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Airbus A320 · Powerplant 题库（142 题）

Airbus A320 机型「Powerplant」相关知识共 142 道题。想练习或模拟考试，请到 题库 · 模拟考试。
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1.The A/THR is armed on the ground provided at least one FD (Flight Director) is on by:

  1. Setting the throttles to TO/GA. ✓
  2. Engine start.
  3. Pressing the A/THR pb manually.
正确答案：Setting the throttles to TO/GA.　·　A320　·　来源 smartcockpit.com

2.How many FADECs are installed on the aircraft?

  1. Two, one per engine. ✓
  2. One, with two Engine Control Units (ECU).
  3. Four in total. Two per engine.
正确答案：Two, one per engine.　·　A320　·　来源 smartcockpit.com

3.During a manual start, how is the start valve opened?

  1. It is automatic once the ENG MASTER is placed to the ON position.
  2. By depressing the ENG MAN START pb on the overhead panel.
  3. By depressing the ENG MAN START pb on the overhead panel while the ENG MODE selector is out of the NORM position. ✓
正确答案：By depressing the ENG MAN START pb on the overhead panel while the ENG MODE selector is out of the NORM position.　·　A320　·　来源 smartcockpit.com

4.A few seconds after selecting reverse, the amber REV indication changes to green. What does this mean?

  1. The reversers have been re-stowed.
  2. The reversers are now fully deployed. ✓
  3. The reverse thrust selection has been activated by the FADEC.
  4. The reversers are unlocked.
正确答案：The reversers are now fully deployed.　·　A320　·　来源 smartcockpit.com

5.Is there any mechanical linkage between the thrust levers and the engines?

  1. There is a fiber optic backup.
  2. There is a mechanical linkage in case the ECU fails.
  3. No, it is electrically powered and hydraulically actuated.
  4. No, it is totally electrical. ✓
正确答案：No, it is totally electrical.　·　A320　·　来源 smartcockpit.com

6.In flight, both igniters are supplied, when the ENG MASTER sw is ON.

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

7.IGNITION FOR STARTING - On the ground, the ignition comes on automatically when N2 reaches _____ and cuts off automatically when N2 reaches _____.

  1. 16% and 50% ✓
  2. 12% and 50%
  3. 18% and 55%
  4. 15% and 55%
正确答案：16% and 50%　·　A320　·　来源 smartcockpit.com

8.If fuel flow data is lost for more than _____, the last two digits are dashed.

  1. One minute. ✓
  2. 45 seconds.
  3. 30 seconds.
  4. 20 seconds.
正确答案：One minute.　·　A320　·　来源 smartcockpit.com

9.When the A/THR system is in use:

  1. The throttles move automatically according to FADEC commands.
  2. The throttles can only be moved manually. ✓
  3. The throttles will move when the A/THR p/b is used.
正确答案：The throttles can only be moved manually.　·　A320　·　来源 smartcockpit.com

10.The thrust levers can only be moved manually. There are 3 detents and 2 stops on the thrust quadrant.

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

11.The Full Authority Digital Engine Control (FADEC) controls:

  1. Fuel metering.
  2. Engine limits.
  3. Automatic and manual starting.
  4. All statements are correct. ✓
正确答案：All statements are correct.　·　A320　·　来源 smartcockpit.com

12.Is any thrust lever action required if an engine failed at rotation while using FLEX takeoff power?

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

13.The ignition system is for engine starting on the ground and restarting in flight. It consists of two identical independent circuits for each engine, normally controlled by the FADEC channel A and channel B. Each FADEC channel can control both igniters.

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

14.What would happen during the takeoff roll if the thrust levers were set to the FLX/MCT detent without FLEX temperature being entered?

  1. Nothing, the thrust setting would be at FLEX since FADEC automatically calculates a reduced thrust setting.
  2. The thrust setting would be MCT and there would be no corresponding warnings.
  3. A LEVEL TWO warning would sound along with the appearance of an ECAM message. ✓
正确答案：A LEVEL TWO warning would sound along with the appearance of an ECAM message.　·　A320　·　来源 smartcockpit.com

15.Can the engines be overboosted in the TOGA position?

  1. Yes, if the autothrust function is not active.
  2. No, because the ECU provides engine protection limit by monitoring N1, N2, and HMU fuel flow adjustments. ✓
  3. No, because the EIU is responsible for monitoring N1 and N2.
正确答案：No, because the ECU provides engine protection limit by monitoring N1, N2, and HMU fuel flow adjustments.　·　A320　·　来源 smartcockpit.com

16.If a throttle is set between two detents, the FADEC selects the rating limit:

  1. Determined by the throttle position.
  2. Corresponding to the higher mode. ✓
  3. Corresponding to the lower mode.
正确答案：Corresponding to the higher mode.　·　A320　·　来源 smartcockpit.com

17.Auto Thrust System - When are the throttles in the engagement range?

  1. Both throttles are above idle but not above the CLB detent when both engines are running.
  2. A single throttle of an operating engine is above idle but not above the MCT detent when one engine is running.
  3. All statements are correct. ✓
正确答案：All statements are correct.　·　A320　·　来源 smartcockpit.com

18.During a manual start, what function does the FADEC perform?

  1. Passive monitoring of the start sequence, to close the start valve and cut off the ignition on the ground. ✓
  2. To control the start sequence and take corrective action in case of a failure or malfunction.
  3. The FADEC does not perform any function during a manual start and all actions have to be carried out by the pilots.
正确答案：Passive monitoring of the start sequence, to close the start valve and cut off the ignition on the ground.　·　A320　·　来源 smartcockpit.com

19.What is considered to be the active range of the A/THR system?

  1. During single engine operations from just above the IDLE stop to the FLX/MCT detent.
  2. During two engine operations from just above the IDLE stop to the CL detent.
  3. All statements are correct. ✓
正确答案：All statements are correct.　·　A320　·　来源 smartcockpit.com

20.You are at the start of a descent and a blue N1 arc is displayed showing the new thrust demand. When does this happen?

  1. Whenever the thrust levers are moved out of the CLIMB position.
  2. Whenever there is a power change in manual thrust.
  3. Whenever there is a power change with the autopilot engaged.
  4. Whenever there is power change with auto thrust engaged. ✓
正确答案：Whenever there is power change with auto thrust engaged.　·　A320　·　来源 smartcockpit.com

21.During an engine start sequence, the gray background on N2 disappears at about 57%. What does this indicate?

