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Boeing 737 · Flight Instruments 题库（133 题）

Boeing 737 机型「Flight Instruments」相关知识共 133 道题。想练习或模拟考试，请到 题库 · 模拟考试。
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1.737CL: The Airspeed Cursor Control on the Captains Mach/Airspeed Indicator must be pushed in to allow

  1. The airspeed cursor to be manually positioned.
  2. The airspeed cursor to be automatically positioned by the AFDS FCC. ✓
  3. The Vmo pointer to be automatically positioned by the AFDS FCC.
正确答案：The airspeed cursor to be automatically positioned by the AFDS FCC.　·　737　·　来源 b737.org.uk

2.The Vmo flag on the Mach/Airspeed indicators

  1. Indicates the Vmo pointer is inoperative. ✓
  2. Indicates the Vmo speed is being exceeded.
  3. Indicates the Vmo pointer is operative.
正确答案：Indicates the Vmo pointer is inoperative.　·　737　·　来源 b737.org.uk

3.The standby airspeed indicator utilises the

  1. The No.1 Aux pitot and the normal static systems.
  2. The No.2 Aux pitot and the alternate static systems. ✓
  3. The No.1 ADC and the alternate static systems.
正确答案：The No.2 Aux pitot and the alternate static systems.　·　737　·　来源 b737.org.uk

4.The Vertical Speed Indicators are fed from their respective

  1. Inertial Reference Units. ✓
  2. Air Data Computers
  3. Static Vents.
正确答案：Inertial Reference Units.　·　737　·　来源 b737.org.uk

5.The ILS signal to the Standby Horizon Indicator is fed from the

  1. FMC
  2. No. 2 ILS receiver.
  3. No. 1 ILS receiver. ✓
正确答案：No. 1 ILS receiver.　·　737　·　来源 b737.org.uk

6.The Flight Recorder will operate on the ground

  1. When either engine is operating only.
  2. When the Test switch is selected to TEST or either engine is operating. ✓
  3. At all times.
正确答案：When the Test switch is selected to TEST or either engine is operating.　·　737　·　来源 b737.org.uk

7.The alternate static system provides static pressure inputs to

  1. The Standby Airspeed indicator / Standby Altimeter and No.2 ADC.
  2. The Standby Airspeed indicator / Standby Altimeter and No.1 ADC.
  3. The Standby Airspeed indicator / Standby Altimeter only. ✓
正确答案：The Standby Airspeed indicator / Standby Altimeter only.　·　737　·　来源 b737.org.uk

8.The Weather Radar ON / OFF selector is located on the

  1. EFIS control panel. ✓
  2. Weather radar control panel.
  3. MCP control panel.
正确答案：EFIS control panel.　·　737　·　来源 b737.org.uk

9.The No 1 VHF NAV is agility tuning. The DME-1 indications on each RDMI

  1. Will display the DME distance to each tuned DME.
  2. Will display 4 dashes. ✓
  3. Will display a warning flag.
正确答案：Will display 4 dashes.　·　737　·　来源 b737.org.uk

10.Before selecting the ILS test facility

  1. Select an ILS frequency on the associated VHF NAV control panel. ✓
  2. Select an ILS frequency on the both VHF NAV control panels.
  3. Select an ILS or VOR frequency on the associated VHF NAV control panel.
正确答案：Select an ILS frequency on the associated VHF NAV control panel.　·　737　·　来源 b737.org.uk

11.If the No 1 ADF mode selector is selected to TEST, the No 1 ADF needle on both RDMIs should

  1. Rotate clockwise continuously.
  2. Indicate 90 degrees right of the lubber line.
  3. Indicate 45 degrees left of the lubber line. ✓
正确答案：Indicate 45 degrees left of the lubber line.　·　737　·　来源 b737.org.uk

12.The marker beacon sensitivity selector is located

  1. On both the Captain's and First Officer's control panel.
  2. On the First Officer's instrument panel.
  3. On the Captains instrument panel. ✓
正确答案：On the Captains instrument panel.　·　737　·　来源 b737.org.uk

13.During auto tuning the No. 1 VHF NAV radio is providing unreliable data for position updating to the FMC. The VHF NAV control panel automatic frequency window will

  1. Display ---- (Update 4 FMC or above.)
  2. Display 108.00 (update 4 FMC or above.) ✓
  3. Display the frequency of the unreliable DME station.
正确答案：Display 108.00 (update 4 FMC or above.)　·　737　·　来源 b737.org.uk

14.The Mach/Airspeed indicator's Mach Digital Counter shows

  1. The aircraft's Mach number, from .25 to .99 Mach, in digital form
  2. The aircraft's Mach number, from .50 to .99 Mach, in digital form and is masked below .50 Mach.
  3. The aircraft's Mach number, from .40 to .99 Mach, in digital form and is masked below .40 Mach. ✓
正确答案：The aircraft's Mach number, from .40 to .99 Mach, in digital form and is masked below .40 Mach.　·　737　·　来源 b737.org.uk

15.The Mach/Airspeed indicator's MACH warning flag will be in view when

  1. The mach number is at or below .35 Mach.
  2. The mach number is at or below .40 Mach.
  3. The mach digital counter display is unreliable. ✓
正确答案：The mach digital counter display is unreliable.　·　737　·　来源 b737.org.uk

16.The Mach/Airspeed indicator's A/S warning flag will be in view when

  1. The Airspeed Digital counter is unreliable only.
  2. The Airspeed Pointer and Airspeed Digital counter are unreliable. ✓
  3. The airspeed pointer exceeds the Vmo pointer.
正确答案：The Airspeed Pointer and Airspeed Digital counter are unreliable.　·　737　·　来源 b737.org.uk

