.
  2. Normal: Jack position is actuated hydraulically. Damping: Jack is controlled electrically.
  3. Active: Jack position is controlled electrically. Damping: Jack follows surface movement. ✓
正确答案：Active: Jack position is controlled electrically. Damping: Jack follows surface movement.　·　A320　·　来源 smartcockpit.com

96.If electrical power to a SEC fails:

  1. The affected spoilers automatically retract. ✓
  2. All spoilers automatically retract.
  3. The affected spoilers remain in the last commanded position.
  4. Half of the spoilers automatically retract.
正确答案：The affected spoilers automatically retract.　·　A320　·　来源 smartcockpit.com

97.What is the true statement concerning the Spoiler Elevator Computers (SECs)?

  1. Two computers which achieve spoiler control and standby elevator and THS control.
  2. Three computers which achieve spoiler control and normal elevator and THS control.
  3. Three computers which achieve spoiler control and standby elevator and THS control. ✓
正确答案：Three computers which achieve spoiler control and standby elevator and THS control.　·　A320　·　来源 smartcockpit.com

98.Seven flight control computers process pilot and autopilot inputs according to normal, alternate, or direct flight control laws.

  1. True. ✓
  2. False.
正确答案：True.　·　A320　·　来源 smartcockpit.com

99.Following nosewheel touchdown, as the pitch attitude becomes less than 2.5 degrees for more than 5 seconds, pitch trim is automatically reset to zero.

  1. True. ✓
  2. False.
正确答案：True.　·　A320　·　来源 smartcockpit.com

100.When deploying flaps when airborne, selecting 1 on the flap lever only moves the slats - i.e. configuration 1 is achieved rather than 1+F.

  1. True. ✓
  2. False.
正确答案：True.　·　A320　·　来源 smartcockpit.com

101.In the event of a complete loss of electrical flight control signals, the airplane reverts to a _____ mode.

  1. Mechanical. ✓
  2. Alternate Law.
  3. Abnormal Attitude law.
正确答案：Mechanical.　·　A320　·　来源 smartcockpit.com

102.If the ground spoilers are not armed and the speed exceeds 72 kt, the ground spoilers will automatically extend as soon as:

  1. Reverse is selected on one engine (the other thrust lever remains at idle). ✓
  2. Both thrust levers are reset to idle.
  3. Both thrust reversers are selected.
正确答案：Reverse is selected on one engine (the other thrust lever remains at idle).　·　A320　·　来源 smartcockpit.com

103.What happens in the side stick-neutral high speed protection mode?

  1. The autopilot disengages, bank angle limit is 30 degrees and the aircraft is 25 degrees roll limited.
  2. The autopilot disengages, bank angle limit is 45 degrees and the aircraft is 25 degrees roll limited.
  3. The autopilot disengages, bank angle limit is 40 degrees and the aircraft rolls wings level and pitches up to slow down to VMO/MMO. ✓
  4. The autopilot disengages, bank angle limit is 35 degrees and the aircraft rolls wings level and pitches to 10 degrees to slow down to VMO/MMO - 20 kt.
正确答案：The autopilot disengages, bank angle limit is 40 degrees and the aircraft rolls wings level and pitches up to slow down to VMO/MMO.　·　A320　·　来源 smartcockpit.com

104.The autopilot will disconnect if the side stick takeover push button is depressed.

  1. True. ✓
  2. False.
正确答案：True.　·　A320　·　来源 smartcockpit.com

105.When ground spoilers deploy automatically:

  1. All ten spoiler panels fully deploy. ✓
  2. Four spoiler panels on each wing deploy.
  3. All ten spoiler panels deploy half way.
  4. Six spoiler panels on each wing deploy.
正确答案：All ten spoiler panels fully deploy.　·　A320　·　来源 smartcockpit.com

106.Are there any control surfaces with a mechanical backup?

  1. Yes, the ailerons.
  2. Yes, the spoilers.
  3. Yes, the ailerons and spoilers.
  4. Yes, the THS and the rudder. ✓
正确答案：Yes, the THS and the rudder.　·　A320　·　来源 smartcockpit.com

107.Direct law is indicated by the ECAM message FCTL DIRECT LAW (PROT LOST). Auto-trim is not available. A "USE MAN PITCH TRIM" message appears on the FMA. Auto turn coordination and dutch roll damping are also lost.