  1. The igniters are no longer being powered.
  2. The start sequence has finished and all engine parameters have stabilized. ✓
  3. The start valve air pressure has dropped.
  4. There is a start fault and a dry crank is in progress.
正确答案：The start sequence has finished and all engine parameters have stabilized.　·　A320　·　来源 smartcockpit.com

22.The FADEC system is self-powered:

  1. Above 12 % N2. ✓
  2. When AC power is fully distributed.
  3. Above 5% N1
  4. When AC power is fully distributed and above 5% N1.
正确答案：Above 12 % N2.　·　A320　·　来源 smartcockpit.com

23.The FADEC prevents the thrust from exceeding the limit for the thrust lever position in automatic mode only.

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

24.If the thrust levers are set in the idle detent, is Alpha floor protection still available?

  1. Yes. Thrust lever position is disregarded. ✓
  2. Yes. As long as A/THR appears in column five.
  3. No, because the IDLE detent is out of the A/THR active range.
正确答案：Yes. Thrust lever position is disregarded.　·　A320　·　来源 smartcockpit.com

25.For reverser actuation, the left engine uses ____ hydraulic system pressure and the right engine uses ____ hydraulic system pressure.

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

26.For an inflight start, the FADEC decides whether the engine is windmilling fast enough or needs assistance from the starter in view of current engine parameters and flight environment parameters.

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

27.While flying the airplane with A/THR active, the speed knob is pulled and turned to a selected speed that happens to be slower than Alpha prot. What speed will the airplane slow to?

  1. VLS. ✓
  2. Green Dot + 5 kt.
  3. Green dot.
  4. Green dot + 10 kt.
正确答案：VLS.　·　A320　·　来源 smartcockpit.com

28.Alpha floor protection is available:

  1. From lift off and down to 100 feet radio altitude in the landing configuration. ✓
  2. From lift off and down to 50 feet radio altitude in the landing configuration.
  3. From lift off and down to 500 feet radio altitude in the landing configuration.
  4. From lift off and down to 750 feet radio altitude in the landing configuration.
正确答案：From lift off and down to 100 feet radio altitude in the landing configuration.　·　A320　·　来源 smartcockpit.com

29.The FADEC will automatically command the reverse to stow, if at least one door is unstowed and reverse thrust is not selected while the engine is running.

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

30.When does oil quantity indication begin to pulse?

  1. The oil quantity goes below the oil advisory limit (3 QT), that corresponds to the amber mark. ✓
  2. During engine start.
  3. There is an oil quantity detector fault.
  4. The oil quantity is the red area.
正确答案：The oil quantity goes below the oil advisory limit (3 QT), that corresponds to the amber mark.　·　A320　·　来源 smartcockpit.com

31.The FADEC will automatically abort an abnormal start thereby providing engine limit protection, but will the FADEC also automatically dry crank the engine?

  1. No, that is why there is a CRANK selection on the ENG MODE selector.
  2. Yes, even if the crew interrupts the start by placing the ENG MASTER switch to OFF.
  3. Yes, as long as the ENG MASTER switch remains in the ON position. ✓
正确答案：Yes, as long as the ENG MASTER switch remains in the ON position.　·　A320　·　来源 smartcockpit.com

32.What is Alpha floor protection?

  1. It helps prevent the aircraft from stalling and protects against windshear encounters during takeoff and approach. ✓
  2. It is a function of the flight control laws to prevent the aircraft from stalling.
  3. It helps prevent the aircraft from stalling by limiting the angle of bank at low airspeeds.
  4. It helps prevent the aircraft from stalling by limiting the angle of climb at high airspeeds.
正确答案：It helps prevent the aircraft from stalling and protects against windshear encounters during takeoff and approach.　·　A320　·　来源 smartcockpit.com

33.The left column, first line of the FMA is used to indicate:

  1. If A/THR is off, armed, or active.
  2. The mode of the A/THR in use when A/THR is armed or active. ✓
  3. Amber caution messages.
  4. The thrust indication.
正确答案：The mode of the A/THR in use when A/THR is armed or active.　·　A320　·　来源 smartcockpit.com

34.The FADEC manages ____ idle modes.

  1. Four (Regulated idle, Modulated idle, Approach idle and Reverse idle).
  2. Three (Modulated idle, Approach idle and Reverse idle). ✓
  3. Two (Modulated idle and Approach idle).
正确答案：Three (Modulated idle, Approach idle and Reverse idle).　·　A320　·　来源 smartcockpit.com

35.Continuous ignition is provided automatically when:

  1. ENG ANTI ICE is selected ON and/or engine flameout is detected in flight
  2. ENG ANTI ICE is selected ON.
  3. ENG ANTI ICE is selected ON and/or engine flameout is detected in flight and/or the EIU fails. ✓
正确答案：ENG ANTI ICE is selected ON and/or engine flameout is detected in flight and/or the EIU fails.　·　A320　·　来源 smartcockpit.com

36.Verification that Autothrust (A/THR) is active can be made by:

  1. Watching the automatic movement of the thrust levers.
  2. Only when the thrust levers are set at TOGA.
  3. Only by looking at column five of the FMA. ✓
正确答案：Only by looking at column five of the FMA.　·　A320　·　来源 smartcockpit.com

37.Thrust reduction must not exceed 25 % of the full rated takeoff thrust. To meet this requirement, the flexible temperature must not be higher than ISA +60 °C(T MAX FLEX).

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

38.If the automatic start fails, the FADEC energizes both igniters at the same time during the second attempt at an engine start.

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

39.The EGT limit appears when a takeoff or a go-around mode is selected, or when the thrust reversers are selected, or if the alpha floor protection is activated.

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

40.During an automatic starting, the FADEC detects a hot start, a hung start, or a stall, but the "no light up" is not monitored.

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

41.What does this indication mean ?

  1. Alphafloor is active. ✓
  2. Alphafloor is inoperative.
  3. Alphafloor is in the alternate mode.
  4. Alphafloor is in the direct mode.
正确答案：Alphafloor is active.　·　A320　·　来源 smartcockpit.com

42.Does the FADEC provide EGT limit protection constantly?

