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Boeing 737 · Auto Flight 题库（227 题）

Boeing 737 机型「Auto Flight」相关知识共 227 道题。想练习或模拟考试，请到 题库 · 模拟考试。
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1.The STAB OUT OF TRIM light operates

  1. Only when the speed trim system is activated.
  2. At any time.
  3. Only when the autopilot is engaged. ✓
正确答案：Only when the autopilot is engaged.　·　737　·　来源 b737.org.uk

2.If the autopilot disengage light is flashing amber, this indicates that

  1. The autopilot has reverted to CWS pitch or roll while in CMD. ✓
  2. The autopilot has reverted to CMD pitch or roll while in CWS.
  3. The light test switch is being held in position 2.
正确答案：The autopilot has reverted to CWS pitch or roll while in CMD.　·　737　·　来源 b737.org.uk

3.If the autothrottle disengagement light is flashing amber, this indicates

  1. The light test switch is being held in position 2.
  2. An autothrottle airspeed error if speed is not held within +15 or -15 knots of commanded speed when in flight, flaps up and autothrottle engaged in MCP SPD or FMC SPD mode.
  3. An autothrottle airspeed error if speed is not held within +10 or -5 knots of commanded speed when in flight, flaps not up and autothrottle engaged in MCP SPD or FMC SPD mode. ✓
正确答案：An autothrottle airspeed error if speed is not held within +10 or -5 knots of commanded speed when in flight, flaps not up and autothrottle engaged in MCP SPD or FMC SPD mode.　·　737　·　来源 b737.org.uk

4.VNAV mode is terminated by

  1. Selecting a different pitch mode or Localiser capture or Extending the wing flaps beyond 5 degrees.
  2. Selecting a different pitch mode or Glideslope capture or Extending the wing flaps beyond 15 degrees. ✓
  3. Selecting a different pitch mode or Glideslope capture or De-selecting LNAV or Extending the wing flaps beyond 25 degrees.
正确答案：Selecting a different pitch mode or Glideslope capture or Extending the wing flaps beyond 15 degrees.　·　737　·　来源 b737.org.uk

5.If during a climb with autopilot engaged, the ALT HOLD switch is pressed, the aircraft will

  1. Continue the climb to the next 1000 feet level and level off.
  2. Stop the climb and level off. ✓
  3. Continue the climb to the preset altitude selected, as the altitude acquire mode is now armed.
正确答案：Stop the climb and level off.　·　737　·　来源 b737.org.uk

6.With autopilot A engaged, the altitude selected on the MCP is referenced to

  1. The First Officer's altimeter.
  2. The Captain's altimeter. ✓
  3. The standby altimeter.
正确答案：The Captain's altimeter.　·　737　·　来源 b737.org.uk

7.VNAV climbs and descents are

  1. Constrained by the selected MCP altitude. ✓
  2. Not constrained by the selected MCP altitude.
  3. Constrained by the selected cabin altitude.
正确答案：Constrained by the selected MCP altitude.　·　737　·　来源 b737.org.uk

8.When intercepting the ILS with APP mode armed

  1. On some airplanes, glideslope may be captured prior to localizer. ✓
  2. On all airplanes, localizer must be captured prior to glideslope.
  3. The second autopilot can be engaged.
正确答案：On some airplanes, glideslope may be captured prior to localizer.　·　737　·　来源 b737.org.uk

9.During a dual channel approach the second autopilot must be engaged in CMD by

  1. 800 feet radio altitude. ✓
  2. 500 feet radio altitude.
  3. 1500 feet radio altitude.
正确答案：800 feet radio altitude.　·　737　·　来源 b737.org.uk

10.The bank angle limit selector sets the limit of bank angle when using

  1. All roll modes.
  2. LNAV and heading select modes.
  3. Heading select and VOR modes. ✓
正确答案：Heading select and VOR modes.　·　737　·　来源 b737.org.uk

11.If FLARE arm is not annunciated by approximately 350 feet radio altitude

  1. Reselect APP mode on the MCP.
  2. The second engaged autopilot will disengage automatically.
  3. Both autopilots will disconnect automatically. ✓
正确答案：Both autopilots will disconnect automatically.　·　737　·　来源 b737.org.uk

12.During a dual channel approach, the autothrottle begins retarding the thrust at approximately

  1. 50 feet radio altitude.
  2. 27 feet radio altitude. ✓
  3. 10 feet radio altitude.
正确答案：27 feet radio altitude.　·　737　·　来源 b737.org.uk

13.During a dual channel go-around, the MCP IAS/Mach display will

  1. Display the Vref speed used during the final approach.
  2. Display the flap manoeuvring speed.
  3. Become blank. ✓
正确答案：Become blank.　·　737　·　来源 b737.org.uk

14.Flight Director roll commands, from take-off mode engagement through to the take-off climbout, are

  1. To hold the wings level. ✓
  2. To maintain the heading selected in the heading window.
  3. To maintain the runway track.
正确答案：To hold the wings level.　·　737　·　来源 b737.org.uk

15.The conditions for engaging the flight director in go-around mode are

  1. The F/D switches must be ON, inflight below 2,000 feet RA-and not in take-off mode, and the TO/GA switch pressed.
  2. The F/D switches can be ON or OFF, inflight below 2,000 feet RA and not in take-off mode, and the TO/GA switch pressed. ✓
  3. The F/D switches must be ON, inflight below 800 feet RA-and not in take-off mode, and the TO/GA switch pressed.
正确答案：The F/D switches can be ON or OFF, inflight below 2,000 feet RA and not in take-off mode, and the TO/GA switch pressed.　·　737　·　来源 b737.org.uk

16.The Flight Director Comparator monitors

  1. The symbol generators.
  2. The IRS headings.
  3. The command bar positions. ✓
正确答案：The command bar positions.　·　737　·　来源 b737.org.uk

17.The Altitude Alerting system is inhibited whenever

  1. The wing flaps are extended past 15 or while the glideslope is captured.
  2. The wing flaps are extended past 25 or while the glideslope is captured. ✓
  3. The glideslope is captured.
正确答案：The wing flaps are extended past 25 or while the glideslope is captured.　·　737　·　来源 b737.org.uk

18.If an engine fails while the autothrottle is in N1 mode, the thrust lever of the failed engine

  1. Advances a few degrees and returns to or below the other thrust lever position. ✓
  2. Retracts a few degrees and returns to or above the other thrust lever position.
  3. Remains stationary.
正确答案：Advances a few degrees and returns to or below the other thrust lever position.　·　737　·　来源 b737.org.uk

19.During a dual channel approach the autothrottle

  1. Must be disengaged manually.
  2. Automatically disengages approximately 10 seconds after the landing touchdown.
  3. Automatically disengages approximately 2 seconds after the landing touchdown. ✓
正确答案：Automatically disengages approximately 2 seconds after the landing touchdown.　·　737　·　来源 b737.org.uk

20.If the MCP displayed altitude changes without altitude selector movement

  1. A warning will be given in the form of intermittent altitude alert tone, flashing altitude alert lights and the MCP displays 50,000 feet. ✓
  2. No warnings are given.
  3. A warning will be given in the form of the aircraft climbing or descending to the new altitude.
正确答案：A warning will be given in the form of intermittent altitude alert tone, flashing altitude alert lights and the MCP displays 50,000 feet.　·　737　·　来源 b737.org.uk

21.The underspeed symbol in the MCP Speed window is a

  1. Flashing "A". ✓
  2. Steady "A".
  3. Flashing "8".
正确答案：Flashing "A".　·　737　·　来源 b737.org.uk

22.During a dual channel autopilot approach, the Autopilot Disengage light illuminates steady red when below 800 feet. This indicates

  1. The stabilizer is out of trim. ✓
  2. A normal condition.
  3. Both autopilots have reverted to CWS mode.
正确答案：The stabilizer is out of trim.　·　737　·　来源 b737.org.uk

23.During an autopilot go-around, the Autopilot Disengage light illuminates steady red. This indicates

  1. A normal condition.
  2. The altitude acquire mode is inhibited (Stabilizer not trimmed for single A/P operation). ✓
  3. One or more autopilots have reverted to CWS mode.
正确答案：The altitude acquire mode is inhibited (Stabilizer not trimmed for single A/P operation).　·　737　·　来源 b737.org.uk

24.If the autothrottle is engaged and an autothrottle disengage switch is pressed

  1. The autothrottle disengages.The A/T disengage lightsflash and the A/T ARM switch trips OFF. A second press and the A/T disengage lights extinguish. ✓
  2. The autothrottle disengages.The A/T disengage lightsflash, the A/T disengage warning tone sounds and the A/T ARM switch trips OFF. A second press and the A/T disengage lights extinguish and the warning tone.
  3. The autothrottle disengages provided the button is held formore than two seconds. The A/T disengage lights flash and the A/T ARM switch trips OFF. A second press and the A/T disengage lights extinguish.
正确答案：The autothrottle disengages.The A/T disengage lightsflash and the A/T ARM switch trips OFF. A second press and the A/T disengage lights extinguish.　·　737　·　来源 b737.org.uk

25.What is the minimum Mach number that can be selected in the IAS/MACH display of the MCP panel

  1. 0.40 M
  2. 0.50 M
  3. 0.60 M ✓
正确答案：0.60 M　·　737　·　来源 b737.org.uk

26.The IAS/MACH display change over switch on the MCP panel will change the display between IAS and MACH when pressed. An automatic change over

  1. Occurs at approximately FL260. ✓
  2. Does not occur.
  3. Occurs at approximately FL350.
正确答案：Occurs at approximately FL260.　·　737　·　来源 b737.org.uk

27.During Autopilot CWS operation above 1500 feet RA, if the roll control force is released with less than 6 degrees of bank, the autopilot will

  1. Roll wings level only.
  2. Roll wings level and hold existing heading. ✓
  3. Remain at the same bank angle.
正确答案：Roll wings level and hold existing heading.　·　737　·　来源 b737.org.uk

28.The mode selector switches on the MCP panel will illuminate the letters ON to indicate that

  1. The mode can be deactivated by pressing the mode switch a second time. ✓
  2. The mode can be deactivated by selecting either F/D switch to OFF.
  3. The mode can not be deactivated by pressing the mode switch a second time.
正确答案：The mode can be deactivated by pressing the mode switch a second time.　·　737　·　来源 b737.org.uk