  1. True. ✓
  2. False.
正确答案：True.　·　A320　·　来源 smartcockpit.com

108.During an approach with L/G not down locked, flaps extended and both engines not at T.O power you get master warning and ECAM 'gear not down!' at an radio height of

  1. lower than 1,000 ft and higher than 850 ft.
  2. lower than 850 ft and higher than 750 ft
  3. lower than 750 ft ✓
正确答案：lower than 750 ft　·　A320　·　来源 Chair Flight A320 Question Bank

109.At _______________ the connection between nosewheel steering and the rudder pedals is removed

  1. 130 knots (aircraft ground speed) ✓
  2. 110 knots (aircraft ground speed)
  3. touchdow
正确答案：130 knots (aircraft ground speed)　·　A320　·　来源 Chair Flight A320 Question Bank

110.If a take-off is aborted just before V1 with auto brake selection MAX but spoilers not armed, the auto brake will:

  1. Not be activated
  2. Become active when at least one thrust lever is set to reverse, and the other at or near idle ✓
  3. Become active when both thrust levers are set to idle only
  4. Become active when both thrust levers are set to reverse only
正确答案：Become active when at least one thrust lever is set to reverse, and the other at or near idle　·　A320　·　来源 Chair Flight A320 Question Bank

111.You are ready to taxi. You apply the toe brakes on the rudder pedals and release the PARK BRK. The BRAKES pressure falls to zero. What should you do?

  1. This should not happen and you must assume that the BRAKES pressure indicator has failed.
  2. Nothing, as this is normal. The BRAKES pressure indicator only indicates alternate (yellow) brake pressure. ✓
  3. You must re-apply the PARK BRK and call for maintenance personnel as the main system pressure has failed.
  4. The indication is normal because once the AUTO BRK is set to MAX the BRAKES indicator is by-passed.
正确答案：Nothing, as this is normal. The BRAKES pressure indicator only indicates alternate (yellow) brake pressure.　·　A320　·　来源 Chair Flight A320 Question Bank

112.Above which speed, do the armed ground spoilers extend automatically upon a rejected T/O?

  1. 80 kt
  2. 72 kt ✓
  3. 55 kt
  4. 90 kt
正确答案：72 kt　·　A320　·　来源 Chair Flight A320 Question Bank

113.In order to avoid overshooting the altitude, due to speedbrake retraction in ALT* mode, retract the speedbrakes at least _________ before the selected altitude.

  1. 1'000ft
  2. 1'500ft
  3. 2'000ft ✓
  4. 2'500ft
正确答案：2'000ft　·　A320　·　来源 Chair Flight A320 Question Bank

114.Which memory items define to retract the speedbrakes?

  1. Unreliable speed indication, GPWS warnings, Stall recovery ✓
  2. Stall recovery, Loss of braking, Emergency descent
  3. GPWS warnings, Emergency descent, TCAS warnings
  4. Unreliable speed indications, Windshear ahead, Stall warning at lift-off
正确答案：Unreliable speed indication, GPWS warnings, Stall recovery　·　A320　·　来源 Chair Flight A320 Question Bank

115.Which statement about landing with slats or flaps jammed is correct?

  1. The flap lever is useless due to jammend slats and flaps and have to maintain at the last selected position
  2. The autopilot must not be used for this kind of abnormal configuration
  3. The autopilot may be used down to 500ft AGL. As it is tuned for abnormal configurations, ist behavior can be less than optimum and must be monitored ✓
  4. The autopilot may be used up to the maximum indicated landing capability with possibility for autoland if indicated
正确答案：The autopilot may be used down to 500ft AGL. As it is tuned for abnormal configurations, ist behavior can be less than optimum and must be monitored　·　A320　·　来源 Chair Flight A320 Question Bank

116.Is there any crosswind limitation for landing with jammend flight controls?