  1. Yes, in all phases of flight.
  2. No, EGT limit protection is only available during ground auto starts. ✓
  3. No, EGT limit protection is only available during ground auto starts and single-engine operations.
正确答案：No, EGT limit protection is only available during ground auto starts.　·　A320　·　来源 smartcockpit.com

43.During engine start the amber FAULT light on the ENG MASTER panel illuminates. What does this indicate?

  1. A failure in the automatic start sequence. ✓
  2. A failure of the ENG MODE SELECTOR.
  3. A failure in the engine fire extinguishing system.
正确答案：A failure in the automatic start sequence.　·　A320　·　来源 smartcockpit.com

44.During normal operation, in what detent are the thrust levers positioned once the thrust reduction altitude has been reached?

  1. CL. ✓
  2. MCT.
  3. FLX.
  4. CRZ.
正确答案：CL.　·　A320　·　来源 smartcockpit.com

45.Is it possible to disconnect Alpha floor?

  1. No, Alpha floor protection is always available.
  2. Yes, by placing the thrust levers to IDLE.
  3. Yes, by depressing the autothrottle push button on the FCU. ✓
正确答案：Yes, by depressing the autothrottle push button on the FCU.　·　A320　·　来源 smartcockpit.com

46.Oil pressure and temperature are monitored upstream of the oil filter.

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

47.When Alpha floor is activated, what power setting is automatically commanded and what FMA annunciation would appear in Column one?

  1. TOGA / A. FLOOR. ✓
  2. CLB / CLB.
  3. MCT / THR LK.
  4. THR / LK.
正确答案：TOGA / A. FLOOR.　·　A320　·　来源 smartcockpit.com

48.Data for the FADECs is directly sourced from the ADIRS, engine sensors and thrust levers. All other required data is amalgamated and supplied by an Engine Interface Unit (EIU).

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

49.After takeoff the A/THR will not become active until:

  1. The thrust levers are placed in the CLIMB position. ✓
  2. The thrust levers are moved out of the TO/GA or FLEX/MCT detents.
  3. The autopilot is engaged.
  4. The A/THR pushbutton is manually selected ON.
正确答案：The thrust levers are placed in the CLIMB position.　·　A320　·　来源 smartcockpit.com

50.Thrust reverser system - Each pivoting door moves independently but the doors are synchronized.

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

51.There is no reverse idle detent. When the pilot moves the lever out of the idle stop by pulling up the reverse lever on the front of the thrust lever, he selects reverse idle.

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

52.What is required for the FADEC to compute a reduced thrust setting?

  1. A FLEX temperature must be entered on the INIT page of the MCDU.
  2. Nothing, it is an automatic function of the FADEC.
  3. A FLEX temperature must be entered on the TAKE OFF PERF page of the MCDU. ✓
  4. A FLEX temperature must be entered on the ENG PERF page of the MCDU.
正确答案：A FLEX temperature must be entered on the TAKE OFF PERF page of the MCDU.　·　A320　·　来源 smartcockpit.com

53.If the thrust lever is set between two detents, the FADEC selects the rating limit corresponding to the:

  1. Lower detent.
  2. Higher detent. ✓
  3. Lower or higher detent depending of the N1 RPM.
  4. Lower or higher detent depending of the N2 RPM.
正确答案：Higher detent.　·　A320　·　来源 smartcockpit.com

54.What does the FLEX represent in the FLX/MCT detent?

  1. This is a reduced thrust setting used for takeoff. ✓
  2. This is the maximum continuous thrust setting for single-engine operations.
  3. This is the thrust setting that should be chosen in the case of a single-engine go-around.
  4. This is a derated thrust according the ground temperature of the day.
正确答案：This is a reduced thrust setting used for takeoff.　·　A320　·　来源 smartcockpit.com

55.You are in the middle of a manual engine start. What are you looking for when you select ENG MASTER 2 ON?

  1. The fuel used is reset, fuel flow is indicated and IGNITION message on the E/WD.
  2. The fuel flow is reset, an igniter is powered and fuel used is indicated.
  3. The fuel used is reset, both igniters are powered and fuel flow is indicated. ✓
  4. The fuel used is reset, both igniters are powered and N2 is increasing.
正确答案：The fuel used is reset, both igniters are powered and fuel flow is indicated.　·　A320　·　来源 smartcockpit.com

56.A/THR engagement is confirmed when A/THR is displayed in _____ in the right column of the FMA.

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

57.During an automatic start, the FADEC controls:

  1. The start valves, igniters and fuel flow.
  2. The start valves, igniters, HP and LP fuel valves.
  3. The igniters and fuel flow.
  4. The start valves, igniters, HP and LP fuel valves, and fuel flow. ✓
正确答案：The start valves, igniters, HP and LP fuel valves, and fuel flow.　·　A320　·　来源 smartcockpit.com

58.Using manual thrust, the thrust lever position will determine the thrust setting for the engine.

  1. True. They will operate like conventional throttles. ✓
  2. True, but care must be taken not to overspeed the engines.
  3. False. The next higher detent will be the thrust limit.
正确答案：True. They will operate like conventional throttles.　·　A320　·　来源 smartcockpit.com

59.For manual starts, the FADEC has very limited authority to abort a start. The sole case is when on the ground and a start EGT exceedance occurs before 50% N2. In all other cases, it is the pilot's responsibility to interrupt the start sequence by either deselecting the manual start button or turning the engine master switch off as appropriate.

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

60.During the automatic start sequence of ENG 2, you notice that only igniter B is powered. Is it normal?

  1. Yes, igniter A is only used for engine anti-ice.
  2. No, normally both igniters are used for all engine starts.
  3. Yes, igniter B is always used for ENG 2 start.
  4. Yes, igniters are used alternately for engine start. ✓
正确答案：Yes, igniters are used alternately for engine start.　·　A320　·　来源 smartcockpit.com

61.The idle setting on the aircraft is capable of modulating due to certain conditions. During descent, what might cause the IDLE N1 setting to increase?

  1. The slats are extended.
  2. For a higher than normal bleed air demand or warmer than normal engine oil temp in flight.
  3. All statements are correct. ✓
正确答案：All statements are correct.　·　A320　·　来源 smartcockpit.com

62.Which steps of a manual start are being taken care of by the FADEC?