29.If the MCP selected Altitude is changed during ALT ACQ mode

  1. Then V/S mode is automatically activated. ✓
  2. The initial selected altitude is held.
  3. The pitch mode prior to ALT ACQ is automatically re-engaged.
正确答案：Then V/S mode is automatically activated.　·　737　·　来源 b737.org.uk

30.LNAV mode terminates whenever

  1. HDG SEL mode is engaged only.
  2. Either HDG SEL, VOR or LOC mode is armed.
  3. HDG SEL mode is engaged or upon VOR or LOC capture. ✓
正确答案：HDG SEL mode is engaged or upon VOR or LOC capture.　·　737　·　来源 b737.org.uk

31.A rectangle is drawn around each pitch, roll, CWS and thrust engaged mode annunciation (EFIS Flight Mode Annunciations) whenever

  1. A mode change has occurred and the rectangle remains for 1 second.
  2. A mode change has occurred and the rectangle remains for 10 seconds. ✓
  3. A mode change occurs from active to armed, and the rectangle remains for 10 seconds.
正确答案：A mode change has occurred and the rectangle remains for 10 seconds.　·　737　·　来源 b737.org.uk

32.An A/T LIM light when illuminated, or an A/T LIM annunciation (as installed) indicates

  1. The autothrottle computer is calculating a degraded N1 limit for the affected engine or engines. ✓
  2. The autothrottle computer is calculating an FMC N1 limit for the affected engine or engines.
  3. The autothrottles are positioned at their normal operating limit as calculated by the FMC.
正确答案：The autothrottle computer is calculating a degraded N1 limit for the affected engine or engines.　·　737　·　来源 b737.org.uk

33.All AFDS modes can be disengaged by selecting another command mode or

  1. By turning the F/Ds off with the autopilot engaged.
  2. By disengaging the A/P only.
  3. By disengaging the A/P and turning the F/Ds off. ✓
正确答案：By disengaging the A/P and turning the F/Ds off.　·　737　·　来源 b737.org.uk

34.What criteria must be met before autopilot engagement

  1. The Stabiliser Trim Auto Pilot Cut-Out Switch is at NORMAL only.
  2. No force is applied to the control wheel or column and the Stabiliser Trim Auto Pilot Cut-Out Switch is at NORMAL. ✓
  3. No force is applied to the control wheel or column, the Stabiliser Trim Auto Pilot Cut-Out Switch is at NORMAL and the autothrottle must be engaged.
正确答案：No force is applied to the control wheel or column and the Stabiliser Trim Auto Pilot Cut-Out Switch is at NORMAL.　·　737　·　来源 b737.org.uk

35.If the autopilot is engaged and either pilot's control wheel Trim Switch is activated

  1. The autopilot will disengage. ✓
  2. The stabiliser will move at a slow rate with the autopilot remains engaged.
  3. The stabiliser will not move and the autopilot remains engaged.
正确答案：The autopilot will disengage.　·　737　·　来源 b737.org.uk

36.When approaching a selected altitude in CWS P (pitch) with the autopilot engage paddle in CMD

  1. The autopilot paddle automatically moves to the CWS position on reaching the selected altitude.
  2. The CWS P annunciation is unaffected.
  3. The CWS P annunciation changes to ALT ACQ and when at the selected altitude, ALT HOLD engages. ✓
正确答案：The CWS P annunciation changes to ALT ACQ and when at the selected altitude, ALT HOLD engages.　·　737　·　来源 b737.org.uk

37.The autopilot is engaged in ALT HOLD mode. The controlcolumn is then pushed, causing the autopilot to engage in CWS P mode. After the aircraft has descended 150 feet from the initial altitude the force applied to the control column is released and

  1. CWS P mode changes to ALT ACQ mode and the A/P remains atthe an altitude of 150 feet lower than the initial altitude and ALT HOLD engages.
  2. CWS P remains engaged and the aircraft will maintain a constant pitch angle in the descent.
  3. CWS P mode changes to ALT ACQ mode and the A/P returns to the initial altitude and ALT HOLD engages. ✓
正确答案：CWS P mode changes to ALT ACQ mode and the A/P returns to the initial altitude and ALT HOLD engages.　·　737　·　来源 b737.org.uk

38.During a VNAV PATH descent, VNAV remains engaged until

  1. Glideslope capture, or Another pitch mode is selected, or Flaps are extended beyond 25, or LNAV is disengaged without localiser capture.
  2. Glideslope capture, or Another pitch mode is selected, or Flaps are extended beyond 15, or LNAV is disengaged without localiser capture. ✓
  3. Approach mode is armed, or Another pitch mode is selected, or Flaps are extended beyond 25, or LNAV is disengaged without localiser capture.
正确答案：Glideslope capture, or Another pitch mode is selected, or Flaps are extended beyond 15, or LNAV is disengaged without localiser capture.　·　737　·　来源 b737.org.uk

39.If VOR/LOC mode is fully engaged during an ILS approach and then the master VHF NAV receiver is placed in the AUTO tuning mode

  1. The VOR/LOC mode remains engaged.
  2. The VOR/LOC mode automatically disengages. ✓
  3. The go-around is initiated automatically without pressing either TOGA switch.
正确答案：The VOR/LOC mode automatically disengages.　·　737　·　来源 b737.org.uk

40.Dual autopilot engagement is possible

  1. Provided that both NAV receivers are tuned to the ILS frequency, APP mode is selected and the aircraft is above 800 feet RA. ✓
  2. At any time below 1500 feet RA.
  3. Provided that both NAV receivers are tuned to the ILS frequency, VOR/LOC mode is selected and the aircraft is above 800 feet RA.
正确答案：Provided that both NAV receivers are tuned to the ILS frequency, APP mode is selected and the aircraft is above 800 feet RA.　·　737　·　来源 b737.org.uk

41.After LOC and G/S are both captured, the APP mode can be exited by

  1. Disengaging the autopilot only.
  2. Pressing the APP mode switch.
  3. Pressing a TOGA switch. ✓
正确答案：Pressing a TOGA switch.　·　737　·　来源 b737.org.uk

42.During a Dual Channel Autoland Approach, the autopilots were disengaged at 200 feet RA and

  1. Forward control column force may be required to hold the desired pitch attitude. ✓
  2. Aft control column force may be required to hold the desired pitch attitude.
  3. No additional control column force would be required to hold the desired pitch attitude.
正确答案：Forward control column force may be required to hold the desired pitch attitude.　·　737　·　来源 b737.org.uk

43.If the Autothrottle is engaged during a touchdown

  1. It will automatically disengage approximately 2 seconds after touchdown. ✓
  2. It will automatically disengage approximately 5 seconds after touchdown.
  3. It will not automatically disengage after touchdown and should be manually disengaged.
正确答案：It will automatically disengage approximately 2 seconds after touchdown.　·　737　·　来源 b737.org.uk

44.During a Dual Channel Autoland, the autopilots

  1. May be manually disengaged after touchdown. The landing roll-out can be executed automatically.
  2. Must be manually disengaged after touchdown. The landing roll-out is executed manually after disengaging the A/P. ✓
  3. Must not be disengaged after touchdown until the airspeed is less than 60 knots.
正确答案：Must be manually disengaged after touchdown. The landing roll-out is executed manually after disengaging the A/P.　·　737　·　来源 b737.org.uk

45.The A/P go-around mode requires dual A/P operation and becomes armed when

  1. LOC and GS capture is annunciated.
  2. FLARE armed is annunciated. ✓
  3. A flap setting of 15 or more is selected.
正确答案：FLARE armed is annunciated.　·　737　·　来源 b737.org.uk

46.Upon Go-Around engagement during a fully automatic approach the autothrottles will

  1. Disengage.
  2. Advance the thrust levers toward the maximum go around N1.
  3. Advance the thrust levers toward the reduced go-around N1. ✓
正确答案：Advance the thrust levers toward the reduced go-around N1.　·　737　·　来源 b737.org.uk

47.During an ILS approach with both flight directors ON

  1. The F/D command bars retract from view at approximately 200 feet RA.
  2. The F/D command bars retract from view at approximately 50 feet RA. ✓
  3. The F/D command bars remain in view until after touchdown, giving full landing flare capability.
正确答案：The F/D command bars retract from view at approximately 50 feet RA.　·　737　·　来源 b737.org.uk

48.Both MA lights on the MCP panel are illuminated during an approach indicating

  1. Independent Flight Director operation. ✓
  2. A Flight Director malfunction.
  3. Go-around mode is armed.
正确答案：Independent Flight Director operation.　·　737　·　来源 b737.org.uk

49.A takeoff is commenced with both Flight Directors selected OFF. At 100 knots IAS a TOGA switch is pressed. What will happen to the F/D ?

  1. The F/D engages in full go-around mode.
  2. The F/D command bars automatically appear for both pilots. ✓
  3. The F/D command bars remain out of view.
正确答案：The F/D command bars automatically appear for both pilots.　·　737　·　来源 b737.org.uk

50.The Altitude Alerting system consists of a momentary tone and illumination of the Altitude Alert lights when approaching the selected altitude. The alert will occur when

  1. Approaching 500 feet of the selected altitude and the lights will extinguish at 250 feet from the selected altitude.
  2. Approaching 750 feet of the selected altitude and the lights will extinguish at 100 feet from the selected altitude.
  3. Approaching 900 feet of the selected altitude and the lights will extinguish at 300 feet from the selected altitude. ✓
正确答案：Approaching 900 feet of the selected altitude and the lights will extinguish at 300 feet from the selected altitude.　·　737　·　来源 b737.org.uk

51.Autothrottle takeoffs

  1. May only be performed with both PMCs ON.
  2. May be performed with both PMCs ON or both PMCs OFF. ✓
  3. May be performed with any combination of PMCs.
正确答案：May be performed with both PMCs ON or both PMCs OFF.　·　737　·　来源 b737.org.uk

52.The recommended Autothrottle approach speed setting is

  1. VREF + 5 knots. ✓
  2. VREF + increments due to wind or gusty conditions.
  3. VREF + 10 knots.
正确答案：VREF + 5 knots.　·　737　·　来源 b737.org.uk

53.The Automatic Flight System (AFS) provides speed, pitch and thrust commands to avoid exceeding the following limit speeds