  1. Yes, 20kt for LANDING WITH SLATS OR FLAPS JAMMED
  2. No, there are no crosswind limits for a landing with jammend flight controls
  3. Yes, 15 kt for RUDDER JAM ✓
  4. Yes, 25 kt for F/CTL L(R) SIDESTICK FAULT
正确答案：Yes, 15 kt for RUDDER JAM　·　A320　·　来源 Chair Flight A320 Question Bank

117.Which statement about the FLAP SYSTEM is correct?

  1. The pilot cannot select an intermediate lever position
  2. Before selecting any position, the pilot must pull the lever out of the detent
  3. Balks at position 1 and 3 prevent the pilot from calling for excessive flap/slat travel with a single action
  4. All answers are correct ✓
正确答案：All answers are correct　·　A320　·　来源 Chair Flight A320 Question Bank

118.Flight control surfaces are all:

  1. Electrically-controlled and Hydraulically-activated ✓
  2. Hydraulically-controlled and Electrically-activated
  3. Electrically-controlled and Mechanically-activated
  4. Mechanically-controlled and Electrically-activated
正确答案：Electrically-controlled and Hydraulically-activated　·　A320　·　来源 Chair Flight A320 Question Bank

119.How many flight control computers process pilot and autopilot inputs?

  1. 7 (2 ELACs, 3 SECs, 2 FACs) ✓
  2. 6 (2 ELACs, 3 SECs, 1 FAC)
  3. 5 (2 ELACs, 2 SECs, 1 FAC)
  4. 4 (2 ELACS, 1 SEC, 1 FAC)
正确答案：7 (2 ELACs, 3 SECs, 2 FACs)　·　A320　·　来源 Chair Flight A320 Question Bank

120.To control the aircraft about the roll axis the following Flight controls will are used:

  1. Aileron, rudder and spoilers
  2. One aileron and four spoilers on each wing ✓
  3. Aileron and rudder
  4. Aileronsonly
正确答案：One aileron and four spoilers on each wing　·　A320　·　来源 Chair Flight A320 Question Bank

121.Mechanical control of the flight controls is available for?

  1. Elevator and aileron
  2. Rudder and elevator
  3. Stabilizer and rudder ✓
  4. Aileron and stabilizer
正确答案：Stabilizer and rudder　·　A320　·　来源 Chair Flight A320 Question Bank

122.With the autopilot engaged, the FMGC computes the rudder trim orders. The rudder trim rotary switch and the rudder trim reset pushbutton_____________.

  1. Are not active ✓
  2. Are active as long as the flight control system is in NORMAL LAW
  3. Operate with limited range (Dependig on the aircraft speed within the envelope)
  4. Are active as long as the flight control system is in ALTERNATE LAW only
正确答案：Are not active　·　A320　·　来源 Chair Flight A320 Question Bank

123.TAKEOFF IN CONFIGURATION 1 + F If the flight crew does not select configuration zero after takeoff, the flaps retract automatically at ___ kt:

  1. 200 kt
  2. 205 kt
  3. 210 kt ✓
  4. 220 kt
正确答案：210 kt　·　A320　·　来源 Chair Flight A320 Question Bank

124.What is the mechanical back-up in the flight controls system?

  1. It consists of cables between the cockpit controls and the flight controls surfaces in the pitch and roll axis in case of a total loss of both ELAC computers
  2. It enables the pilot to control the aircraft during a temporary complete loss of electrical power. It does this in pitch by manually applying trim to the THS ✓
  3. It enables the pilot to control the aircraft when the pitch attitude exceeds 50° nose up or 30° nose down and when bank angle exceeds 125°
  4. It enables the pilot to control the aircraft during ELEC EMER configuration. The PFDs display USE MAN PITCH TRIM
正确答案：It enables the pilot to control the aircraft during a temporary complete loss of electrical power. It does this in pitch by manually applying trim to the THS　·　A320　·　来源 Chair Flight A320 Question Bank

125.RUD TRIM RESET pb: By pushing the RESET pb on the ground, the zero trim position is ordered at 1.5 °/s. After the reset, an indication of up to ___ ° (L or R) may be observed in the rudder trim position indication:

  1. 2.5
  2. 2.0
  3. 1.0
  4. 0.3 ✓
正确答案：0.3　·　A320　·　来源 Chair Flight A320 Question Bank

126.Which spoilers are used as speedbrakes?