  1. Starter valve closure and ignition cut off. ✓
  2. Starter valve opening and ignition start.
  3. Starter valve closure and ignition start.
  4. Starter valve opening and ignition cut off.
正确答案：Starter valve closure and ignition cut off.　·　A320　·　来源 smartcockpit.com

63.In normal operation, autothrust is available when the thrust levers are in the range between the idle stop and CLB detent.

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

64.A/THR - Holding the instinctive disconnect pb for more than 15 seconds will:

  1. Disengage the A/THR (including Alpha Floor) until below 1000 feet AGL for the reminder of the flight.
  2. Disengage the A/THR (including Alpha Floor) until below 500 feet AGL for the reminder of the flight.
  3. Disengage the A/THR (excluding Alpha Floor) for the reminder of the flight.
  4. Disengage the A/THR (including Alpha Floor) for the reminder of the flight. ✓
正确答案：Disengage the A/THR (including Alpha Floor) for the reminder of the flight.　·　A320　·　来源 smartcockpit.com

65.The EGT red line appears between the EGT red limit and the end of the scale. The EGT red limit is:

  1. 750 deg.C
  2. 850 deg.C
  3. 900 deg.C
  4. 950 deg.C. ✓
正确答案：950 deg.C.　·　A320　·　来源 smartcockpit.com

66.For automatic starts, the FADEC opens the HP fuel valve at _____. For manual starts, the HP fuel valve opens when the engine master switch is turned on.

  1. 22% N2 on the ground and 15% N2 in flight.
  2. 15% N2 on the ground and 22% N2 in flight. ✓
  3. 10% N2 on the ground and 15% N2 in flight.
  4. 15% N2 on the ground and 10% N2 in flight.
正确答案：15% N2 on the ground and 22% N2 in flight.　·　A320　·　来源 smartcockpit.com

67.How do you arm the A/THR in flight?

  1. A/THR switch ON when throttles are in the engagement mode.
  2. A/THR switch ON when throttles are not in the engagement mode. ✓
正确答案：A/THR switch ON when throttles are not in the engagement mode.　·　A320　·　来源 smartcockpit.com

68.Maximum reverse should not be used below _____. Idle reverse is permitted down to aircraft stop.

  1. 60 kt.
  2. 70 kt. ✓
  3. 80 kt.
  4. 90 kt.
正确答案：70 kt.　·　A320　·　来源 smartcockpit.com

69.The FADEC is normally powered by:

  1. The AC aircraft electrical system.
  2. Its own magnetic alternator. ✓
  3. The DC then the AC aircraft electrical system.
  4. The DC aircraft electrical system.
正确答案：Its own magnetic alternator.　·　A320　·　来源 smartcockpit.com

70.If an A/THR disconnect switch is pushed and held for more than _____, the A/THR system is disconnected for the reminder of the flight. This includes the Alpha floor protection.

  1. 6 Seconds.
  2. 12 Seconds.
  3. 15 Seconds. ✓
  4. 18 Seconds.
正确答案：15 Seconds.　·　A320　·　来源 smartcockpit.com

71.What is the difference between variable thrust and the speed mode?

  1. In the fixed thrust mode, thrust is fixed and the elevator controls the speed. ✓
  2. In the variable thrust mode, thrust is fixed and speed is controlled by the elevator.
  3. In the fixed thrust mode, thrust is variable and speed is controlled by the elevator.
正确答案：In the fixed thrust mode, thrust is fixed and the elevator controls the speed.　·　A320　·　来源 smartcockpit.com

72.When an engine out condition is detected, autothrust is available between the idle stop and MCT/FLX detent.

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

73.How many thrust lever positions are there, and how are they labeled?

  1. There are 7 thrust levers positions: TO/GA, MCT, FLEX, CL, IDLE, REV IDLE, and MREV.
  2. There are 6 thrust levers positions: TO/GA, FLX/MCT, CL, IDLE, REV IDLE and MREV. ✓
  3. There are 5 thrust levers positions: TO/GA, FLX/MCT, CL, IDLE and REV IDLE.
  4. There are 4 thrust levers positions: TO/GA, FLX/MCT, CL, IDLE.
正确答案：There are 6 thrust levers positions: TO/GA, FLX/MCT, CL, IDLE, REV IDLE and MREV.　·　A320　·　来源 smartcockpit.com

74.The Full Authority Digital Engine Control (FADEC) controls which of the following functions:

  1. Fuel metering
  2. Engine limits
  3. Automatic and manual starting.
  4. All of the above. ✓
正确答案：All of the above.　·　A320　·　来源 quizizz.com

75.During an automatic start sequence; selecting the ENG MASTER switch to on:

  1. Closes the pack valves.
  2. Initiates the start sequence.
  3. Displays the ECAM engine page.
  4. First two statements are correct ✓
正确答案：First two statements are correct　·　A320　·　来源 quizizz.com

76.The FADEC has control during a manual engine start sequence except for:

  1. The high pressure fuel valve.
  2. The start valve.
  3. An automatic abort. ✓
正确答案：An automatic abort.　·　A320　·　来源 quizizz.com

77.Continuous ignition is automatically provided during the following:

  1. Takeoff, landing, and flight through heavy precipitation or turbulence ✓
  2. Cruise at high altitude
  3. Taxiing on the ground
  4. Engine shutdown procedures
正确答案：Takeoff, landing, and flight through heavy precipitation or turbulence　·　A320　·　来源 quizizz.com

78.Flex or TO/GA thrust is selected on the ground.

  1. Flex or TO/GA thrust is selected on the ground.
  2. ENG ANTI ICE switch is ON
  3. Engine surge or stall occurs in flight.
  4. Any of the above. ✓
正确答案：Any of the above.　·　A320　·　来源 quizizz.com

79.The A/THR is armed on the ground provided at least one FD is on by:

  1. Setting the throttles to TO/GA. ✓
  2. Automatically at engine start.
  3. With engines running; pressing the A/THR p/b manually.
正确答案：Setting the throttles to TO/GA.　·　A320　·　来源 quizizz.com

80.A/THR engagement is confirmed when “A/THR” is displayed in the right column of the FMA.

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

81.If an A/THR disconnect switch is pushed and held for more than ______ seconds; the A/THR system is disconnected for the remainder of the flight; including the _______.