  1. Vmo / Mmo. Wing flap placard. Turbulence penetration. Minimum speed (maximum angle of attack).
  2. Vmo / Mmo. Minimum speed (maximum angle of attack).
  3. Vmo / Mmo. Wing flap placard. Landing gear placards. Minimum speed (maximum angle of attack). ✓
正确答案：Vmo / Mmo. Wing flap placard. Landing gear placards. Minimum speed (maximum angle of attack).　·　737　·　来源 b737.org.uk

54.Which radio altimeter provides radio altitude to the autothrottle

  1. The First Officer's.
  2. The Captain's. ✓
  3. Both the Captain's and the First Officer's.
正确答案：The Captain's.　·　737　·　来源 b737.org.uk

55.Dual channel Autopilot operation is possible

  1. Only when two generators are powering the busses. ✓
  2. When AC power is available to at least one generator bus.
  3. Without any generator busses being energised.
正确答案：Only when two generators are powering the busses.　·　737　·　来源 b737.org.uk

56.The Autothrottle sets take-off thrust prior to

  1. 64 knots groundspeed during the take-off roll.
  2. 60 knots groundspeed during the take-off roll.
  3. 60 knots IAS during the take-off roll. ✓
正确答案：60 knots IAS during the take-off roll.　·　737　·　来源 b737.org.uk

57.During a single Autopilot approach, a Go-around is initiated by pressing a TOGA button. This causes

  1. The autopilot to remain engaged throughout the go-around.
  2. The autopilot to disengage. ✓
  3. The autothrottle to disengage.
正确答案：The autopilot to disengage.　·　737　·　来源 b737.org.uk

58.LNAV capture criteria is satisfied when

  1. The aircraft is within 3 nm of the active route segmentirrespective of heading, or The aircraft is greater than 3 nm from the active route segment but the heading is on a intercept course of 90 degrees or less and will intercept the route segment before the active waypoint. ✓
  2. The aircraft is within 5 nm of the active route segmentirrespective of heading, orThe aircraft is greater than 5 nm. from the active route segment but the heading is on a intercept course of 90degrees or less and will intercept the route segment before the active waypoint.
  3. The aircraft is greater than 5 nm from the active route segment but the heading is on a intercept course of 60 degrees or less and will intercept the route segment before the active waypoint.
正确答案：The aircraft is within 3 nm of the active route segmentirrespective of heading, or The aircraft is greater than 3 nm from the active route segment but the heading is on a intercept course of 90 degrees or less and will intercept the route segment before the active waypoint.　·　737　·　来源 b737.org.uk

59.The Autothrottle is engaged in FMC speed mode. What is displayed in the IAS/MACH display of the MCP

  1. The FMC demanded speed.
  2. Blank. ✓
  3. The aircraft's actual speed.
正确答案：Blank.　·　737　·　来源 b737.org.uk

60.When operating in "ALT HOLD", the V/S mode is ARMED if the MCP altitude is changed by more than

  1. 200 feet.
  2. 100 feet. ✓
  3. 500 feet.
正确答案：100 feet.　·　737　·　来源 b737.org.uk

61.The aircraft is climbing with the autopilot in CMD and the pilot pushes the control column forward. The autopilot will

  1. Totally disengage.
  2. Revert to CWS P and CWS R.
  3. Revert to CWS P and the Roll axis remains in CMD. ✓
正确答案：Revert to CWS P and the Roll axis remains in CMD.　·　737　·　来源 b737.org.uk

62.During a single engine F/D go-around

  1. The autothrottle will increase thrust to the full N1 limit. ✓
  2. The autothrottle will increase thrust to the reduced thrust go-around thrust setting.
  3. The autothrottle will disengage.
正确答案：The autothrottle will increase thrust to the full N1 limit.　·　737　·　来源 b737.org.uk

63.The Flight Director Comparator monitors:

  1. The symbol generators.
  2. The IRS headings.
  3. The command bar positions. ✓
正确答案：The command bar positions.　·　MAX　·　来源 smartcockpit.com

64.For dual autopilot operation, both VHF NAV receivers must be tuned to the ILS frequency and both autopilots must be selected in CMD prior to _____

  1. 800 feet RA. ✓
  2. 1 200 ft RA.
  3. 1 000 ft RA.
  4. 950 ft RA.
正确答案：800 feet RA.　·　MAX　·　来源 smartcockpit.com

65.Minimum speed reversion is also available when the Autothrottle is OFF and the AFDS is in ALT HOLD or after GS capture.rnrn

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

66.Automatic Flight Approach and Landing - If FLARE is not armed by approximately _____, both autopilots automatically disengage.

  1. 250 ft RA.
  2. 350 feet RA. ✓
  3. 400 ft RA.
  4. 500 ft RA.
正确答案：350 feet RA.　·　MAX　·　来源 smartcockpit.com

67.The white AT LIM symbol appears on the upper display unit. What is the correct statement?

  1. The autothrottle has reached the thrust limit for the selected assumed temperature.
  2. The N1 has been manually set and not by the FMC, therefore the AT LIM will be illuminated.
  3. The AT is using the upgraded BLT performance information.
  4. The FMC is not providing autothrottle with N1 limit values. ✓
正确答案：The FMC is not providing autothrottle with N1 limit values.　·　MAX　·　来源 smartcockpit.com

68.If engaged the autothrottle will disengage ____ after landing touchdown.rn

  1. 2 seconds ✓
  2. 5 seconds
  3. 7 seconds
  4. 6 seconds
正确答案：2 seconds　·　MAX　·　来源 smartcockpit.com

69.If the autopilot is engaged and either pilot's control wheel Trim Switch is activated:

  1. The stabiliser will move at a slow rate with the autopilot remains engaged.
  2. The autopilot will disengage. ✓
  3. The stabiliser will not move and the autopilot remains engaged.
正确答案：The autopilot will disengage.　·　MAX　·　来源 smartcockpit.com

70.With the AT Arm switch at ARM, the AT gou2013around mode is armed:

  1. When descending below 2000 feet RA, when above 2000 feet RA with flaps not up or G/S captured, with or without the AFDS engaged. ✓
  2. When descending below 2500 feet RA, when above 2000 feet RA with flaps not up or G/S captured, with the AFDS engaged.
  3. When descending below 2000 feet RA, with G/S captured, with or without the AFDS engaged.
  4. When descending below 2000 feet RA, when above 2000 feet RA with flaps not up or G/S captured, with the AFDS engaged.
正确答案：When descending below 2000 feet RA, when above 2000 feet RA with flaps not up or G/S captured, with or without the AFDS engaged.　·　MAX　·　来源 smartcockpit.com

71.LNAV arming criteria on the ground:

  1. Origin runway in flight plan, active route entered in FMC, track of first leg within 5 degrees of runway heading, LNAV selected prior to TOGA. ✓
  2. Origin runway in flight plan, active route entered in FMC, LNAV selected prior to TOGA.
  3. Origin runway in flight plan, active route entered in FMC, itrack of first leg within 7 degrees of runway track, LNAV selected prior to TOGA.
  4. Origin runway in flight plan, active route entered in FMC, track of first leg within 8 degrees of runway heading, LNAV selected prior to TOGA.
正确答案：Origin runway in flight plan, active route entered in FMC, track of first leg within 5 degrees of runway heading, LNAV selected prior to TOGA.　·　MAX　·　来源 smartcockpit.com

72.The following annunciation provide the flight crew with autoland system mode and status:

  1. LAND 3 means two autopilots, two inertial sources at least and the associated sensors are operating normally for an automatic landing
  2. LAND 3 means two autopilots, three inertial sources at least and the associated sensors are operating normally for an automatic landing
  3. LAND 3 means two autopilots, three inertial sources and the associated sensors are operating normally for an automatic landing and rollout. ✓
  4. LAND 3 means two autopilots, three inertial sources, the associated sensors are operating normally for an automatic landing and rollout and at least one FMS is operative.
正确答案：LAND 3 means two autopilots, three inertial sources and the associated sensors are operating normally for an automatic landing and rollout.　·　MAX　·　来源 smartcockpit.com

73.When control wheel pressure is released during CWS roll operation, the airplane will roll wings level when the bank angle is:

  1. 5 degrees or less
  2. 6 degrees or less ✓
  3. 10 degrees or less
  4. 15 degrees or less.
正确答案：6 degrees or less　·　MAX　·　来源 smartcockpit.com

74.With VNAV engaged, the AFDS (Autopilot Flight Director System) pitch and AT modes are commanded by the:

  1. MCP
  2. FMC ✓
  3. FCC
正确答案：FMC　·　MAX　·　来源 smartcockpit.com

75.If windshear is encountered during FD takeoff or go-around, the FD pitch command bar provides commands to maintain V2+20 kts until vertical speed decreases to approximately:

  1. 600 fpm. ✓
  2. 800 fpm.
  3. 1000 fpm.
  4. 1200 fpm.
正确答案：600 fpm.　·　MAX　·　来源 smartcockpit.com

76.When one of the placard limit reversions (gear, flap or Vmo/Mmo) is reached, the overspeed limiting symbol appears in the MCP IAS Mach display.

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

77.When in ALT HOLD at FL80 you change the barometric setting from STD to QNH 1030 (3041 In.Hg). What will the aircraft do?

  1. The aircraft will climb 500 feet to the new pressure level
  2. The aircraft will descend 500 feet to the new pressure level
  3. You cannot change the altitude when in ALT HOLD
  4. The aircraft will continue at FL80, but the ALT readout will change. ✓
正确答案：The aircraft will continue at FL80, but the ALT readout will change.　·　MAX　·　来源 smartcockpit.com

78.A takeoff is commenced with both Flight Directors selected OFF. At 100 knots IAS a TOGA switch is pressed. What will happen to the F/D ?

  1. The F/D command bars automatically appear for both pilots. ✓
  2. The F/D engages in full go-around mode.
  3. The F/D command bars remain out of view.
正确答案：The F/D command bars automatically appear for both pilots.　·　MAX　·　来源 smartcockpit.com

79.When a conflict occurs between the VNAV profile and the MCP altitude, the airplane levels and the pitch flight mode annunciation becomes:rn

  1. VNAV SPD.
  2. VNAV PTH.
  3. VNAV.
  4. VNAV ALT. ✓
正确答案：VNAV ALT.　·　MAX　·　来源 smartcockpit.com

80.Bank angle is limited to 8 degrees below 400 feet, and _____ above 400 feet AGL.