  1. 1,2 and 3
  2. 1,2,3,4and5
  3. 2,3and4 ✓
  4. 3,4and5
正确答案：2,3and4　·　A320　·　来源 Chair Flight A320 Question Bank

127.Which spoilers are used as ground spoilers?

  1. 1,2and3
  2. 1,2,3,4and5 ✓
  3. 2,3and4
  4. 3,4and5
正确答案：1,2,3,4and5　·　A320　·　来源 Chair Flight A320 Question Bank

128.Under NORMAL LAW, when the angle-of-attack becomes greater than ____, the system switches elevator control from normal mode to a protection mode, in which the angle-of-attack is proportional to sidestick deflection.

  1. ALPHA FLOOR
  2. ALPHAPROT ✓
  3. ALPHAMAX
  4. ALPHAPROT+1°
正确答案：ALPHAPROT　·　A320　·　来源 Chair Flight A320 Question Bank

129.Which of the following statements, describing the ground spoilers function during a rejected takeoff, is correct?

  1. If the ground spoilers are armed and the speed exceeds 72kts the ground spoilers will automatically extend as soon as one thrust lever are reset to idle
  2. If the ground spoilers are armed and the speed exceeds 72kts the ground spoilers will automatically extend as soon as both thrust levers are reset to idle ✓
  3. If the ground spoilers are not armed and the speed exceeds 72kts the ground spoiler will automatically extend as soon as both thrust levers are reset to idle
  4. If the ground spoilers are not armed and the speed exceeds 72kts the ground spoilers will never extend
正确答案：If the ground spoilers are armed and the speed exceeds 72kts the ground spoilers will automatically extend as soon as both thrust levers are reset to idle　·　A320　·　来源 Chair Flight A320 Question Bank

130.The maximum rudder deflection that the rudder travel limiter will allow under normal conditions is:

  1. 25° rudder deflection up to a speed of 160kts ✓
  2. 15° rudder deflection up to a speed of 150kts
  3. 45° rudder deflection up to a speed of 160kts
  4. 25° rudder deflection at a speed of 300kts
正确答案：25° rudder deflection up to a speed of 160kts　·　A320　·　来源 Chair Flight A320 Question Bank

131.A spoiler panel amber triangle symbol on the ECAM F/CTL page indicates that

  1. Spoiler is missing
  2. Spoiler fault deflected ✓
  3. Spoiler fault retracted
  4. Spoiler position not valid
正确答案：Spoiler fault deflected　·　A320　·　来源 Chair Flight A320 Question Bank

132.Which of the following statements is true about the sidesticks and their operation?

  1. If the aircraft is on the ground and commencing its take off with one stick deactivated, the takeoff CONFIG warning will be activated ✓
  2. A green light comes on in front of the pilot who has taken priority, if the other stick is in the neutral position
  3. If both pilots press their takeover push buttons, the pilot that presses first gets priority
正确答案：If the aircraft is on the ground and commencing its take off with one stick deactivated, the takeoff CONFIG warning will be activated　·　A320　·　来源 Chair Flight A320 Question Bank

133.Depending on the failures occuring to the flight control system or on its peripherals, control reconfigurations to certain levels can occur. These are:

  1. Primary law, secondary law and emergency law
  2. Normal law, abnormal law and emergency law
  3. Direct law, normal law and G-load law
  4. Alternate law, direct law and mechanical back-up ✓
正确答案：Alternate law, direct law and mechanical back-up　·　A320　·　来源 Chair Flight A320 Question Bank

134.On the A319 and A320,the flight controls are comprised of, among others:

  1. 5 slat surfaces per wing, 8 spoilers, 2 cruise ailerons, 1 rudder surface
  2. 8 slat surfaces, 10 spoilers, 2 ailerons, 1 rudder surface
  3. 8 slat surfaces, 2 flap surfaces, 2 rudder surfaces, 4 split elevator surfaces
  4. 10 slat surfaces, 4 flap surfaces, 1 rudder surface, 2 elevator surfaces ✓
正确答案：10 slat surfaces, 4 flap surfaces, 1 rudder surface, 2 elevator surfaces　·　A320　·　来源 Chair Flight A320 Question Bank

135.Is full rudder deflection available during all flight regimes?