  1. 10 Seconds - Alpha floor Protection
  2. 12 Seconds - Alpha floor Protection
  3. 15 Seconds - Alpha floor Protection ✓
  4. 18 Seconds - Alpha floor Protection
正确答案：15 Seconds - Alpha floor Protection　·　A320　·　来源 quizizz.com

82.Takeoff can be performed using which power settings?

  1. Any manual setting.
  2. FLEX and MCT.
  3. CLIMB and TO/GA
  4. FLEX/MCT and TO/GA. ✓
正确答案：FLEX/MCT and TO/GA.　·　A320　·　来源 quizizz.com

83.When is T.O. INHIBIT and LDG INHIBIT active?

  1. TO 750 feet AGL, LND below 1500 feet AGL.
  2. TO 1000 feet AGL, LND below 1000 feet AGL.
  3. TO 1500 feet AGL, LND below 750 feet AGL. ✓
  4. TO 1500 feet AGL, LND below 1000 feet AGL.
正确答案：TO 1500 feet AGL, LND below 750 feet AGL.　·　A320　·　来源 quizizz.com

84.You are just about to take off. You have not inserted a FLEX temperature. Can you still takeoff?

  1. Yes, by setting the thrust levers to the CLIMB detent.
  2. Yes, by setting the thrust levers to the FLEX/MCT detent.
  3. Yes, but only using the TO/GA detent. ✓
  4. Not until a FLEX temperature is inserted.
正确答案：Yes, but only using the TO/GA detent.　·　A320　·　来源 quizizz.com

85.How many FADEC’s are installed in the aircraft?

  1. Two, one per engine. ✓
  2. One, shared between both engines.
  3. Three, one for each engine and one backup.
  4. None, the aircraft does not use FADEC.
正确答案：Two, one per engine.　·　A320　·　来源 quizizz.com

86.What are the two basic modes of the A/THR system?

  1. Thrust and Mach.
  2. Thrust and speed. ✓
  3. Variable thrust and fixed speed.
  4. Mach and speed.
正确答案：Thrust and speed.　·　A320　·　来源 quizizz.com

87.How can A/THR be ARMED automatically?

  1. Whenever a takeoff or go-around is initiated with at least one flight director ON.
  2. When Alpha floor protection is activated.
  3. Both are correct. ✓
正确答案：Both are correct.　·　A320　·　来源 quizizz.com

88.Auto Thrust System: When are the throttles in the engagement range?

  1. Both throttles are above idle but not above the CLB detent when both engines are running.
  2. A single throttle of an operating engine is above idle but not above the MCT detent when one engine is running.
  3. All of the above. ✓
正确答案：All of the above.　·　A320　·　来源 quizizz.com

89.Holding the instinctive disconnect push button’s for more than fifteen seconds will:

  1. Disengage the A/THR (including Alpha Floor) until below 1000 feet AGL for the remainder of the flight.
  2. Disengage the A/THR (including Alpha Floor) until below 500 feet AGL for the remainder of the flight.
  3. Disengage the A/THR (excluding Alpha Floor) for the remainder of the flight.
  4. Disengage the A/THR (including Alpha Floor) for the remainder of the flight. ✓
正确答案：Disengage the A/THR (including Alpha Floor) for the remainder of the flight.　·　A320　·　来源 quizizz.com

90.As far as FMA annunciations are concerned, what would indicate that the A/THR system is active?

  1. The FMA displays 'A/THR' in white.
  2. The FMA displays 'A/THR' in green. ✓
  3. The FMA displays 'A/THR' in amber.
  4. The FMA displays 'A/THR' in blue.
正确答案：The FMA displays 'A/THR' in green.　·　A320　·　来源 quizizz.com

91.Which of the following statements about SPEED and A/THR indications is correct?

  1. A: “SPEED” appears in green in column one, line one. ✓
  2. B: “A/THR” changes from blue to white as shown in column five, line three.
  3. C: “A/THR” changes from white to blue in column five, line one.
  4. D: “SPEED” appears in amber in column one, line one.
正确答案：A: “SPEED” appears in green in column one, line one.　·　A320　·　来源 quizizz.com

92.If a thrust lever is set between two detents, the FADEC selects the rating limit corresponding to the higher limit.

  1. True. This limit is displayed on the upper ECAM. ✓
  2. False. For safety reasons, it always selects the rating limit corresponding to the lower limit.
正确答案：True. This limit is displayed on the upper ECAM.　·　A320　·　来源 quizizz.com

93.What abnormals would cause the FADEC to automatically abort a start?

  1. A hot start, an overtemp, a stalled start or no liftoff. ✓
  2. An engine overspeed.
  3. A hot start, a stalled start, an overtemp or APU underspeed.
  4. A hot start, an overtemp or an engine overspeed.
正确答案：A hot start, an overtemp, a stalled start or no liftoff.　·　A320　·　来源 quizizz.com

94.During an in-flight start or a manual start, will the FADEC auto abort for an abnormal?

  1. Yes. It will for an in-flight start (but not for a manual start). ✓
  2. Yes.
  3. No.
正确答案：Yes. It will for an in-flight start (but not for a manual start).　·　A320　·　来源 quizizz.com

95.For reverser actuation, the left engine uses hydraulic system pressure and the right engine uses hydraulic system pressure.

  1. Green - Yellow. ✓
  2. Yellow - Blue.
  3. Yellow - Green.
  4. Blue - Green.
正确答案：Green - Yellow.　·　A320　·　来源 quizizz.com

96.Where is the thrust reduction altitude found and is the number always the same?

  1. Column four, row three of the FMA. It will always be 1500 ft. AGL. ✓
  2. TAKE OFF PERF page of the MCDU (it can be modified).
正确答案：Column four, row three of the FMA. It will always be 1500 ft. AGL.　·　A320　·　来源 quizizz.com

97.After take off the A/THR will not become active until:

  1. The thrust levers are placed in the CLIMB position. ✓
  2. The thrust levers are moved out of the TO/GA or FLEX/MCT detents.
  3. The autopilot is engaged.
  4. The A/THR pushbutton is manually selected ON.
正确答案：The thrust levers are placed in the CLIMB position.　·　A320　·　来源 quizizz.com

98.What would happen in flight if the FADEC’s alternator failed?

  1. Automatic control of the engine would be lost.
  2. The standby channel of the ECU would take over.
  3. The FADEC would now be powered using ship’s power. ✓
  4. The FADEC would now be powered using ship’s battery power.
正确答案：The FADEC would now be powered using ship’s power.　·　A320　·　来源 quizizz.com

99.Each FADEC is a dual channel (A&B) computer providing full engine management.