17.The Altimeter OFF warning flag is in view when

  1. The indicated altitude is below zero feet.
  2. The Reference Altitude Marker control knob is pulled.
  3. The ADC signal is lost or a malfunction exists. ✓
正确答案：The ADC signal is lost or a malfunction exists.　·　737　·　来源 b737.org.uk

18.The standby altimeter indicator utilises the

  1. The alternate static source. ✓
  2. The normal static source.
  3. The No.1 ADC and the alternate static source.
正确答案：The alternate static source.　·　737　·　来源 b737.org.uk

19.The Vertical Speed pointer on the VSI indicates zero with the OFF flag in view

  1. When the associated static source is blocked.
  2. When the associated IRS vertical speed is unreliable. ✓
  3. When the alternate static source is selected.
正确答案：When the associated IRS vertical speed is unreliable.　·　737　·　来源 b737.org.uk

20.The Standby Horizon is

  1. Normally powered when any one or more generators are on line.
  2. Normally powered at all times even with the loss of all AC generators. ✓
  3. Only powered from the No2 AC Transfer Bus.
正确答案：Normally powered at all times even with the loss of all AC generators.　·　737　·　来源 b737.org.uk

21.On aircraft fitted with a Air Temp/True airspeed indicator, the displays are derived from data from

  1. ADC No. 1. ✓
  2. ADC No. 2.
  3. Standby ADC.
正确答案：ADC No. 1.　·　737　·　来源 b737.org.uk

22.How many Air Data Computers are fitted to the B737

  1. 2 (1 AC powered and 1 DC powered).
  2. 3 (2 AC powered and 1 DC powered).
  3. 2 (both AC powered). ✓
正确答案：2 (both AC powered).　·　737　·　来源 b737.org.uk

23.On the ground the TAT indication is approximately the outside air temperature

  1. Provided the pitot heat is OFF. ✓
  2. Provided the pitot heat is ON.
  3. Irrespective of the pitot heat being ON or OFF.
正确答案：Provided the pitot heat is OFF.　·　737　·　来源 b737.org.uk

24.The Standby Horizon ILS selector when selected to OFF

  1. Retracts the ILS pointers and ILS failure flags from view. ✓
  2. Retracts the ILS pointers only from view.
  3. Retracts the ILS failure flags from view only.
正确答案：Retracts the ILS pointers and ILS failure flags from view.　·　737　·　来源 b737.org.uk

25.If a DEU fails prior to engaging the second autopilot for a dual autopilot approach, engagement of the second autopilot is only possible above 1,500 feet AGL.

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

26.The Expanded Localizer Scale is displayed when the autopilot or flight director is in LOC mode, deviation is:

  1. Slightly more than one dot and track is within 7 degrees of the MCP selected course.
  2. Slightly more than half a dot.
  3. Slightly more than half a dot and track is within 5 degrees of the MCP selected course. ✓
  4. Slightly more than one dot and track is within 3 degrees of the MCP selected course.
正确答案：Slightly more than half a dot and track is within 5 degrees of the MCP selected course.　·　MAX　·　来源 smartcockpit.com

27.With the CONTROL PANEL select switch on the DISPLAYS Source Panel in the BOTH ON 2 position:

  1. The first officer's EFIS Control Panel is supplying identical inputs to the captain's & first officer's displays ✓
  2. Both pilots displays are using the No.2 symbol generator.
  3. DEU 2 controls all six display units.
  4. ADIRU inputs for both the L & R ADIRU are being received from the first officer's pitot probe
正确答案：The first officer's EFIS Control Panel is supplying identical inputs to the captain's & first officer's displays　·　MAX　·　来源 smartcockpit.com

28.If the Upper Display fails:

  1. The engine display automatically moves to the Inboard display and the Upper display blanks.
  2. The engine display automatically moves to the Outboard display and the Upper display blanks.
  3. The engine display automatically moves to the Lower display and the Upper display blanks. ✓
  4. The engine display automatically moves to the Inboard or Outboard display and the Upper display blanks.
正确答案：The engine display automatically moves to the Lower display and the Upper display blanks.　·　MAX　·　来源 smartcockpit.com

29.AOA Disagree Alert (amber) - It indicates the Captainu2019s (left) and First Officeru2019s (right) angle of attack values disagree by:

  1. More than 10 degrees for more than 10 continuous seconds. ✓
  2. More than 5 degrees for more than 10 continuous seconds.
  3. More than 5 degrees for more than 5 continuous seconds.
  4. More than 7 degrees for more than 5 continuous seconds.
正确答案：More than 10 degrees for more than 10 continuous seconds.　·　MAX　·　来源 smartcockpit.com

30.The FMC Alerting Message VERIFY POSITION indicates:

  1. The airplane is excessively off the flight planned course.
  2. Position information is contradictory ✓
  3. The latitude-longitude position is not within 1 NM of the origin airport
  4. The latitude or longitude position is not within 1 NM of the origin airport
正确答案：Position information is contradictory　·　MAX　·　来源 smartcockpit.com

31.The purpose of the FMC LEGS page is to display the lateral and vertical flight path details for each waypoint and to make route modifications involving a portion of a route segment.