  1. 30 degrees.
  2. 35 degrees.
  3. 40 degrees.
  4. 10u201330 degrees selectable. ✓
正确答案：10u201330 degrees selectable.　·　MAX　·　来源 smartcockpit.com

81.Maximum and minimum glideslope angles for autoland are 3.25 degrees and 2.5 degrees respectively.

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

82.Which of the following occurs when a TOGA switch is pressed below 2000 feet RA for a flight director go-around from a single autopilot ILS approach?

  1. The autopilot disengages.
  2. GA mode of the flight director engages.
  3. The autothrottle advances thrust levers to reduced go-around N1.
  4. All statements are correct. ✓
正确答案：All statements are correct.　·　MAX　·　来源 smartcockpit.com

83.During a dual channel go-around, the MCP IAS/Mach display will:

  1. Display the Vref speed used during the final approach.
  2. Become blank. ✓
  3. Display the flap manoeuvring speed.
正确答案：Become blank.　·　MAX　·　来源 smartcockpit.com

84.How many independent Flight Control Computers (FCCs) are there in the AFDS?

  1. One
  2. Two ✓
  3. Three
  4. Fours (two for each channel)
正确答案：Two　·　MAX　·　来源 smartcockpit.com

85.The underspeed symbol in the MCP Speed window is a:

  1. Steady 'A'.
  2. Steady '8'.
  3. Flashing 'A'. ✓
正确答案：Flashing 'A'.　·　MAX　·　来源 smartcockpit.com

86.The AUTOLAND warning light is armed during dual ILS AP approach below ____ feet.

  1. 2500 feet
  2. 800 feet
  3. 500 feet ✓
  4. 200 feet
正确答案：500 feet　·　MAX　·　来源 smartcockpit.com

87.The AUTOLAND warning light flashed RED if:rn

  1. AP disengages and ILS deviation occurs below 200 feet
  2. AP disengages, stab trim warning occurs and ILS deviation occurs below 200 feetrn ✓
  3. AP disengages, stab trim warning occurs and ILS deviation occurs below 500 feet
  4. AP disengages, stab trim or autothrottle warning occurs and ILS deviation occurs below 500 feet
正确答案：AP disengages, stab trim warning occurs and ILS deviation occurs below 200 feetrn　·　MAX　·　来源 smartcockpit.com

88.Trimming the stabilizer with the electrical trim switch on the control wheel does not disengages the autopilot.rnrnrn

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

89.One VHF NAV receiver must be tuned to an ILS frequency before the approach mode can be selected. For a dual AP approach, the second VHF NAV receiver must be tuned to the ILS frequency and the corresponding AP engaged in CMD prior to _____.

  1. 1200 ft RA.
  2. 800 feet RA. ✓
  3. APP capture.
  4. The second autopilot engagement.
正确答案：800 feet RA.　·　MAX　·　来源 smartcockpit.com

90.The conditions for engaging the flight director in go-around mode are:

  1. The F/D switches can be ON or OFF, inflight below 2,000 feet RA and not in takeoff mode, and the TO/GA switch pressed. ✓
  2. The F/D switches must be ON, inflight below 2,000 feet RA-and not in takeoff mode, and the TO/GA switch pressed.
  3. The F/D switches must be ON, inflight below 800 feet RA-and not in take-off mode, and the TO/GA switch pressed.
正确答案：The F/D switches can be ON or OFF, inflight below 2,000 feet RA and not in takeoff mode, and the TO/GA switch pressed.　·　MAX　·　来源 smartcockpit.com

91.During a single FD go-around, with a push of either TOGA switch:

  1. FD roll commands hold current heading.
  2. FD roll commands hold current ground track. ✓
  3. FD roll commands hold current heading until passing 400 ft.
  4. FD roll commands hold current heading until passing 250 ft RA.
正确答案：FD roll commands hold current ground track.　·　MAX　·　来源 smartcockpit.com

92.Antenna switching from tail antenna to nose antenna occurs when:rnrn

  1. VOR frequency is selected and VOR/LOC is armed or engaged.
  2. LOC frequency is selected only.
  3. LOC frequency is selected and VOR/LOC is armed or engaged. ✓
  4. VOR frequency is selected only.
正确答案：LOC frequency is selected and VOR/LOC is armed or engaged.　·　MAX　·　来源 smartcockpit.com

93.Two independent radio altimeters provide radio altitude to the respective FCCs. With a radio altimeter inoperative, the autopilot will disconnect ____ after LOC and GS capture.

  1. Immediately.
  2. 2 seconds. ✓
  3. Between 2 and 5 seconds depending on the altitude.rn
  4. 4 seconds.
正确答案：2 seconds.　·　MAX　·　来源 smartcockpit.com

94.Above _____, selection of another pitch mode or engaging an autopilot will terminate the takeoff mode.

  1. 200 ft RA.
  2. 400 feet RA. ✓
  3. 800 feet RA.
  4. 500 ft RA.
正确答案：400 feet RA.　·　MAX　·　来源 smartcockpit.com

95.When operating in 'ALT HOLD', the V/S mode is ARMED if the MCP altitude is changed by more than:

  1. 200 feet.
  2. 100 feet. ✓
  3. 500 feet.
正确答案：100 feet.　·　MAX　·　来源 smartcockpit.com

96.After localizer or glideslope capture, during a single channel autopilot approach, CWS can be engaged by manually overriding pitch and or roll control forces.

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

97.If an engine fails while the autothrottle is in N1 mode, the thrust lever of the failed engine:

  1. Advances a few degrees and returns to or below the other thrust lever position. ✓
  2. Remains stationary.
  3. Retracts a few degrees and returns to or above the other thrust lever position.
正确答案：Advances a few degrees and returns to or below the other thrust lever position.　·　MAX　·　来源 smartcockpit.com

98.LNAV mode terminates whenever:

  1. Either HDG SEL, VOR or LOC mode is armed.
  2. HDG SEL mode is engaged or upon VOR or LOC capture. ✓
  3. HDG SEL mode is engaged only.
正确答案：HDG SEL mode is engaged or upon VOR or LOC capture.　·　MAX　·　来源 smartcockpit.com

99.During Autopilot CWS operation above 1500 feet RA, if the roll control force is released with less than 6 degrees of bank, the autopilot will:

  1. Roll wings level and hold existing heading. ✓
  2. Remain at the same bank angle.
  3. Roll wings level only.
正确答案：Roll wings level and hold existing heading.　·　MAX　·　来源 smartcockpit.com

100.As you push the TOGA switch for an automatic go-around, what is the correct FMA in terms of Thrust mode - Roll mode - Pitch mode?

  1. N1 - VOR LOC - TOGA
  2. GA - LNAV - MCP SPD
  3. GA - TOGA ✓
  4. MCP SPD - GA
正确答案：GA - TOGA　·　MAX　·　来源 smartcockpit.com

101.Dual channel AP operation is possible ONLY when two generators are powering the busses. rn

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

102.You are established on the ILS at 3000 ft and inadvertently press TOGA once. What will happen?

  1. The AP will disengage but the aircraft will remain in approach logic
  2. The AP will stay connected but the FMS will change to GA logic
  3. Nothing will happen since the aircraft has not descended below 2000 ft RA.
  4. The AP will disconnect and AT will add thrust to reduced G/A, FD will pitch 15 degrees nose up ✓
正确答案：The AP will disconnect and AT will add thrust to reduced G/A, FD will pitch 15 degrees nose up　·　MAX　·　来源 smartcockpit.com

103.With an active route entered in FMC, LNAV engages within _____ with any airplane heading.rn

  1. 3 NM. ✓
  2. 2NM
  3. 1.5 NM
  4. 5 NM
正确答案：3 NM.　·　MAX　·　来源 smartcockpit.com

104.Each autopilot can be engaged by pushing a separate CMD or CWS engage switch. Autopilot engagement in CMD or CWS is inhibited unless the below conditions are met:

  1. No force is being applied to the control wheel and the STAB TRIM AUTOPILOT cutout switch is at NORMAL. ✓
  2. the STAB TRIM AUTOPILOT cutout switch is at NORMAL and one FD switch is ON.
  3. No force is being applied to the control wheel, at least one FD switch is ON, and the STAB TRIM AUTOPILOT cutout switch is at NORMAL.
  4. No force is being applied to the control wheel and at least one autopilot channel is operational.
正确答案：No force is being applied to the control wheel and the STAB TRIM AUTOPILOT cutout switch is at NORMAL.　·　MAX　·　来源 smartcockpit.com

105.The autopilot is engaged in ALT HOLD mode. The control column is then pushed, causing the autopilot to engage in CWS P mode. After the aircraft has descended 150 feet from the initial altitude the force applied to the control column is released and:

  1. CWS P mode changes to ALT ACQ mode and the A/P returns to the initial altitude and ALT HOLD engages. ✓
  2. CWS P remains engaged and the aircraft will maintain a constant pitch angle in the descent.
  3. CWS P mode changes to ALT ACQ mode and the A/P remains atthe an altitude of 150 feet lower than the initial altitude and ALT HOLD engages.
正确答案：CWS P mode changes to ALT ACQ mode and the A/P returns to the initial altitude and ALT HOLD engages.　·　MAX　·　来源 smartcockpit.com

106.A mode change highlight symbol (rectangle) is drawn around each pitch, roll, autopilot status, and thrust engaged mode annunciation for a period of _____ after each engagement.

  1. 10 seconds. ✓
  2. 5 seconds.
  3. 2 seconds.
  4. 3 seconds.
正确答案：10 seconds.　·　MAX　·　来源 smartcockpit.com

107.VNAV mode is terminated by any one of the following:

  1. Selecting another pitch mode, glideslope capture, reaching end of LNAV route, transition of glideslope intercept waypoint if GS is armed, crosstrack deviation exceeds twice the RNP
  2. Selecting another pitch mode, glideslope capture, reaching end of LNAV route, and transition of glideslope intercept waypoint if GS is armed
  3. Selecting another pitch mode, glideslope capture, transition of glideslope intercept waypoint if GS is armed, crosstrack deviation exceeds twice the RNP
  4. Selecting another pitch mode, glideslope capture, reaching end of LNAV route, transition of glideslope intercept waypoint if GS is armed, crosstrack deviation exceeds twice the RNP value during PTH descent for an active leg with a database vertical angle and LNAV not engaged. ✓
正确答案：Selecting another pitch mode, glideslope capture, reaching end of LNAV route, transition of glideslope intercept waypoint if GS is armed, crosstrack deviation exceeds twice the RNP value during PTH descent for an active leg with a database vertical angle and LNAV not engaged.　·　MAX　·　来源 smartcockpit.com

108.During a reduced thrust takeoff, a second press of the TOGA switch below 800 feet above field elevation will change the thrust limit mode to GA and N1 reference bugs to increase to full GA thrust, thrust levers will not be in motion.