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

100.In addition to when the engine is operating, when else will the FADEC be powered?

  1. When the FADEC GND PWR pb on the maintenance panel is depressed, or the ENG MASTER switch is placed to ON.
  2. When the FADEC control switch is placed to the IGN/START position.
  3. For five minutes after electrical power is applied to the aircraft, when the FADEC GND PWR pb on the maintenance panel is depressed, or when the ENG MODE control switch is placed to IGN/START position. ✓
  4. As long as electrical power is established on the aircraft, the FADEC is powered.
正确答案：For five minutes after electrical power is applied to the aircraft, when the FADEC GND PWR pb on the maintenance panel is depressed, or when the ENG MODE control switch is placed to IGN/START position.　·　A320　·　来源 quizizz.com

101.How is manual arming of the A/THR system accomplished?

  1. By pressing the A/THR pb on the FCU confirm the pushbutton illuminates green or confirm an A/THR annunciation is displayed in column 5 of the FMA. ✓
  2. By placing the thrust levers into the active range.
  3. Advance at least one thrust lever to the TOGA or FLX/MCT detent with at least one Flight Director (FD) on.
正确答案：By pressing the A/THR pb on the FCU confirm the pushbutton illuminates green or confirm an A/THR annunciation is displayed in column 5 of the FMA.　·　A320　·　来源 quizizz.com

102.During engine start the amber FAULT light on the ENG MASTER panel illuminates. This indicates:

  1. A failure in the automatic start sequence. ✓
  2. A failure of the ENG MODE SELECTOR.
  3. A failure in the engine fire extinguishing system.
正确答案：A failure in the automatic start sequence.　·　A320　·　来源 quizizz.com

103.Can Alpha-floor be disengaged while in Alpha Protection?

  1. Yes, by manually disengaging the auto throttles. ✓
  2. No, the system is designed to avoid such a disengagement.
  3. Yes, by reducing at idle one of the throttles (for more than 5 seconds)
正确答案：Yes, by manually disengaging the auto throttles.　·　A320　·　来源 quizizz.com

104.The maximum permissible N1 is the red arc, showing the prohibited or 'redline' area of operation. It begins at _________.

  1. 101%
  2. 102%
  3. 103%
  4. 104% ✓
正确答案：104%　·　A320　·　来源 Chair Flight A320 Question Bank

105.In manual start, the thrust lever position must set to idle otherwise

  1. The engine will not start
  2. The engine will rapidly accelerate to generate the thrust demanded by the TLA ✓
  3. The engine will be stuck TOGA position
  4. There will be no effect. The engine will run at idle after start until the thrust lever will be moved
正确答案：The engine will rapidly accelerate to generate the thrust demanded by the TLA　·　A320　·　来源 Chair Flight A320 Question Bank

106.On ground the engine start sequence is automatically aborted...

  1. only in case of hot or hung start
  2. There is no automatic abort sequence
  3. only In case of tailpipe fire or hot start
  4. in case of hot start, hung start, stall or no light up ✓
正确答案：in case of hot start, hung start, stall or no light up　·　A320　·　来源 Chair Flight A320 Question Bank

107.The FADEC system is:

  1. Always self powered
  2. Self powered above 15% N1 and with AC power when N1 is below 15%
  3. Self powered above 12% N2 and with AC power when N2 is below 12% ✓
  4. Always powered by the aircraft AC electrical circuit
正确答案：Self powered above 12% N2 and with AC power when N2 is below 12%　·　A320　·　来源 Chair Flight A320 Question Bank

108.In manual mode, when the thrust levers are between the climb detent and idle:

  1. N1 is frozen
  2. N1 is climb N1
  3. N1 is idle N1
  4. Each position of the thrust levers corresponds to an N1 ✓
正确答案：Each position of the thrust levers corresponds to an N1　·　A320　·　来源 Chair Flight A320 Question Bank

109.The REV green indication on the E/WD N1 indication appears when:

  1. The minimum 2 of the 4 blocker doors of the associated engine are fully deployed
  2. All 4 blocker doors of the associated engine are unlocked and a minimum of 2 blocker doors are fully deployed
  3. The thrust levers are selected to either full or idle reverse detent
  4. All 4 blocker doors of the associated engine are fully deployed ✓
正确答案：All 4 blocker doors of the associated engine are fully deployed　·　A320　·　来源 Chair Flight A320 Question Bank

110.The thrust rating limit is computed by:

  1. The FADEC according to the AP/FD mode
  2. The FMGC according to the AP/FD mode
  3. The FADEC according to the thrust lever position (TLA) ✓
  4. The FMGC according to the FADEC mode
正确答案：The FADEC according to the thrust lever position (TLA)　·　A320　·　来源 Chair Flight A320 Question Bank

111.Engine cranking may be manually selected by setting:

  1. With master switch in OFF position the mode selector to NORM and the MAN START pb to on
  2. With master switch in OFF position the mode selector to CRANK and the MAN START pb to on ✓
  3. With master switch in ON position the mode selector to CRANK and the MAN START pb to on
  4. The mode selector to CRANK and the master switch to ON
正确答案：With master switch in OFF position the mode selector to CRANK and the MAN START pb to on　·　A320　·　来源 Chair Flight A320 Question Bank

112.During the automatic start sequence of ENG 2, you notice that only igniter B is powered. Is this normal?

  1. Yes, igniter A is only used for engine anti Ice
  2. No, normally both igniters are used for all engine starts
  3. Yes, igniters are used alternately for engine start ✓
  4. Yes, igniter B is always used for ENG 2 start
正确答案：Yes, igniters are used alternately for engine start　·　A320　·　来源 Chair Flight A320 Question Bank

113.The Thrust Reverser Auto Restow Function …

  1. is inhibited on ground only.
  2. stows thrust reverser doors if N1 greater than 70%.
  3. restows the thrust reverser doors in case of hydraulic failures.
  4. is inhibited in flight and on ground, with N1 greater than 70%. ✓
正确答案：is inhibited in flight and on ground, with N1 greater than 70%.　·　A320　·　来源 Chair Flight A320 Question Bank

114.When are both igniters powered during engine start sequence?