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

32.When the ROLL amber flag appears on the Attitude indicator, Captainu2019s and F/Ou2019s roll angle displays differ by more than:

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

33.Top of the red and black bar indicates the speed at which:

  1. 1.3g maneuver capability occurs at 40 degrees of bank.
  2. Stick shaker occurs. ✓
  3. 1.4g maneuver capability occurs at 40 degrees of bank
  4. Minimum maneuver speed that permits a 40-degree bank.
正确答案：Stick shaker occurs.　·　MAX　·　来源 smartcockpit.com

34.The ND Wind direction-speed and wind arrow is:

  1. Displayed in only in ND MAP mode.
  2. Blanked if wind speed becomes less than 6 knots.
  3. Displayed if wind speed is greater than 6 knots. ✓
  4. Displayed only in ILS mode.
正确答案：Displayed if wind speed is greater than 6 knots.　·　MAX　·　来源 smartcockpit.com

35.The amber crosshatched area indicates:

  1. The FMC landing altitude for the destination runway or the landing altitude for departure runway.
  2. The FMC landing altitude for the destination runway or the landing altitude for departure runway or airport until 400 NM from departure.
  3. The FMC landing altitude for the destination runway or airport, or the landing altitude for departure runway or airport until 400 NM from departure or one-half the distance to destination, whichever occurs first. ✓
  4. The destination landing altitude for the designated runway or the landing altitude for departure airport until 400 NM from departure.
正确答案：The FMC landing altitude for the destination runway or airport, or the landing altitude for departure runway or airport until 400 NM from departure or one-half the distance to destination, whichever occurs first.　·　MAX　·　来源 smartcockpit.com

36.Pitch Limit Indication is displayed in amber and it indicates pitch limit (stick shaker activation for existing flight conditions). It is displayed when:

  1. When the flaps are not up and it also displayed at slow speeds with the flaps up. ✓
  2. When flaps are up.
  3. When flaps are not up.
  4. In all conditions.
正确答案：When the flaps are not up and it also displayed at slow speeds with the flaps up.　·　MAX　·　来源 smartcockpit.com

37.The Static Air temperature is displayed on:

  1. The CDU IDENT page.
  2. The CDU PERF INIT page.
  3. The CDU CLB page.
  4. The CDU PROGRESS page. ✓
正确答案：The CDU PROGRESS page.　·　MAX　·　来源 smartcockpit.com

38.Weather Radar Annunciations (expanded and center MAP, expanded APP, expanded VOR modes) - What does the amber WXR ATT indicate?

  1. Weather radar has failed. No weather data are displayed.
  2. Range data input has failed. Only displayed in WXR TEST.
  3. Attitude stabilization for antenna has been lost. ✓
  4. Range data input has failed.
正确答案：Attitude stabilization for antenna has been lost.　·　MAX　·　来源 smartcockpit.com

39.On the FMC TAKEOFF REF Page, the SEL temperature entry may be made in either degrees Celsius or Fahrenheit:

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

40.Concerning Navigation Display Information, Heading is supplied by Air Data Inertial Reference System (ADIRS) and Track is supplied by the FMC during normal operation.

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

41.Selection of an ILS approach from a DEP-ARR page will automatically remove a previously selected approach:

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

42.EFIS Control Panel - WXR (weather radar): when the 640 nm range is selected, weather radar returns are limited to:

  1. 320 nm. ✓
  2. 160 nm.
  3. 80 nm
  4. 40 nm.
正确答案：320 nm.　·　MAX　·　来源 smartcockpit.com

43.The bottom of the red and black bar indicates the:

  1. Maximum speed as limited by the lowest of the Vmo-Mmo, landing gear placard speed and flap placard speed. ✓
  2. Maximum maneuver speed.
  3. 1.3g maneuver capability that occurs at 40 degrees of bank in level flight.
  4. 1.3g maneuver capability occurs at 45 degrees of bank in level flight.
正确答案：Maximum speed as limited by the lowest of the Vmo-Mmo, landing gear placard speed and flap placard speed.　·　MAX　·　来源 smartcockpit.com

44.Reduced maneuver capability exists when operating within the amber regions below the minimum maneuver speed or above the maximum maneuver speed. During non-normal conditions the target speed may be below the minimum maneuver speed.

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

45.Vertical speed is displayed in white and it shows vertical speed when greater than _____. The display is located above the vertical speed indication when climbing and below when descending.

  1. 100 fpm.
  2. 500 fpm.
  3. 80 fpm.
  4. 400 fpm. ✓
正确答案：400 fpm.　·　MAX　·　来源 smartcockpit.com

46.If a DEU fails above FL220:

  1. The autopilot and flight directors are not affected ✓
  2. The flight director pitch command bar is removed from both pilotu2019s displays.
  3. The flight director pitch command bar is removed from both pilotu2019s displays and the autopilot is inoperative.
  4. The autopilot engages in CWS P.
正确答案：The autopilot and flight directors are not affected　·　MAX　·　来源 smartcockpit.com

47.The white position trend vector with (dashed lines) is displayed in MAP and MAP CTR. Predicts position at the end of 60, 90, and 120 second intervals.

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

48.To climb to FL280 in the shortest distance, MAX ANGLE should be selected on this page:

  1. CLB or CRZ
  2. PROG
  3. CLB ✓
  4. CLB or PERF
正确答案：CLB　·　MAX　·　来源 smartcockpit.com

49.Display System Annunciations - When there is a problem with the DEU display system, and when CDS MAINT is shown in white in the lower left corner of the PFD:

  1. A dispatchable CDS fault has occurred. Displayed on the ground only, prior to start of the second engine. ✓
  2. A non-dispatchable CDS fault has occurred. Displayed on the ground only, prior to start of the second engine.
  3. A dispatchable CDS fault has occurred. Displayed on the ground only.
  4. A non-dispatchable CDS fault has occurred. Displayed on the ground only, prior to start of the first engine.
正确答案：A dispatchable CDS fault has occurred. Displayed on the ground only, prior to start of the second engine.　·　MAX　·　来源 smartcockpit.com

50.The rising runway is displayed when localizer pointer is in view and radio altitude is less than ____ feet.

  1. 200
  2. 500
  3. 1500
  4. 2500 ✓
正确答案：2500　·　MAX　·　来源 smartcockpit.com

51.The white position trend vector with (dashed lines) is displayed in MAP and MAP CTR. Selected range determines the number of segments displayed. For a range of more than 20 nm, there are 3 segments. For a range of 20 nm, there are 2 segments. For a range less or equal than 10 nm, there is only 1 segment.

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

52.What is the purpose of the Air Data Modules (ADMs)?