  1. No, except in approach with flaps 1 selected
  2. No, it is limited as a function of speed and gradually reduces as speed increases ✓
  3. No, it is limited as a function of speed and gradually increases as speed increases
  4. Yes, except in level cruise flight
正确答案：No, it is limited as a function of speed and gradually reduces as speed increases　·　A320　·　来源 Chair Flight A320 Question Bank

136.At touchdown with reverse selected and only one landing gear strut is compressed, how will the ground spoilers extend?

  1. Fully
  2. The spoilers do not extend, unti both struts are compressed.
  3. Partially, until both main landing gear struts are compressed ✓
正确答案：Partially, until both main landing gear struts are compressed　·　A320　·　来源 Chair Flight A320 Question Bank

137.Seven flight control computers process pilot and autopilot inputs. 3 SECs are used for:

  1. Spoiler Control ✓
  2. Elevator Control
  3. Stabilizer Control
  4. Aileron Control
正确答案：Spoiler Control　·　A320　·　来源 Chair Flight A320 Question Bank

138.Regarding Alternate law and Low speed stability: An artificial low speed stability replaces the normal angle-of-attack protection. It is available for all slat/flap configurations, and the low speed stability is active from ___________ above stall warning speed, depending on the aircraft's gross weight and slats/flaps configuration.

  1. about 10 knots up to about 15 knots.
  2. about 5 knots up to about 10 knots. ✓
  3. about 5 knots up to about 15 knots.
正确答案：about 5 knots up to about 10 knots.　·　A320　·　来源 Chair Flight A320 Question Bank

139.Pitch Control Protections: The normal law protects the aircraft throughout the flight Control envelope, as follows:

  1. Manoeuvre protection • pitch attitude protection • high speed protection
  2. Manoeuvre protection • high angle of attack protection • high speed protection
  3. Load Factor limitation • pitch attitude Protection • high AOA protection • low speed protection
  4. Load Factor limitation • pitch attitude Protection • high AOA protection • high speed protection ✓
正确答案：Load Factor limitation • pitch attitude Protection • high AOA protection • high speed protection　·　A320　·　来源 Chair Flight A320 Question Bank

140.In alternate law only the yaw damping function is available. Damper authority is limited to _______ of rudder deflection.

  1. ±3°
  2. ±5° ✓
  3. ±7°
正确答案：±5°　·　A320　·　来源 Chair Flight A320 Question Bank

141.How many flight control computers process pilot and autopilot inputs according to normal, alternate, or direct flight control laws?

  1. Five
  2. Seven ✓
正确答案：Seven　·　A320　·　来源 Chair Flight A320 Question Bank

142.When the aircraft has recovered from its abnormal attitude, the flight control laws in effect are: (more than one answer may be correct)

  1. In pitch: alternate law with no protection and with autotrim.
  2. In roll: direct law is active
  3. In yaw: alternate law without protection or yaw dampening
  4. 1,2 ✓
正确答案：1,2　·　A320　·　来源 Chair Flight A320 Question Bank

143.How many control modes are there on the elevators servo jacks?

  1. Three ✓
  2. Four
正确答案：Three　·　A320　·　来源 Chair Flight A320 Question Bank

144.What would happen if your headset cable got stuck around the sidestick radio selector, thereby blocking it in the radio position for a longer period of time?

  1. The system is of a fail safe type and will deactivate any transmission immediately for the remainder flight
  2. After 30 seconds an alarm will sound only as a reminder for the crew
  3. After 20 seconds an alarm will sound and the emission will be turned off
  4. After 30 seconds an alarm will sound and the emission will be turned off. To reactivate the emission, you will have to to release and press the PTT button again ✓
正确答案：After 30 seconds an alarm will sound and the emission will be turned off. To reactivate the emission, you will have to to release and press the PTT button again　·　A320　·　来源 Chair Flight A320 Question Bank

145.Which of the following statements are correct concerning the side stick takeover push button?

  1. The last pilot to depress the push button has priority
  2. If the takeover push button is depressed for more than 40 seconds, the onside system will retain priority after the push button is released
  3. Both are correct ✓
正确答案：Both are correct　·　A320　·　来源 A320 HANDBOOK (general ATA)
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