  1. If the automatic start fails, the FADEC energizes both igniters at the same time during the second engine start attempt. ✓
  2. The FADEC is testing both igniters before selecting the one to be used.
  3. Both igniters are always used for every engine start.
  4. Engine anti-ice has been selected on prior to engine start.
正确答案：If the automatic start fails, the FADEC energizes both igniters at the same time during the second engine start attempt.　·　A320　·　来源 Chair Flight A320 Question Bank

115.During engine start sequence the gray background on N2 disappears at about 50%. What does this indicate?

  1. That the start valve air pressure has dropped.
  2. That the start sequence has finished and all engine parameters have stabilized. ✓
  3. That there is a start fault and a dry crank is in progress.
  4. That the Igniters are no longer being powered.
正确答案：That the start sequence has finished and all engine parameters have stabilized.　·　A320　·　来源 Chair Flight A320 Question Bank

116.What is the starting EGT limit?

  1. 650°C
  2. 725°C ✓
  3. 850°C
  4. 950°C
正确答案：725°C　·　A320　·　来源 Chair Flight A320 Question Bank

117.During a manual engine start sequence:

  1. Igniter A is always used
  2. Igniter B is always used
  3. Igniter A or B are used alternately
  4. Igniters A and B are used simultaneously ✓
正确答案：Igniters A and B are used simultaneously　·　A320　·　来源 Chair Flight A320 Question Bank

118.During landing, at which speed should the reversers be set to idle latest?

  1. 100 knots.
  2. 70 knots ✓
  3. 50 knots
  4. At taxi speed.
正确答案：70 knots　·　A320　·　来源 Chair Flight A320 Question Bank

119.Manual engine start is recommended in the following cases:

  1. in cold air conditions
  2. when APU bleed u/s
  3. for training purposes
  4. after aborting a start, because of engine EGT overlimit ✓
正确答案：after aborting a start, because of engine EGT overlimit　·　A320　·　来源 Chair Flight A320 Question Bank

120.The thrust levers can only be moved manually over a sector that is divided into ___ operating segments and into___ positions defined by detents or stops

  1. five, four
  2. four, four
  3. four, five ✓
  4. five, five
正确答案：four, five　·　A320　·　来源 Chair Flight A320 Question Bank

121.The IDLE CONTROL of the engine has three idle modes:

  1. regulated idle, ground idle, reverse idle
  2. modulated idle, approach idle, reverse idle ✓
  3. bleed demand idle, regulated idle, reverse idle
  4. ground idle, inflight idle, approach idle
正确答案：modulated idle, approach idle, reverse idle　·　A320　·　来源 Chair Flight A320 Question Bank

122.The following functions are provided by the FADEC during a manual engine start:

  1. Opening of the start valve when the ENG MODE selector is set to IGN/START and the MAN START pushbutton switch is pressed. The FADEC makes a passive survey of the engine during the starting sequence. ✓
  2. Positioning of the HP fuel valve and operation of both igniters when the engine master switch is turned on. The FADEC has full authority over the start sequence.
  3. For an inflight start, the FADEC decides whether the engine is windmilling fast enough or needs assistance from the starter in view of current engine parameters and flight environment.
  4. During a manual start, the FADEC never has the authority to abort the start sequence.
正确答案：Opening of the start valve when the ENG MODE selector is set to IGN/START and the MAN START pushbutton switch is pressed. The FADEC makes a passive survey of the engine during the starting sequence.　·　A320　·　来源 Chair Flight A320 Question Bank

123.Manual engine starting is recommended after aborting a start because of:

  1. Engine stall
  2. Engine EGT overlimit
  3. Low start air pressure
  4. All answers are correct ✓
正确答案：All answers are correct　·　A320　·　来源 Chair Flight A320 Question Bank

124.Which idle mode does the FADEC select in the following situation: Inflight in descent through FL250?

  1. Reverse idle
  2. Modulated idle ✓
  3. Approach idle
  4. Hard idle
正确答案：Modulated idle　·　A320　·　来源 Chair Flight A320 Question Bank

125.Which idle mode does the FADEC select in the following situation: REV are stowed after landing?

  1. It switches from reverse-idle to modulated-idle, resulting in an increase of thrust
  2. It switches from reverse-idle to ground-idle, resulting in a decrease of thrust
  3. It switches from reverse-idle to ground-idle, resulting in an increase of thrust
  4. It switches from reverse-idle to modulated-idle, resulting in a decrease of thrust ✓
正确答案：It switches from reverse-idle to modulated-idle, resulting in a decrease of thrust　·　A320　·　来源 Chair Flight A320 Question Bank

126.Which igniter channel will be used for automatic engine start?

  1. Igniter A or B are used alternately ✓
  2. Igniters A and B are used simultaneously
  3. Igniter A is always used
  4. Igniter B is always used
正确答案：Igniter A or B are used alternately　·　A320　·　来源 Chair Flight A320 Question Bank

127.For operating under ENGINE INTERMIX TYPE 1 condition, the following procedure applies:

  1. The CM1 must progressively adjust engine thrust in 2 steps. Step 1: Idle to 70% N1 - Brakes released, when the 70% N1 is stabilized on both engines; Step 2: Both engines N1 to takeoff thrust.
  2. The CM1 must progressively adjust engine thrust in 2 steps. Step 1: Idle to takeoff thrust within 5 seconds; Step 2: release brakes when takeoff thrust is stabilized on both engines.
  3. The CM1 must progressively adjust engine thrust in 2 steps. Step 1: Idle to 50% N1 - Brakes released, when the 50% N1 is stabilized on both engines; Step 2: Both engines N1 to takeoff thrust. ✓
正确答案：The CM1 must progressively adjust engine thrust in 2 steps. Step 1: Idle to 50% N1 - Brakes released, when the 50% N1 is stabilized on both engines; Step 2: Both engines N1 to takeoff thrust.　·　A320　·　来源 Chair Flight A320 Question Bank

128.During push back you start engine 2. After push back you observe the NW STRG DISC memo has changed to amber. Why?