  1. The ADMs provide only pitot & static pressure to the standby instruments.
  2. The ADMs provide inertial position & track data to the displays thru the ADIRUs.
  3. The ADMs measure thru the Alpha vanes the airplane angle-of-attack.
  4. The ADMs convert pneumatic pressure to electrical signals and send these data to the ADIRUs. ✓
正确答案：The ADMs convert pneumatic pressure to electrical signals and send these data to the ADIRUs.　·　MAX　·　来源 smartcockpit.com

53.Airspeed Disagree Alert (amber) - Indicates the Captainu2019s and First Officeru2019s airspeed indications disagree by:

  1. More than 8 knots for 5 continuous seconds.
  2. More than 10 knots for 5 continuous seconds.
  3. More than 15 knots for 5 continuous seconds.
  4. More than 5 knots for 5 continuous seconds. ✓
正确答案：More than 5 knots for 5 continuous seconds.　·　MAX　·　来源 smartcockpit.com

54.WPT (waypoint)- displays the waypoints in the FMC data base which are not in the flight plan route if the selected range is:

  1. 160 nm or less.
  2. 20 nm or less.
  3. 40 nm or less. ✓
  4. 80 nm or less.
正确答案：40 nm or less.　·　MAX　·　来源 smartcockpit.com

55.An airspeed trend vector indicates predicted airspeed in:

  1. 5 seconds.
  2. 10 seconds. ✓
  3. 15 seconds.
  4. 20 seconds.
正确答案：10 seconds.　·　MAX　·　来源 smartcockpit.com

56.Magnetic-True Heading is annunciated in green. When TRU is displayed and the airplane descends _____, an amber box is drawn around TRU. The box flashes for 10 seconds, then turns steady amber.

  1. Below 10,000 feet at a descent rate greater than 1000 fpm.
  2. Below 20,000 feet.
  3. Below 10,000 feet.
  4. More than 2000 feet at a descent rate greater than 800 fpm. ✓
正确答案：More than 2000 feet at a descent rate greater than 800 fpm.　·　MAX　·　来源 smartcockpit.com

57.EFIS Control Panel - Pushing the WXR (weather radar) switch energizes the weather radar transmitter and displays weather radar returns in _____.

  1. MAP, expanded VOR, and expanded APP modes
  2. MAP, and expanded VOR modes.
  3. MAP, center MAP, and expanded APP modes
  4. MAP, center MAP, expanded VOR, and expanded APP modes. ✓
正确答案：MAP, center MAP, expanded VOR, and expanded APP modes.　·　MAX　·　来源 smartcockpit.com

58.The flight recorder OFF Light (amber) is illuminated. What does this indicate?

  1. The recorder is not operating or the test is invalid.
  2. The recorder is not operating or the test is invalid. It may also indicate a power failure, a loss of input data, or an electronic malfunction. ✓
  3. The flight recorder is inoperative or not powered.
  4. The flight recorder is inoperative or not powered. It may also indicate an electronic malfunction.
正确答案：The recorder is not operating or the test is invalid. It may also indicate a power failure, a loss of input data, or an electronic malfunction.　·　MAX　·　来源 smartcockpit.com

59.If the FAULT light on the IRS Mode Selector Unit illuminates, what does it indicate?

  1. A failure of a Symbol Generator or a system fault affective NAV Mode of the ADIRU.
  2. An entry of an invalid present position
  3. A system fault affecting the respective IRS ATT and or NAV Mode ✓
  4. That DC power for the respective IRS is degraded.
正确答案：A system fault affecting the respective IRS ATT and or NAV Mode　·　MAX　·　来源 smartcockpit.com

60.The V2+15 white bug of the airspeed indicator is normally displayed for takeoff. It is removed:

  1. At first flap retraction or when VREF is entered ✓
  2. When landing gear lever is placed UP
  3. When speed is more than 250 knots KIAS
  4. All statements are correct.
正确答案：At first flap retraction or when VREF is entered　·　MAX　·　来源 smartcockpit.com

61.During PATH DESCENT and below the speed restriction altitude, the FMC OVERSPEED DISCONNECT alerting message is displayed. What does this indicate?

  1. VNAV has disengaged because airspeed has exceeded FMC speed restriction by more than 15 knots. ✓
  2. The FMC has disengaged the autothrottles due to excessive speed.
  3. VNAV has disengaged at VMO minus 5 knots.
  4. VNAV has disengaged because airspeed has exceeded FMC target speed by more than 10 knots.
正确答案：VNAV has disengaged because airspeed has exceeded FMC speed restriction by more than 15 knots.　·　MAX　·　来源 smartcockpit.com

62.If you select the BOTH ON 1 switch of the CONTROL PANEL:

  1. Both the Captainu2019s and First Officeru2019s CDS displays and baro are controlled from the left EFIS panel ✓
  2. The Right EFIS control panel controls both pilots' outboard and inboard display units.
  3. The Left ADIRS controls both pilots' outboard and inboard display units.
  4. The Right ADIRS controls both pilots' outboard and inboard display units.
正确答案：Both the Captainu2019s and First Officeru2019s CDS displays and baro are controlled from the left EFIS panel　·　MAX　·　来源 smartcockpit.com

63.The Slip-Skid Indication displaces beneath the bank pointer to indicate slip or skid. It turns amber if:

  1. Bank angle is 35 degrees or more. ✓
  2. Bank angle is 42 degrees or more.
  3. Bank angle is 45 degrees or more.
  4. Bank angle is 40 degrees or more.
正确答案：Bank angle is 35 degrees or more.　·　MAX　·　来源 smartcockpit.com

64.The ND wind direction-speed and wind arrow is displayed:

  1. If wind magnitude is greater than 6 knots and blanked if wind magnitude becomes less than 4 knots. ✓
  2. If wind magnitude is greater than 2 knots and blanked if wind magnitude becomes less than 2 knots.
  3. If wind magnitude is greater than 5 knots and blanked if wind magnitude becomes less than 4 knots.
  4. If wind magnitude is greater than 3 knots and blanked if wind magnitude becomes less than 3 knots.
正确答案：If wind magnitude is greater than 6 knots and blanked if wind magnitude becomes less than 4 knots.　·　MAX　·　来源 smartcockpit.com

65.When flaps are up, the bottom of the amber bar indicates the:

  1. 1.3g maneuver capability to high speed buffet.
  2. Maximum maneuver speed. ✓
  3. 1.4g maneuver capability to high speed buffet.
  4. 1.5g maneuver capability to high speed buffet.
正确答案：Maximum maneuver speed.　·　MAX　·　来源 smartcockpit.com

66.On which CDU is the ground speed displayed?