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

109.VS mode automatically engages if ALT ACQ mode is engaged and a new MCP altitude is selected which is more than _____ different from previously selected altitude.

  1. 50 feet.
  2. 100 feet. ✓
  3. 80 feet.
  4. 20 feet.
正确答案：100 feet.　·　MAX　·　来源 smartcockpit.com

110.Which Autothrottle modes permit manual thrust change without Autothrottle interference?

  1. THR HLD and ARM ✓
  2. Only THR HLD
正确答案：THR HLD and ARM　·　MAX　·　来源 smartcockpit.com

111.Dual channel autopilot operation is possible only when two generators are powering the busses.

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

112.The FD can also be engaged in the takeoff mode with the FD switches off. If a TOGA switch is pushed after 80 knots below _____ and prior to 150 seconds after liftu2013off, the FD command bars automatically appear for both pilots.

  1. 1000 feet AGL.
  2. 2000 feet AGL. ✓
  3. 1500 feet AGL.
  4. 2500 feet AGL.
正确答案：2000 feet AGL.　·　MAX　·　来源 smartcockpit.com

113.After takeoff, the autopilot is engaged before flaps up. What is the correct mode (Thrust mode / Roll mode / Pitch mode) being displayed on the FMA? rnrn

  1. ARM - HDG SEL - TOGA
  2. N1 - LNAV - MCP SPD ✓
  3. ARM - LNAV - FMC SPD
  4. N1 - HDG SEL - VNAV
正确答案：N1 - LNAV - MCP SPD　·　MAX　·　来源 smartcockpit.com

114.The autopilot flare maneuver starts at approximately ____ feet RA and is completed at touchdown.rn

  1. 27 feet
  2. 35 feet
  3. 50 feet ✓
  4. 100 feet
正确答案：50 feet　·　MAX　·　来源 smartcockpit.com

115.if an engine failure occurs on the ground, the pitch command target speed at lift-off is _____, whichever is greater.

  1. V2 or airspeed at lift-off. ✓
  2. V2.
  3. V2+10.
  4. V2 + 20.
正确答案：V2 or airspeed at lift-off.　·　MAX　·　来源 smartcockpit.com

116.When performing an autopilot ILS approach, the glide slope can be technically captured from above or below:

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

117.During a dual channel autopilot approach, the Autopilot Disengage light illuminates steady red when below 800 feet. What does this indicate?

  1. The stabilizer is out of trim. ✓
  2. Both autopilots have reverted to CWS mode.
  3. A normal condition.
正确答案：The stabilizer is out of trim.　·　MAX　·　来源 smartcockpit.com

118.The aircraft is climbing with the autopilot in CMD and the pilot pushes the control column forward. The autopilot will:

  1. Revert to CWS P and the Roll axis remains in CMD. ✓
  2. Revert to CWS P and CWS R.
  3. Totally disengage.
正确答案：Revert to CWS P and the Roll axis remains in CMD.　·　MAX　·　来源 smartcockpit.com

119.What is the true statement about the Stabilizer Out Of Trim (STAB OUT OF TRIM) light?

  1. It is operational at all time.
  2. Operates only with autopilot engaged. Remains extinguished with autopilot not engaged. ✓
  3. Indicates that auto trim is degraded.
  4. When no autopilot is engaged, it means that auto trim is inoperative. With autopilot engaged, it means that autopilot is not trimming stabilizer properly.
正确答案：Operates only with autopilot engaged. Remains extinguished with autopilot not engaged.　·　MAX　·　来源 smartcockpit.com

120.If the MCP selected Altitude is changed during ALT ACQ mode:

  1. Then V/S mode is automatically activated. ✓
  2. The initial selected altitude is held.
  3. The pitch mode prior to ALT ACQ is automatically re-engaged.
正确答案：Then V/S mode is automatically activated.　·　MAX　·　来源 smartcockpit.com

121.The LOC capture point is variable and depends on intercept angle and rate of closure. Capture occurs no later than _____. Upon LOC capture, VOR LOC annunciates captured, SINGLE CH is annunciated for AP status, the previous roll mode disengages and the airplane turns to track the LOC.

  1. 1/2 dot ✓
  2. 1/3
  3. 1
  4. 1.5 dot
正确答案：1/2 dot　·　MAX　·　来源 smartcockpit.com

122.The Automatic Flight System (AFS) consists of:

  1. The autopilots.
  2. The Flight Directors.
  3. The Autothrottles.
  4. All statements are correct. ✓
正确答案：All statements are correct.　·　MAX　·　来源 smartcockpit.com

123.During a single engine FD go-around, the FD pitch commands ____ degrees nose up. As climb rate increases, FD pitch commands maintain a target speed.rn

  1. 8 degrees
  2. 10 degrees
  3. 13 degrees ✓
  4. 15 degrees
正确答案：13 degrees　·　MAX　·　来源 smartcockpit.com

124.When the pitch mode changes from VNAV SPD to ALT ACQ during an intermediate level off, the autothrottle will command a target IAS rather than Mach number.

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

125.After a normal takeoff which pitch command can you expect? rn

  1. V2
  2. V2 to V2+15kt rn
  3. V2 to V2+20kt
  4. V2+20kt ✓
正确答案：V2+20kt　·　MAX　·　来源 smartcockpit.com

126.Moving the autopilot Stabilizer Trim Cutout Switch to the CUTOUT position will disengage the autopilot.

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

127.The Control wheel force required to override the Autopilot COMMAND mode is:

  1. Less than normal CWS force
  2. Greater than normal CWS force ✓
  3. The same as normal CWS force.
正确答案：Greater than normal CWS force　·　MAX　·　来源 smartcockpit.com

128.In the 'ARM' autothrottle mode, the thrust lever autothrottle servos maintain thrust at the selected N1 limit displayed on the thrust mode display.rn

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

129.Localizer can be intercepted in HDG SEL, LNAV, or CWS R.

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

130.What pitch mode is annunciated after takeoff when the autopilot is first engaged in CMD?

  1. CWS P
  2. MCP SPD ✓
  3. VNAV
  4. VS
正确答案：MCP SPD　·　MAX　·　来源 smartcockpit.com

131.The AT Disengage flashing light (amber) indicates an airspeed error under the following conditions: inflight, flaps not up and airspeed differs from commanded value by _______ and is not approaching commanded value. rn

  1. + or - 10 knots
  2. + 10 knots or - 5 knots ✓
  3. + 5 knots or - 10 knots
  4. + 15 knots or -10 knots.
正确答案：+ 10 knots or - 5 knots　·　MAX　·　来源 smartcockpit.com

132.When flying on a geometrical path with VNAV engaged you push SPD INTV. What will happen? rn

  1. VNAV SPD will engage and MCP SPD will be annunciated in the FMA.
  2. VNAV PTH will remain engaged and MCP SPD will be annunciated in the FMA.
  3. VNAV PTH will remain engaged and FMC SPD will be annunciated in the FMA. ✓
  4. VNAV SPD will engage and FMC SPD will be annunciated in the FMA.
正确答案：VNAV PTH will remain engaged and FMC SPD will be annunciated in the FMA.　·　MAX　·　来源 smartcockpit.com

133.What is the minimum Mach number that can be selected in the IAS/MACH display of the MCP panel?

  1. 0.60 M ✓
  2. 0.65 M
  3. 0.70 M
正确答案：0.60 M　·　MAX　·　来源 smartcockpit.com

134.The Autothrottle is engaged in FMC speed mode. What is displayed in the IAS/MACH display of the MCP?

  1. Blank. ✓
  2. The aircraft's actual speed.
  3. The FMC speed.
正确答案：Blank.　·　MAX　·　来源 smartcockpit.com

135.Pushing a CWS engage switch engages the autopilot pitch and roll axes in the CWS mode and displays CWS P and CWS R on the FMAs. The autopilot maneuvers the airplane in response to control pressures applied by either pilot. The control pressure is similar to that required for manual flight. If aileron pressure is released with 6 degrees or less bank, the autopilot rolls the wings level and holds existing heading. The heading hold feature with bank less than 6 degrees is inhibited when:

  1. Below 1500 feet RA with the landing gear down or after FD VOR capture with TAS 250 knots or less or after FD LOC capture in the APP mode. ✓
  2. Below 2500 feet RA with the landing gear down or after FD VOR capture with TAS 200 knots or less or after FD LOC capture in the APP mode.
  3. Below 1500 feet RA with the landing gear down or after FD VOR capture with TAS 200 knots or less or after FD LOC capture in the APP mode.
  4. Below 2500 feet RA with the landing gear down or after FD VOR capture with TAS 250 knots or less or after FD LOC capture in the APP mode.
正确答案：Below 1500 feet RA with the landing gear down or after FD VOR capture with TAS 250 knots or less or after FD LOC capture in the APP mode.　·　MAX　·　来源 smartcockpit.com

136.What happens with the IAS/MACH display on the MCP if SPD INTV is pushed during VNAV operations?rn

  1. IAS/MACH displays opens up and shows 250 kts.
  2. IAS/MACH displays opens up and shows FMC target speed ✓
  3. IAS/MACH displays opens up and shows slashes.
  4. IAS/MACH displays opens up and shows dashes.
正确答案：IAS/MACH displays opens up and shows FMC target speed　·　MAX　·　来源 smartcockpit.com

137.Normally, N1 limits and target N1 values are provided to the autothrottle by the:

  1. Autothrottle computer.
  2. FMC. ✓
  3. IRUs.
正确答案：FMC.　·　MAX　·　来源 smartcockpit.com

138.During takeoff with FD ON, the AFDS commands pitch attitude ____ degrees after ____ IAS.rn

  1. 10 degrees nose up and 60 kt IAS.
  2. 15 degrees nose up and 60 kt IAS. ✓
  3. 0 degrees nose up and 84 kt IAS.
  4. 15 degrees nose up and 84 kt IAS.
正确答案：15 degrees nose up and 60 kt IAS.　·　MAX　·　来源 smartcockpit.com

139.If the autopilot ALT HOLD mode is manually overriden with control column pressure, which of the following will occur?