  1. The NW STRG disconnect mechanism has failed
  2. The yellow hydraulic system is now pressurized and the amber caption is a warning not to move the hand wheel
  3. The memo has become amber because one engine is running ✓
  4. The nose wheel steering is being re-connected by ground personnel. It is amber because the pin is removed
正确答案：The memo has become amber because one engine is running　·　A320　·　来源 Chair Flight A320 Question Bank

129.Engine 2 powers:

  1. The blue system.
  2. The green system.
  3. The yellow system pump and the green system via the PTU should green system pump fail. ✓
正确答案：The yellow system pump and the green system via the PTU should green system pump fail.　·　A320　·　来源 Chair Flight A320 Question Bank

130.Which Statement about the Ram Air Turbine (RAT) is correct?

  1. The RAT does not deploy automatically
  2. The RAT deploy automatically if the BLUE hydraulic system pressure is lost only
  3. The RAT deploy automatically, if AC BUS 1 and AC BUS 2 are both lost only ✓
  4. The RAT deploy automatically, if the BLUE hydraulic system pressure is lost or If AC BUS 1 and AC BUS 2 are both lost
正确答案：The RAT deploy automatically, if AC BUS 1 and AC BUS 2 are both lost only　·　A320　·　来源 Chair Flight A320 Question Bank

131.After deploying the ram air turbine (RAT), is it possible to check its position and status?

  1. Yes, check to see if the blue system ELEC PUMP OFF light is illuminated or the “RAT” Memo on the upper ECAM Display
  2. Yes, on the ECAM ELEC page and in the MEMO of the upper ECAM (RAT OUT)
  3. Yes, on the ECAM HYD page and in the MEMO of the upper ECAM (RAT OUT) ✓
  4. No, it is not possible
正确答案：Yes, on the ECAM HYD page and in the MEMO of the upper ECAM (RAT OUT)　·　A320　·　来源 Chair Flight A320 Question Bank

132.The green pump pressure is low (inhibited on the ground, when the engine is stopped). The FAULT light goes out, when the crew selects OFF, except during an overheat.

  1. True ✓
  2. False
正确答案：True　·　A320　·　来源 Chair Flight A320 Question Bank

133.In case on an engine 1 failure at lift-off....

  1. All hydraulic systems remain available but the landing gear retraction is rate reduced because the green system capacity is limited due to the PTU
  2. All hydraulic systems remain fully available, only the G ENG 1 PUMP is inop ✓
  3. The only normal working hydraulic system remains the yellow. The green system is flow limited via the PTU and the blue system is lost as a consequence of the loss of generator 1
  4. The only normal working hydraulic system remains the yellow. The green system is flow limited via the PTU
正确答案：All hydraulic systems remain fully available, only the G ENG 1 PUMP is inop　·　A320　·　来源 Chair Flight A320 Question Bank

134.If FDs are engaged in DES or OPEN DES mode or EXP DES (if installed) and if the pilot does not follow the FD bars to maintain the commanded descent _______________, (pitch too high and autothrust in IDLE).

  1. The aircraft accelerates.
  2. The aircraft decelerates. ✓
正确答案：The aircraft decelerates.　·　A320　·　来源 Chair Flight A320 Question Bank

135.What does the autothrust system do, if it is active:

  1. Maintains a specific thrust in THRUST mode
  2. Controls the aircraft speed or MACH in SPEED/MACH mode
  3. Uses ALPHA FLOOR mode to set maximum thrust when the aircraft angle of attack exceeds a specific threshold
  4. All answers are correct ✓
正确答案：All answers are correct　·　A320　·　来源 Chair Flight A320 Question Bank

136.ALPHA FLOOR is a protection that commands ___ thrust, regardless of the thrust levers’ positions. This protection is available from lift-off to ___ ft RA on approach

  1. MCT / 100ft RA
  2. TOGA / 100ft RA ✓
  3. MCT / 50ft RA
  4. TOGA / 50ft RA
正确答案：TOGA / 100ft RA　·　A320　·　来源 Chair Flight A320 Question Bank

137.What happens when the EIU (Engine Interface Unit) power supply circuit breakers are pulled?

  1. The engine anti-ice valve closes
  2. The engine anti-ice valve opens (simulating a loss of electrical power) ✓
  3. The engine will automatically shut down
  4. The FADEC will use the alternate air source
正确答案：The engine anti-ice valve opens (simulating a loss of electrical power)　·　A320　·　来源 Em42 A320 FAM ATA 30,35,29

138.Is it possible to stow the Ram Air Turbine (RAT) in flight?

  1. Yes, by pressing the RAT MAN ON button again
  2. No, it is not, An interlock mechanism will only permit RAT stowage if the blades are properly aligned, this condition can only be accomplish on ground ✓
  3. Yes, it stows automatically when the aircraft exceeds 250 knots
  4. No, it stows automatically when the blue electric pump is turned on
正确答案：No, it is not, An interlock mechanism will only permit RAT stowage if the blades are properly aligned, this condition can only be accomplish on ground　·　A320　·　来源 Em42 A320 FAM ATA 30,35,29

139.What is the function of the interlock mechanism in the Ram Air Turbine?

  1. The interlock mechanism will only permit RAT stowage if the blades are properly aligned; it also prevents rotation when stowed ✓
  2. The interlock mechanism will only permit RAT deployment if the blades are properly aligned; it also prevents rotation when stowed
  3. The interlock mechanism will only permit RAT stowage if the blades are properly aligned; it also permit rotation when stowed
正确答案：The interlock mechanism will only permit RAT stowage if the blades are properly aligned; it also prevents rotation when stowed　·　A320　·　来源 Em42 A320 FAM ATA 30,35,29

140.In flight, either the AP/FD pitch control, or autothrust may acquire and hold a target speed or Mach number, depending on the engaged modes. Speed control is “Managed” when the target comes from the SPD/MACH FCU window

  1. true
  2. false ✓
正确答案：false　·　A320　·　来源 A320 HANDBOOK (general ATA)

141.What is the FADEC?

  1. An engine speed control box
  2. A thrust control unit
  3. A Full Authority Digital Engine Control unit ✓
  4. A Front Access Direct Engine Compartment
正确答案：A Full Authority Digital Engine Control unit　·　A320　·　来源 A320 HANDBOOK (general ATA)

142.REV GREEN appears on the N1 indicator when?

  1. The thrust levers are selected to full reverse sector
  2. The thrust reverser system is fully deployed ✓
  3. The thrust lever position is in the idle reverse sector
  4. Ground spoilers extend
正确答案：The thrust reverser system is fully deployed　·　A320　·　来源 A320 HANDBOOK (general ATA)
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