  1. PROGRESS page 1
  2. CRZ
  3. POS REF page 2 ✓
  4. INIT REF
正确答案：POS REF page 2　·　MAX　·　来源 smartcockpit.com

67.Weather Radar Annunciations (expanded and center MAP, expanded APP, expanded VOR modes) - What does the amber WXR WEAK indicate?

  1. WXR data input is degraded.
  2. Range data input has failed. Only displayed in WXR TEST.
  3. Weather radar calibration fault. ✓
  4. Antenna stabilization is degraded.
正确答案：Weather radar calibration fault.　·　MAX　·　来源 smartcockpit.com

68.The Altitude Disagree Alert indicates the Captainu2019s and F/Ou2019s altitude indications disagree by:

  1. More than 200 feet for more than 5 continuous seconds. ✓
  2. More than 150 feet for more than 5 continuous seconds.
  3. More than 100 feet for more than 5 continuous seconds.
  4. More than 300 feet for more than 5 continuous seconds.
正确答案：More than 200 feet for more than 5 continuous seconds.　·　MAX　·　来源 smartcockpit.com

69.The Bank Pointer indicates bank angle. It fills and turns amber if bank angle is 35 degrees or more.

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

70.The altitude range arc (also called the green banana by Boeing pilots) is displayed in MAP and MAP CTR modes. It indicates the approximate map position where the MCP altitude will be reached. It is based on:

  1. Vertical speed.
  2. Vertical speed and groundspeed ✓
  3. Vertical speed and speed constraints.
  4. Vertical speed, speed and altitude constraints.
正确答案：Vertical speed and groundspeed　·　MAX　·　来源 smartcockpit.com

71.The Landing Altitude Reference Bar is displayed vertically and it indicates height above touchdown. The bar is white between ______ above landing altitude and it is amber between ______ above landing altitude.

  1. 500 to 1500 feet and minimums to 500 feet.
  2. 500 to 1000 feet and 0 to 500 feet. ✓
  3. 500 to 2500 feet and minimums to 500 feet.
  4. 500 to 5000 feet and 0 to 500 feet.
正确答案：500 to 1000 feet and 0 to 500 feet.　·　MAX　·　来源 smartcockpit.com

72.The standby attitude indicator provides attitude information that is independent of the primary attitude displays. The indicator is powered by:

  1. The Battery bus. ✓
  2. The Transfer bus 1.
  3. The Transfer bus 2.
  4. The TR2.
正确答案：The Battery bus.　·　MAX　·　来源 smartcockpit.com

73.On ground, the PERF DEFAULTS INVALID alerting message is displayed. What does this indicate?

  1. Validity check of performance defaults database has failed. ✓
  2. DC power is not available to the performance module.
  3. AC power is not available to the performance module.
  4. AC or DC power is not available to the performance module.
正确答案：Validity check of performance defaults database has failed.　·　MAX　·　来源 smartcockpit.com

74.The current Mach number is displayed when airspeed increases above ___ Mach.

  1. 0.30
  2. 0.40 ✓
  3. 0.50
  4. 0.60
正确答案：0.40　·　MAX　·　来源 smartcockpit.com

75.The standby radio magnetic indicator (RMI) displays magnetic heading and VOR-ADF bearing to the station. The RMI is powered by:

  1. The AC transfer bus 2
  2. The AC standby bus ✓
  3. The DC standby bus.
  4. The TR3.
正确答案：The AC standby bus　·　MAX　·　来源 smartcockpit.com

76.STA (station) displays all FMC data base navigation aids if on map scales ______.

  1. 5, 10, 20 or 40 nm. ✓
  2. 5, 10, or 20 nm.
  3. 80, 160, 320 or 640 nm.
  4. 80, 160, or 320 nm.
正确答案：5, 10, 20 or 40 nm.　·　MAX　·　来源 smartcockpit.com

77.The amber crosshatched area indicates:

  1. The FMC landing altitude for the destination runway or the landing altitude for departure runway.
  2. The FMC landing altitude for the destination runway or the landing altitude for departure runway or airport until 400 NM from departure.
  3. The FMC landing altitude for the destination runway or airport, or the landing altitude for departure runway or airport until 400 NM from departure or one-half the distance to destination, whichever occurs first. ✓
  4. The destination landing altitude for the designated runway or the landing altitude for departure airport until 400 NM from departure.
正确答案：The FMC landing altitude for the destination runway or airport, or the landing altitude for departure runway or airport until 400 NM from departure or one-half the distance to destination, whichever occurs first.　·　NG　·　来源 smartcockpit.com

78.If you select the "BOTH ON 1" switch of the CONTROL PANEL:

  1. Both the Captain’s and First Officer’s CDS displays and baro are controlled from the left EFIS panel ✓
  2. The Right EFIS control panel controls both pilots' outboard and inboard display units.
  3. The Left ADIRS controls both pilots' outboard and inboard display units.
  4. The Right ADIRS controls both pilots' outboard and inboard display units.
正确答案：Both the Captain’s and First Officer’s CDS displays and baro are controlled from the left EFIS panel　·　NG　·　来源 smartcockpit.com

79.Top of the red and black bar indicates the speed at which:

  1. 1.3g maneuver capability occurs at 40 degrees of bank.
  2. Stick shaker occurs. ✓
  3. 1.4g maneuver capability occurs at 40 degrees of bank
  4. Minimum maneuver speed that permits a 40-degree bank.
正确答案：Stick shaker occurs.　·　NG　·　来源 smartcockpit.com

80.The flight recorder OFF Light (amber) is illuminated. What does this indicate?