  1. The autopilot disengages.
  2. LNAV disengages.
  3. The autopilot changes to CWS P and returns to ALT HLD if control pressure released within 250 ft of selected altitude. ✓
  4. LEVEL CHANGE automatically engages.
正确答案：The autopilot changes to CWS P and returns to ALT HLD if control pressure released within 250 ft of selected altitude.　·　MAX　·　来源 smartcockpit.com

140.If thrust levers become separated more than 10 degrees during a dual channel approach (before FLARE armed is annunciated), the autothrottle is then disengaged.

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

141.LNAV mode terminates whenever:

  1. Either HDG SEL, VOR or LOC mode is armed.
  2. HDG SEL mode is engaged or upon VOR or LOC capture. ✓
  3. HDG SEL mode is engaged only.
正确答案：HDG SEL mode is engaged or upon VOR or LOC capture.　·　NG　·　来源 smartcockpit.com

142.After takeoff, the autopilot is engaged before flaps up. What is the correct mode (Thrust mode / Roll mode / Pitch mode) being displayed on the FMA?

  1. ARM - HDG SEL - TOGA
  2. N1 - LNAV - MCP SPD ✓
  3. ARM - LNAV - FMC SPD
  4. N1 - HDG SEL - VNAV
正确答案：N1 - LNAV - MCP SPD　·　NG　·　来源 smartcockpit.com

143.When flying on a geometrical path with VNAV engaged you push SPD INTV. What will happen?

  1. VNAV SPD will engage and MCP SPD will be annunciated in the FMA.
  2. VNAV PTH will remain engaged and MCP SPD will be annunciated in the FMA.
  3. VNAV PTH will remain engaged and FMC SPD will be annunciated in the FMA. ✓
  4. VNAV SPD will engage and FMC SPD will be annunciated in the FMA.
正确答案：VNAV PTH will remain engaged and FMC SPD will be annunciated in the FMA.　·　NG　·　来源 smartcockpit.com

144.As you push the TOGA switch for an automatic go-around, what is the correct FMA in terms of Thrust mode - Roll mode - Pitch mode?

  1. N1 - VOR LOC - TOGA
  2. GA - LNAV - MCP SPD
  3. GA - TOGA ✓
  4. MCP SPD - GA
正确答案：GA - TOGA　·　NG　·　来源 smartcockpit.com

145.The Autothrottle is engaged in FMC speed mode. What is displayed in the IAS/MACH display of the MCP?

  1. Blank. ✓
  2. The aircraft's actual speed.
  3. The FMC speed.
正确答案：Blank.　·　NG　·　来源 smartcockpit.com

146.Two independent radio altimeters provide radio altitude to the respective FCCs. With a radio altimeter inoperative, the autopilot will disconnect ____ after LOC and GS capture.

  1. Immediately.
  2. 2 seconds. ✓
  3. Between 2 and 5 seconds depending on the altitude.
  4. 4 seconds.
正确答案：2 seconds.　·　NG　·　来源 smartcockpit.com

147.The Control wheel force required to override the Autopilot COMMAND mode is:

  1. Less than normal CWS force
  2. Greater than normal CWS force ✓
  3. The same as normal CWS force.
正确答案：Greater than normal CWS force　·　NG　·　来源 smartcockpit.com

148.During a reduced thrust takeoff, a second press of the TOGA switch below 800 feet above field elevation will change the thrust limit mode to GA and N1 reference bugs to increase to full GA thrust, thrust levers will not be in motion.

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

149.If the autopilot is engaged and either pilot's control wheel Trim Switch is activated:

  1. The stabiliser will move at a slow rate with the autopilot remains engaged.
  2. The autopilot will disengage. ✓
  3. The stabiliser will not move and the autopilot remains engaged.
正确答案：The autopilot will disengage.　·　NG　·　来源 smartcockpit.com

150.When the pitch mode changes from VNAV SPD to ALT ACQ during an intermediate level off, the autothrottle will command a target IAS rather than Mach number.

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

151.During Autopilot CWS operation above 1500 feet RA, if the roll control force is released with less than 6 degrees of bank, the autopilot will:

  1. Roll wings level and hold existing heading. ✓
  2. Remain at the same bank angle.
  3. Roll wings level only.
正确答案：Roll wings level and hold existing heading.　·　NG　·　来源 smartcockpit.com

152.What is the true statement about the Stabilizer Out Of Trim (STAB OUT OF TRIM) light?

  1. It is operational at all time.
  2. Operates only with autopilot engaged. Remains extinguished with autopilot not engaged. ✓
  3. Indicates that auto trim is degraded.
  4. When no autopilot is engaged, it means that auto trim is inoperative. With autopilot engaged, it means that autopilot is not trimming stabilizer properly.
正确答案：Operates only with autopilot engaged. Remains extinguished with autopilot not engaged.　·　NG　·　来源 smartcockpit.com

153.If thrust levers become separated more than 10 degrees during a dual channel approach (before FLARE armed is annunciated), the autothrottle is then disengaged.

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

154.Trimming the stabilizer with the electrical trim switch on the control wheel does not disengages the autopilot.

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

155.Bank angle is limited to 8 degrees below 400 feet, and _____ above 400 feet AGL.

  1. 30 degrees.
  2. 35 degrees.
  3. 40 degrees.
  4. 10-30 degrees selectable. ✓
正确答案：10-30 degrees selectable.　·　NG　·　来源 smartcockpit.com

156.The AT Disengage flashing light (amber) indicates an airspeed error under the following conditions: inflight, flaps not up and airspeed differs from commanded value by _______ and is not approaching commanded value.

  1. + or - 10 knots
  2. + 10 knots or - 5 knots ✓
  3. + 5 knots or - 10 knots
  4. + 15 knots or -10 knots.
正确答案：+ 10 knots or - 5 knots　·　NG　·　来源 smartcockpit.com

157.When operating in 'ALT HOLD', the V/S mode is ARMED if the MCP altitude is changed by more than:

  1. 200 feet.
  2. 100 feet. ✓
  3. 500 feet.
正确答案：100 feet.　·　NG　·　来源 smartcockpit.com

158.If engaged the autothrottle will disengage ____ after landing touchdown.

  1. 2 seconds ✓
  2. 5 seconds
  3. 7 seconds
  4. 6 seconds
正确答案：2 seconds　·　NG　·　来源 smartcockpit.com

159.If an engine fails while the autothrottle is in N1 mode, the thrust lever of the failed engine:

  1. Advances a few degrees and returns to or below the other thrust lever position. ✓
  2. Remains stationary.
  3. Retracts a few degrees and returns to or above the other thrust lever position.
正确答案：Advances a few degrees and returns to or below the other thrust lever position.　·　NG　·　来源 smartcockpit.com

160.During a single FD go-around, with a push of either TOGA switch:

  1. FD roll commands hold current heading.
  2. FD roll commands hold current ground track. ✓
  3. FD roll commands hold current heading until passing 400 ft.
  4. FD roll commands hold current heading until passing 250 ft RA.
正确答案：FD roll commands hold current ground track.　·　NG　·　来源 smartcockpit.com

161.For dual autopilot operation, both VHF NAV receivers must be tuned to the ILS frequency and both autopilots must be selected in CMD prior to _____

  1. 800 feet RA. ✓
  2. 1 200 ft RA.
  3. 1 000 ft RA.
  4. 950 ft RA.
正确答案：800 feet RA.　·　NG　·　来源 smartcockpit.com

162.VS mode automatically engages if ALT ACQ mode is engaged and a new MCP altitude is selected which is more than _____ different from previously selected altitude.

  1. 50 feet.
  2. 100 feet. ✓
  3. 80 feet.
  4. 20 feet.
正确答案：100 feet.　·　NG　·　来源 smartcockpit.com

163.The conditions for engaging the flight director in go-around mode are:

  1. The F/D switches can be ON or OFF, inflight below 2,000 feet RA and not in takeoff mode, and the TO/GA switch pressed. ✓
  2. The F/D switches must be ON, inflight below 2,000 feet RA-and not in takeoff mode, and the TO/GA switch pressed.
  3. The F/D switches must be ON, inflight below 800 feet RA-and not in take-off mode, and the TO/GA switch pressed.
正确答案：The F/D switches can be ON or OFF, inflight below 2,000 feet RA and not in takeoff mode, and the TO/GA switch pressed.　·　NG　·　来源 smartcockpit.com

164.The Flight Director Comparator monitors:

  1. The symbol generators.
  2. The IRS headings.
  3. The command bar positions. ✓
正确答案：The command bar positions.　·　NG　·　来源 smartcockpit.com

165.When a conflict occurs between the VNAV profile and the MCP altitude, the airplane levels and the pitch flight mode annunciation becomes:

  1. VNAV SPD.
  2. VNAV PTH.
  3. VNAV.
  4. VNAV ALT. ✓
正确答案：VNAV ALT.　·　NG　·　来源 smartcockpit.com

166.The LOC capture point is variable and depends on intercept angle and rate of closure. Capture occurs no later than _____. Upon LOC capture, VOR LOC annunciates captured, SINGLE CH is annunciated for AP status, the previous roll mode disengages and the airplane turns to track the LOC.

  1. 1/2 dot ✓
  2. 1/3
  3. 1
  4. 1.5 dot
正确答案：1/2 dot　·　NG　·　来源 smartcockpit.com

167.Each autopilot can be engaged by pushing a separate CMD or CWS engage switch. Autopilot engagement in CMD or CWS is inhibited unless the below conditions are met:

  1. No force is being applied to the control wheel and the STAB TRIM AUTOPILOT cutout switch is at NORMAL. ✓
  2. the STAB TRIM AUTOPILOT cutout switch is at NORMAL and one FD switch is ON.
  3. No force is being applied to the control wheel, at least one FD switch is ON, and the STAB TRIM AUTOPILOT cutout switch is at NORMAL.
  4. No force is being applied to the control wheel and at least one autopilot channel is operational.
正确答案：No force is being applied to the control wheel and the STAB TRIM AUTOPILOT cutout switch is at NORMAL.　·　NG　·　来源 smartcockpit.com

168.During a single engine FD go-around, the FD pitch commands ____ degrees nose up. As climb rate increases, FD pitch commands maintain a target speed.