  1. The recorder is not operating or the test is invalid.
  2. The recorder is not operating or the test is invalid. It may also indicate a power failure, a loss of input data, or an electronic malfunction. ✓
  3. The flight recorder is inoperative or not powered.
  4. The flight recorder is inoperative or not powered. It may also indicate an electronic malfunction.
正确答案：The recorder is not operating or the test is invalid. It may also indicate a power failure, a loss of input data, or an electronic malfunction.　·　NG　·　来源 smartcockpit.com

81.Airspeed Disagree Alert (amber) - Indicates the Captain’s and First Officer’s airspeed indications disagree by:

  1. More than 8 knots for 5 continuous seconds.
  2. More than 10 knots for 5 continuous seconds.
  3. More than 15 knots for 5 continuous seconds.
  4. More than 5 knots for 5 continuous seconds. ✓
正确答案：More than 5 knots for 5 continuous seconds.　·　NG　·　来源 smartcockpit.com

82.On which CDU is the ground speed displayed?

  1. PROGRESS page 1
  2. CRZ
  3. POS REF page 2 ✓
  4. INIT REF
正确答案：POS REF page 2　·　NG　·　来源 smartcockpit.com

83.The standby radio magnetic indicator (RMI) displays magnetic heading and VOR-ADF bearing to the station. The RMI is powered by:

  1. The AC transfer bus 2
  2. The AC standby bus ✓
  3. The DC standby bus.
  4. The TR3.
正确答案：The AC standby bus　·　NG　·　来源 smartcockpit.com

84.The standby attitude indicator provides attitude information that is independent of the primary attitude displays. The indicator is powered by:

  1. The Battery bus. ✓
  2. The Transfer bus 1.
  3. The Transfer bus 2.
  4. The TR2.
正确答案：The Battery bus.　·　NG　·　来源 smartcockpit.com

85.On the FMC TAKEOFF REF Page, the SEL temperature entry may be made in either degrees Celsius or Fahrenheit:

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

86.If a DEU fails prior to engaging the second autopilot for a dual autopilot approach, engagement of the second autopilot is only possible above 1,500 feet AGL.

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

87.The Slip-Skid Indication displaces beneath the bank pointer to indicate slip or skid. It turns amber if:

  1. Bank angle is 35 degrees or more. ✓
  2. Bank angle is 42 degrees or more.
  3. Bank angle is 45 degrees or more.
  4. Bank angle is 40 degrees or more.
正确答案：Bank angle is 35 degrees or more.　·　NG　·　来源 smartcockpit.com

88.The bottom of the red and black bar indicates the:

  1. Maximum speed as limited by the lowest of the Vmo-Mmo, landing gear placard speed and flap placard speed. ✓
  2. Maximum maneuver speed.
  3. 1.3g maneuver capability that occurs at 40 degrees of bank in level flight.
  4. 1.3g maneuver capability occurs at 45 degrees of bank in level flight.
正确答案：Maximum speed as limited by the lowest of the Vmo-Mmo, landing gear placard speed and flap placard speed.　·　NG　·　来源 smartcockpit.com

89.On ground, the PERF DEFAULTS INVALID alerting message is displayed. What does this indicate?

  1. Validity check of performance defaults database has failed. ✓
  2. DC power is not available to the performance module.
  3. AC power is not available to the performance module.
  4. AC or DC power is not available to the performance module.
正确答案：Validity check of performance defaults database has failed.　·　NG　·　来源 smartcockpit.com

90.The ND wind direction-speed and wind arrow is displayed:

  1. If wind magnitude is greater than 6 knots and blanked if wind magnitude becomes less than 4 knots. ✓
  2. If wind magnitude is greater than 2 knots and blanked if wind magnitude becomes less than 2 knots.
  3. If wind magnitude is greater than 5 knots and blanked if wind magnitude becomes less than 4 knots.
  4. If wind magnitude is greater than 3 knots and blanked if wind magnitude becomes less than 3 knots.
正确答案：If wind magnitude is greater than 6 knots and blanked if wind magnitude becomes less than 4 knots.　·　NG　·　来源 smartcockpit.com

91.What is the purpose of the Air Data Modules (ADMs)?

  1. The ADMs provide only pitot & static pressure to the standby instruments.
  2. The ADMs provide inertial position & track data to the displays thru the ADIRUs.
  3. The ADMs measure thru the Alpha vanes the airplane angle-of-attack.
  4. The ADMs convert pneumatic pressure to electrical signals and send these data to the ADIRUs. ✓
正确答案：The ADMs convert pneumatic pressure to electrical signals and send these data to the ADIRUs.　·　NG　·　来源 smartcockpit.com

92.During PATH DESCENT and below the speed restriction altitude, the FMC "OVERSPEED DISCONNECT" alerting message is displayed. What does this indicate?

  1. VNAV has disengaged because airspeed has exceeded FMC speed restriction by more than 15 knots. ✓
  2. The FMC has disengaged the autothrottles due to excessive speed.
  3. VNAV has disengaged at VMO minus 5 knots.
  4. VNAV has disengaged because airspeed has exceeded FMC target speed by more than 10 knots.
正确答案：VNAV has disengaged because airspeed has exceeded FMC speed restriction by more than 15 knots.　·　NG　·　来源 smartcockpit.com

93.The purpose of the FMC LEGS page is to display the lateral and vertical flight path details for each waypoint and to make route modifications involving a portion of a route segment.

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

94.To climb to FL280 in the shortest distance, MAX ANGLE should be selected on this page:

  1. CLB or CRZ
  2. PROG
  3. CLB ✓
  4. CLB or PERF
正确答案：CLB　·　NG　·　来源 smartcockpit.com

95.The current Mach number is displayed when airspeed increases above ___ Mach.

  1. 0.30
  2. 0.40 ✓
  3. 0.50
  4. 0.60
正确答案：0.40　·　NG　·　来源 smartcockpit.com

96.The altitude range arc (also called "the green banana" by Boeing pilots) is displayed in MAP and MAP CTR modes. It indicates the approximate map position where the MCP altitude will be reached. It is based on:

  1. Vertical speed.
  2. Vertical speed and groundspeed ✓
  3. Vertical speed and speed constraints.
  4. Vertical speed, speed and altitude constraints.
正确答案：Vertical speed and groundspeed　·　NG　·　来源 smartcockpit.com

97.EFIS Control Panel - WXR (weather radar): when the 640 nm range is selected, weather radar returns are limited to:

  1. 320 nm. ✓
  2. 160 nm.
  3. 80 nm
  4. 40 nm.
正确答案：320 nm.　·　NG　·　来源 smartcockpit.com

98.The ND Wind direction-speed and wind arrow is:

  1. Displayed in only in ND MAP mode.
  2. Blanked if wind speed becomes less than 6 knots.
  3. Displayed if wind speed is greater than 6 knots. ✓
  4. Displayed only in ILS mode.
正确答案：Displayed if wind speed is greater than 6 knots.　·　NG　·　来源 smartcockpit.com

99.Weather Radar Annunciations (expanded and center MAP, expanded APP, expanded VOR modes) - What does the amber WXR ATT indicate?

  1. Weather radar has failed. No weather data are displayed.
  2. Range data input has failed. Only displayed in WXR TEST.
  3. Attitude stabilization for antenna has been lost. ✓
  4. Range data input has failed.
正确答案：Attitude stabilization for antenna has been lost.　·　NG　·　来源 smartcockpit.com

100.The V2+15 white bug of the airspeed indicator is normally displayed for takeoff. It is removed:

  1. At first flap retraction or when VREF is entered ✓
  2. When landing gear lever is placed UP
  3. When speed is more than 250 knots KIAS
  4. All statements are correct.
正确答案：At first flap retraction or when VREF is entered　·　NG　·　来源 smartcockpit.com

101.Magnetic-True Heading is annunciated in green. When TRU is displayed and the airplane descends _____, an amber box is drawn around TRU. The box flashes for 10 seconds, then turns steady amber.

  1. Below 10,000 feet at a descent rate greater than 1000 fpm.
  2. Below 20,000 feet.
  3. Below 10,000 feet.
  4. More than 2000 feet at a descent rate greater than 800 fpm. ✓
正确答案：More than 2000 feet at a descent rate greater than 800 fpm.　·　NG　·　来源 smartcockpit.com

102.The FMC Alerting Message "VERIFY POSITION" indicates:

  1. The airplane is excessively off the flight planned course.
  2. Position information is contradictory ✓
  3. The latitude-longitude position is not within 1 NM of the origin airport
  4. The latitude or longitude position is not within 1 NM of the origin airport
正确答案：Position information is contradictory　·　NG　·　来源 smartcockpit.com

103.WPT (waypoint) - displays the waypoints in the FMC data base which are not in the flight plan route if the selected range is:

  1. 160 nm or less.
  2. 20 nm or less.
  3. 40 nm or less. ✓
  4. 80 nm or less.
正确答案：40 nm or less.　·　NG　·　来源 smartcockpit.com

104.Pitch Limit Indication is displayed in amber and it indicates pitch limit (stick shaker activation for existing flight conditions). It is displayed when:

  1. When the flaps are not up and it also displayed at slow speeds with the flaps up. ✓
  2. When flaps are up.
  3. When flaps are not up.
  4. In all conditions.
正确答案：When the flaps are not up and it also displayed at slow speeds with the flaps up.　·　NG　·　来源 smartcockpit.com

105.With the CONTROL PANEL select switch on the DISPLAYS Source Panel in the BOTH ON 2 position:

  1. The first officer's EFIS Control Panel is supplying identical inputs to the captain's & first officer's displays ✓
  2. Both pilots displays are using the No.2 symbol generator.
  3. DEU 2 controls all six display units.
  4. ADIRU inputs for both the L & R ADIRU are being received from the first officer's pitot probe
正确答案：The first officer's EFIS Control Panel is supplying identical inputs to the captain's & first officer's displays　·　NG　·　来源 smartcockpit.com

106.EFIS Control Panel - Pushing the WXR (weather radar) switch energizes the weather radar transmitter and displays weather radar returns in _____.

  1. MAP, expanded VOR, and expanded APP modes
  2. MAP, and expanded VOR modes.
  3. MAP, center MAP, and expanded APP modes
  4. MAP, center MAP, expanded VOR, and expanded APP modes. ✓
正确答案：MAP, center MAP, expanded VOR, and expanded APP modes.　·　NG　·　来源 smartcockpit.com

107.STA (station) displays all FMC data base navigation aids if on map scales ______.

  1. 5, 10, 20 or 40 nm. ✓
  2. 5, 10, or 20 nm.
  3. 80, 160, 320 or 640 nm.
  4. 80, 160, or 320 nm.
正确答案：5, 10, 20 or 40 nm.　·　NG　·　来源 smartcockpit.com

108.The white position trend vector with (dashed lines) is displayed in MAP and MAP CTR. Predicts position at the end of 60, 90, and 120 second intervals.