  1. 8 degrees
  2. 10 degrees
  3. 13 degrees ✓
  4. 15 degrees
正确答案：13 degrees　·　NG　·　来源 smartcockpit.com

169.The AUTOLAND warning light flashed RED if:

  1. AP disengages and ILS deviation occurs below 200 feet
  2. AP disengages, stab trim warning occurs and ILS deviation occurs below 200 feet ✓
  3. AP disengages, stab trim warning occurs and ILS deviation occurs below 500 feet
  4. AP disengages, stab trim or autothrottle warning occurs and ILS deviation occurs below 500 feet
正确答案：AP disengages, stab trim warning occurs and ILS deviation occurs below 200 feet　·　NG　·　来源 smartcockpit.com

170.Automatic Flight Approach and Landing - If FLARE is not armed by approximately _____, both autopilots automatically disengage.

  1. 250 ft RA.
  2. 350 feet RA. ✓
  3. 400 ft RA.
  4. 500 ft RA.
正确答案：350 feet RA.　·　NG　·　来源 smartcockpit.com

171.With an active route entered in FMC, LNAV engages within _____ with any airplane heading.

  1. 3 NM. ✓
  2. 2NM
  3. 1.5 NM
  4. 5 NM
正确答案：3 NM.　·　NG　·　来源 smartcockpit.com

172.The aircraft is climbing with the autopilot in CMD and the pilot pushes the control column forward. The autopilot will:

  1. Revert to CWS P and the Roll axis remains in CMD. ✓
  2. Revert to CWS P and CWS R.
  3. Totally disengage.
正确答案：Revert to CWS P and the Roll axis remains in CMD.　·　NG　·　来源 smartcockpit.com

173.Localizer can be intercepted in HDG SEL, LNAV, or CWS R.

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

174.During a dual channel autopilot approach, the Autopilot Disengage light illuminates steady red when below 800 feet. What does this indicate?

  1. The stabilizer is out of trim. ✓
  2. Both autopilots have reverted to CWS mode.
  3. A normal condition.
正确答案：The stabilizer is out of trim.　·　NG　·　来源 smartcockpit.com

175.A takeoff is commenced with both Flight Directors selected OFF. At 100 knots IAS a TOGA switch is pressed. What will happen to the F/D ?

  1. The F/D command bars automatically appear for both pilots. ✓
  2. The F/D engages in full go-around mode.
  3. The F/D command bars remain out of view.
正确答案：The F/D command bars automatically appear for both pilots.　·　NG　·　来源 smartcockpit.com

176.If the autopilot ALT HOLD mode is manually overriden with control column pressure, which of the following will occur?

  1. The autopilot disengages.
  2. LNAV disengages.
  3. The autopilot changes to CWS P and returns to ALT HLD if control pressure released within 250 ft of selected altitude. ✓
  4. LEVEL CHANGE automatically engages.
正确答案：The autopilot changes to CWS P and returns to ALT HLD if control pressure released within 250 ft of selected altitude.　·　NG　·　来源 smartcockpit.com

177.You are established on the ILS at 3000 ft and inadvertently press TOGA once. What will happen?

  1. The AP will disengage but the aircraft will remain in approach logic
  2. The AP will stay connected but the FMS will change to GA logic
  3. Nothing will happen since the aircraft has not descended below 2000 ft RA.
  4. The AP will disconnect and AT will add thrust to reduced G/A, FD will pitch 15 degrees nose up ✓
正确答案：The AP will disconnect and AT will add thrust to reduced G/A, FD will pitch 15 degrees nose up　·　NG　·　来源 smartcockpit.com

178.Minimum speed reversion is also available when the Autothrottle is OFF and the AFDS is in ALT HOLD or after GS capture.

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

179.With VNAV engaged, the AFDS (Autopilot Flight Director System) pitch and AT modes are commanded by the:

  1. MCP
  2. FMC ✓
  3. FCC
正确答案：FMC　·　NG　·　来源 smartcockpit.com

180.When performing an autopilot ILS approach, the glide slope can be technically captured from above or below:

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

181.Pushing a CWS engage switch engages the autopilot pitch and roll axes in the CWS mode and displays CWS P and CWS R on the FMAs. The autopilot maneuvers the airplane in response to control pressures applied by either pilot. The control pressure is similar to that required for manual flight. If aileron pressure is released with 6 degrees or less bank, the autopilot rolls the wings level and holds existing heading. The heading hold feature with bank less than 6 degrees is inhibited when:

  1. Below 1500 feet RA with the landing gear down or after FD VOR capture with TAS 250 knots or less or after FD LOC capture in the APP mode. ✓
  2. Below 2500 feet RA with the landing gear down or after FD VOR capture with TAS 200 knots or less or after FD LOC capture in the APP mode.
  3. Below 1500 feet RA with the landing gear down or after FD VOR capture with TAS 200 knots or less or after FD LOC capture in the APP mode.
  4. Below 2500 feet RA with the landing gear down or after FD VOR capture with TAS 250 knots or less or after FD LOC capture in the APP mode.
正确答案：Below 1500 feet RA with the landing gear down or after FD VOR capture with TAS 250 knots or less or after FD LOC capture in the APP mode.　·　NG　·　来源 smartcockpit.com

182.When control wheel pressure is released during CWS roll operation, the airplane will roll wings level when the bank angle is:

  1. 5 degrees or less
  2. 6 degrees or less ✓
  3. 10 degrees or less
  4. 15 degrees or less.
正确答案：6 degrees or less　·　NG　·　来源 smartcockpit.com

183.LNAV arming criteria on the ground:

  1. Origin runway in flight plan, active route entered in FMC, track of first leg within 5 degrees of runway heading, LNAV selected prior to TOGA. ✓
  2. Origin runway in flight plan, active route entered in FMC, LNAV selected prior to TOGA.
  3. Origin runway in flight plan, active route entered in FMC, itrack of first leg within 7 degrees of runway track, LNAV selected prior to TOGA.
  4. Origin runway in flight plan, active route entered in FMC, track of first leg within 8 degrees of runway heading, LNAV selected prior to TOGA.
正确答案：Origin runway in flight plan, active route entered in FMC, track of first leg within 5 degrees of runway heading, LNAV selected prior to TOGA.　·　NG　·　来源 smartcockpit.com

184.Normally, N1 limits and target N1 values are provided to the autothrottle by the:

  1. Autothrottle computer.
  2. FMC. ✓
  3. IRUs.
正确答案：FMC.　·　NG　·　来源 smartcockpit.com

185.What is the minimum Mach number that can be selected in the IAS/MACH display of the MCP panel?

  1. 0.60 M ✓
  2. 0.65 M
  3. 0.70 M
正确答案：0.60 M　·　NG　·　来源 smartcockpit.com

186.Above _____, selection of another pitch mode or engaging an autopilot will terminate the takeoff mode.

  1. 200 ft RA.
  2. 400 feet RA. ✓
  3. 800 feet RA.
  4. 500 ft RA.
正确答案：400 feet RA.　·　NG　·　来源 smartcockpit.com

187.In the 'ARM' autothrottle mode, the thrust lever autothrottle servos maintain thrust at the selected N1 limit displayed on the thrust mode display.

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

188.What happens with the IAS/MACH display on the MCP if SPD INTV is pushed during VNAV operations?

  1. IAS/MACH displays opens up and shows 250 kts.
  2. IAS/MACH displays opens up and shows FMC target speed ✓
  3. IAS/MACH displays opens up and shows slashes.
  4. IAS/MACH displays opens up and shows dashes.
正确答案：IAS/MACH displays opens up and shows FMC target speed　·　NG　·　来源 smartcockpit.com

189.After localizer or glideslope capture, during a single channel autopilot approach, CWS can be engaged by manually overriding pitch and or roll control forces.

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

190.Antenna switching from tail antenna to nose antenna occurs when:

  1. VOR frequency is selected and VOR/LOC is armed or engaged.
  2. LOC frequency is selected only.
  3. LOC frequency is selected and VOR/LOC is armed or engaged. ✓
  4. VOR frequency is selected only.
正确答案：LOC frequency is selected and VOR/LOC is armed or engaged.　·　NG　·　来源 smartcockpit.com

191.Moving the autopilot Stabilizer Trim Cutout Switch to the CUTOUT position will disengage the autopilot.

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

192.After a normal takeoff which pitch command can you expect?

  1. V2
  2. V2 to V2+15kt
  3. V2 to V2+20kt
  4. V2+20kt ✓
正确答案：V2+20kt　·　NG　·　来源 smartcockpit.com

193.When one of the placard limit reversions (gear, flap or Vmo/Mmo) is reached, the overspeed limiting symbol appears in the MCP IAS Mach display.

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

194.The Automatic Flight System (AFS) consists of:

  1. The autopilots.
  2. The Flight Directors.
  3. The Autothrottles.
  4. All statements are correct. ✓
正确答案：All statements are correct.　·　NG　·　来源 smartcockpit.com

195.How many independent Flight Control Computers (FCCs) are there in the AFDS?

  1. One
  2. Two ✓
  3. Three
  4. Fours (two for each channel)
正确答案：Two　·　NG　·　来源 smartcockpit.com

196.The autopilot flare maneuver starts at approximately ____ feet RA and is completed at touchdown.

  1. 27 feet
  2. 35 feet
  3. 50 feet ✓
  4. 100 feet
正确答案：50 feet　·　NG　·　来源 smartcockpit.com

197.The following annunciation provide the flight crew with autoland system mode and status:

  1. LAND 3 means two autopilots, two inertial sources at least and the associated sensors are operating normally for an automatic landing
  2. LAND 3 means two autopilots, three inertial sources at least and the associated sensors are operating normally for an automatic landing
  3. LAND 3 means two autopilots, three inertial sources and the associated sensors are operating normally for an automatic landing and rollout. ✓
  4. LAND 3 means two autopilots, three inertial sources, the associated sensors are operating normally for an automatic landing and rollout and at least one FMS is operative.
正确答案：LAND 3 means two autopilots, three inertial sources and the associated sensors are operating normally for an automatic landing and rollout.　·　NG　·　来源 smartcockpit.com

198.With the AT Arm switch at ARM, the AT go-around mode is armed:

  1. When descending below 2000 feet RA, when above 2000 feet RA with flaps not up or G/S captured, with or without the AFDS engaged. ✓
  2. When descending below 2500 feet RA, when above 2000 feet RA with flaps not up or G/S captured, with the AFDS engaged.
  3. When descending below 2000 feet RA, with G/S captured, with or without the AFDS engaged.
  4. When descending below 2000 feet RA, when above 2000 feet RA with flaps not up or G/S captured, with the AFDS engaged.
正确答案：When descending below 2000 feet RA, when above 2000 feet RA with flaps not up or G/S captured, with or without the AFDS engaged.　·　NG　·　来源 smartcockpit.com

199.Maximum and minimum glideslope angles for autoland are 3.25 degrees and 2.5 degrees respectively.

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

200.If the MCP selected Altitude is changed during ALT ACQ mode:

  1. Then V/S mode is automatically activated. ✓
  2. The initial selected altitude is held.
  3. The pitch mode prior to ALT ACQ is automatically re-engaged.
正确答案：Then V/S mode is automatically activated.　·　NG　·　来源 smartcockpit.com

201.During takeoff with FD ON, the AFDS commands pitch attitude ____ degrees after ____ IAS.

  1. 10 degrees nose up and 60 kt IAS.
  2. 15 degrees nose up and 60 kt IAS. ✓
  3. 0 degrees nose up and 84 kt IAS.
  4. 15 degrees nose up and 84 kt IAS.
正确答案：15 degrees nose up and 60 kt IAS.　·　NG　·　来源 smartcockpit.com

202.One VHF NAV receiver must be tuned to an ILS frequency before the approach mode can be selected. For a dual AP approach, the second VHF NAV receiver must be tuned to the ILS frequency and the corresponding AP engaged in CMD prior to _____.

  1. 1200 ft RA.
  2. 800 feet RA. ✓
  3. APP capture.
  4. The second autopilot engagement.
正确答案：800 feet RA.　·　NG　·　来源 smartcockpit.com

203.The underspeed symbol in the MCP Speed window is a:

  1. Steady 'A'.
  2. Steady '8'.
  3. Flashing 'A'. ✓
正确答案：Flashing 'A'.　·　NG　·　来源 smartcockpit.com

204.During a dual channel go-around, the MCP IAS/Mach display will:

  1. Display the Vref speed used during the final approach.
  2. Become blank. ✓
  3. Display the flap manoeuvring speed.
正确答案：Become blank.　·　NG　·　来源 smartcockpit.com

205.The FD can also be engaged in the takeoff mode with the FD switches off. If a TOGA switch is pushed after 80 knots below _____ and prior to 150 seconds after lift-off, the FD command bars automatically appear for both pilots.

  1. 1000 feet AGL.
  2. 2000 feet AGL. ✓
  3. 1500 feet AGL.
  4. 2500 feet AGL.
正确答案：2000 feet AGL.　·　NG　·　来源 smartcockpit.com

206.When in ALT HOLD at FL80 you change the barometric setting from STD to QNH 1030 (3041 In.Hg). What will the aircraft do?

  1. The aircraft will climb 500 feet to the new pressure level
  2. The aircraft will descend 500 feet to the new pressure level
  3. You cannot change the altitude when in ALT HOLD
  4. The aircraft will continue at FL80, but the ALT readout will change. ✓
正确答案：The aircraft will continue at FL80, but the ALT readout will change.　·　NG　·　来源 smartcockpit.com

207.Which Autothrottle modes permit manual thrust change without Autothrottle interference?

  1. THR HLD and ARM ✓
  2. Only THR HLD
正确答案：THR HLD and ARM　·　NG　·　来源 smartcockpit.com

208.Dual channel AP operation is possible ONLY when two generators are powering the busses.

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

209.Dual channel autopilot operation is possible only when two generators are powering the busses.

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

210.Which of the following occurs when a TOGA switch is pressed below 2000 feet RA for a flight director go-around from a single autopilot ILS approach?

  1. The autopilot disengages.
  2. GA mode of the flight director engages.
  3. The autothrottle advances thrust levers to reduced go-around N1.
  4. All statements are correct. ✓
正确答案：All statements are correct.　·　NG　·　来源 smartcockpit.com

211.VNAV mode is terminated by any one of the following:

  1. Selecting another pitch mode, glideslope capture, reaching end of LNAV route, transition of glideslope intercept waypoint if GS is armed, crosstrack deviation exceeds twice the RNP
  2. Selecting another pitch mode, glideslope capture, reaching end of LNAV route, and transition of glideslope intercept waypoint if GS is armed
  3. Selecting another pitch mode, glideslope capture, transition of glideslope intercept waypoint if GS is armed, crosstrack deviation exceeds twice the RNP
  4. Selecting another pitch mode, glideslope capture, reaching end of LNAV route, transition of glideslope intercept waypoint if GS is armed, crosstrack deviation exceeds twice the RNP value during PTH descent for an active leg with a database vertical angle and LNAV not engaged. ✓
正确答案：Selecting another pitch mode, glideslope capture, reaching end of LNAV route, transition of glideslope intercept waypoint if GS is armed, crosstrack deviation exceeds twice the RNP value during PTH descent for an active leg with a database vertical angle and LNAV not engaged.　·　NG　·　来源 smartcockpit.com

212.The AUTOLAND warning light is armed during dual ILS AP approach below ____ feet.

  1. 2500 feet
  2. 800 feet
  3. 500 feet ✓
  4. 200 feet
正确答案：500 feet　·　NG　·　来源 smartcockpit.com

213.What pitch mode is annunciated after takeoff when the autopilot is first engaged in CMD?

  1. CWS P
  2. MCP SPD ✓
  3. VNAV
  4. VS
正确答案：MCP SPD　·　NG　·　来源 smartcockpit.com

214.The white AT LIM symbol appears on the upper display unit. What is the correct statement?

  1. The autothrottle has reached the thrust limit for the selected assumed temperature.
  2. The N1 has been manually set and not by the FMC, therefore the AT LIM will be illuminated.
  3. The AT is using the upgraded BLT performance information.
  4. The FMC is not providing autothrottle with N1 limit values. ✓
正确答案：The FMC is not providing autothrottle with N1 limit values.　·　NG　·　来源 smartcockpit.com

215.A mode change highlight symbol (rectangle) is drawn around each pitch, roll, autopilot status, and thrust engaged mode annunciation for a period of _____ after each engagement.

  1. 10 seconds. ✓
  2. 5 seconds.
  3. 2 seconds.
  4. 3 seconds.
正确答案：10 seconds.　·　NG　·　来源 smartcockpit.com

216.The autopilot is engaged in ALT HOLD mode. The control column is then pushed, causing the autopilot to engage in CWS P mode. After the aircraft has descended 150 feet from the initial altitude the force applied to the control column is released and:

  1. CWS P mode changes to ALT ACQ mode and the A/P returns to the initial altitude and ALT HOLD engages. ✓
  2. CWS P remains engaged and the aircraft will maintain a constant pitch angle in the descent.
  3. CWS P mode changes to ALT ACQ mode and the A/P remains atthe an altitude of 150 feet lower than the initial altitude and ALT HOLD engages.
正确答案：CWS P mode changes to ALT ACQ mode and the A/P returns to the initial altitude and ALT HOLD engages.　·　NG　·　来源 smartcockpit.com

217.If windshear is encountered during FD takeoff or go-around, the FD pitch command bar provides commands to maintain V2+20 kts until vertical speed decreases to approximately:

  1. 600 fpm. ✓
  2. 800 fpm.
  3. 1000 fpm.
  4. 1200 fpm.
正确答案：600 fpm.　·　NG　·　来源 smartcockpit.com

218.if an engine failure occurs on the ground, the pitch command target speed at lift-off is _____, whichever is greater.

  1. V2 or airspeed at lift-off. ✓
  2. V2.
  3. V2+10.
  4. V2 + 20.
正确答案：V2 or airspeed at lift-off.　·　NG　·　来源 smartcockpit.com

219.In flight below 2000 feet RA, on an ILS Autopilot approach with flare armed, what happens if you push a TO/GA switch once?

  1. Autothrottle advances thrust levers to reduced Go-Around N1. ✓
  2. Autothrottle will disengage, and ARM is dispalyed in FMA.
  3. Autothrottle advances thrust levers to full Go-Around N1.
  4. Autopilot will disengage, and CWS P will annunciate.
正确答案：Autothrottle advances thrust levers to reduced Go-Around N1.　·　NG　·　来源 Chair Flight B737 Question Bank

220.After takeoff the autothrottle will remain in Throttle Hold (THR HLD) until 800 feet RA.

  1. True ✓
  2. False
正确答案：True　·　NG　·　来源 Chair Flight B737 Question Bank

221.What normally provides the N1 limits and target N1 values to the Autothrottle?

  1. The Electronic Engine Controls (EECs).
  2. The Flight Management Computer. ✓
  3. The Autothrottle Computer.
  4. The Flight Control Computers.
正确答案：The Flight Management Computer.　·　NG　·　来源 Chair Flight B737 Question Bank

222.In flight, with Autopilot engaged in CMD B, which FCC controls the logic for the flight directors on the Captain's PFD.

  1. FMS A
  2. FMS B
  3. FCC A
  4. FCC B ✓
正确答案：FCC B　·　NG　·　来源 Chair Flight B737 Question Bank

223.The VOR/LOC mode must be armed before the second Autopilot can be selected during a dual channel autopilot approach.

  1. True
  2. False ✓
正确答案：False　·　NG　·　来源 Chair Flight B737 Question Bank

224.For approach, by what altitude must the second Autopilot be selected for dual Autopilot operation?

  1. 1500 feet RA
  2. 500 feet RA
  3. 350 feet RA
  4. 800 feet RA ✓
正确答案：800 feet RA　·　NG　·　来源 Chair Flight B737 Question Bank

225.Below which RA should FLARE mode be armed during AUTOLAND?

  1. 350 feet RA.
  2. 1500 RA ✓
  3. 50 feet RA.
  4. 350 feet AGL.
正确答案：1500 RA　·　NG　·　来源 Chair Flight B737 Question Bank

226.At what altitude will the FLARE manoeuvre start during AUTOLAND?

  1. 50 feet AGL.
  2. 50 RA. ✓
  3. 350 feet RA.
  4. 500 feet AGL.
正确答案：50 RA.　·　NG　·　来源 Chair Flight B737 Question Bank

227.The Autothrottle (A/T) system, provides automatic thrust control from the start of takeoff, through all stages of flight to up to and including landing.

  1. True ✓
  2. False
正确答案：True　·　NG　·　来源 Chair Flight B737 Question Bank
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