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

109.Display System Annunciations - When there is a problem with the DEU display system, and when CDS MAINT is shown in white in the lower left corner of the PFD:

  1. A dispatchable CDS fault has occurred. Displayed on the ground only, prior to start of the second engine. ✓
  2. A non-dispatchable CDS fault has occurred. Displayed on the ground only, prior to start of the second engine.
  3. A dispatchable CDS fault has occurred. Displayed on the ground only.
  4. A non-dispatchable CDS fault has occurred. Displayed on the ground only, prior to start of the first engine.
正确答案：A dispatchable CDS fault has occurred. Displayed on the ground only, prior to start of the second engine.　·　NG　·　来源 smartcockpit.com

110.The white position trend vector with (dashed lines) is displayed in MAP and MAP CTR. Selected range determines the number of segments displayed. For a range of more than 20 nm, there are 3 segments. For a range of 20 nm, there are 2 segments. For a range less or equal than 10 nm, there is only 1 segment.

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

111.The rising runway is displayed when localizer pointer is in view and radio altitude is less than ____ feet.

  1. 200
  2. 500
  3. 1500
  4. 2500 ✓
正确答案：2500　·　NG　·　来源 smartcockpit.com

112.When flaps are up, the bottom of the amber bar indicates the:

  1. 1.3g maneuver capability to high speed buffet.
  2. Maximum maneuver speed. ✓
  3. 1.4g maneuver capability to high speed buffet.
  4. 1.5g maneuver capability to high speed buffet.
正确答案：Maximum maneuver speed.　·　NG　·　来源 smartcockpit.com

113.Concerning Navigation Display Information, Heading is supplied by Air Data Inertial Reference System (ADIRS) and Track is supplied by the FMC during normal operation.

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

114.The Expanded Localizer Scale is displayed when the autopilot or flight director is in LOC mode, deviation is:

  1. Slightly more than one dot and track is within 7 degrees of the MCP selected course.
  2. Slightly more than half a dot.
  3. Slightly more than half a dot and track is within 5 degrees of the MCP selected course. ✓
  4. Slightly more than one dot and track is within 3 degrees of the MCP selected course.
正确答案：Slightly more than half a dot and track is within 5 degrees of the MCP selected course.　·　NG　·　来源 smartcockpit.com

115.If the Upper Display fails:

  1. The engine display automatically moves to the Inboard display and the Upper display blanks.
  2. The engine display automatically moves to the Outboard display and the Upper display blanks.
  3. The engine display automatically moves to the Lower display and the Upper display blanks. ✓
  4. The engine display automatically moves to the Inboard or Outboard display and the Upper display blanks.
正确答案：The engine display automatically moves to the Lower display and the Upper display blanks.　·　NG　·　来源 smartcockpit.com

116.If a DEU fails above FL220:

  1. The autopilot and flight directors are not affected ✓
  2. The flight director pitch command bar is removed from both pilot’s displays.
  3. The flight director pitch command bar is removed from both pilot’s displays and the autopilot is inoperative.
  4. The autopilot engages in CWS P.
正确答案：The autopilot and flight directors are not affected　·　NG　·　来源 smartcockpit.com

117.AOA Disagree Alert (amber) - It indicates the Captain’s (left) and First Officer’s (right) angle of attack values disagree by:

  1. More than 10 degrees for more than 10 continuous seconds. ✓
  2. More than 5 degrees for more than 10 continuous seconds.
  3. More than 5 degrees for more than 5 continuous seconds.
  4. More than 7 degrees for more than 5 continuous seconds.
正确答案：More than 10 degrees for more than 10 continuous seconds.　·　NG　·　来源 smartcockpit.com

118.Reduced maneuver capability exists when operating within the amber regions below the minimum maneuver speed or above the maximum maneuver speed. During non-normal conditions the target speed may be below the minimum maneuver speed.

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

119.When the ROLL amber flag appears on the Attitude indicator, Captain’s and F/O’s roll angle displays differ by more than:

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

120.The Bank Pointer indicates bank angle. It fills and turns amber if bank angle is 35 degrees or more.

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

121.Selection of an ILS approach from a DEP-ARR page will automatically remove a previously selected approach:

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

122.If the FAULT light on the IRS Mode Selector Unit illuminates, what does it indicate?

  1. A failure of a Symbol Generator or a system fault affective NAV Mode of the ADIRU.
  2. An entry of an invalid present position
  3. A system fault affecting the respective IRS ATT and or NAV Mode ✓
  4. That DC power for the respective IRS is degraded.
正确答案：A system fault affecting the respective IRS ATT and or NAV Mode　·　NG　·　来源 smartcockpit.com

123.Weather Radar Annunciations (expanded and center MAP, expanded APP, expanded VOR modes) - What does the amber WXR WEAK indicate?

  1. WXR data input is degraded.
  2. Range data input has failed. Only displayed in WXR TEST.
  3. Weather radar calibration fault. ✓
  4. Antenna stabilization is degraded.
正确答案：Weather radar calibration fault.　·　NG　·　来源 smartcockpit.com

124.The Landing Altitude Reference Bar is displayed vertically and it indicates height above touchdown. The bar is white between ______ above landing altitude and it is amber between ______ above landing altitude.

  1. 500 to 1500 feet and minimums to 500 feet.
  2. 500 to 1000 feet and 0 to 500 feet. ✓
  3. 500 to 2500 feet and minimums to 500 feet.
  4. 500 to 5000 feet and 0 to 500 feet.
正确答案：500 to 1000 feet and 0 to 500 feet.　·　NG　·　来源 smartcockpit.com

125.The Altitude Disagree Alert indicates the Captain’s and F/O’s altitude indications disagree by:

  1. More than 200 feet for more than 5 continuous seconds. ✓
  2. More than 150 feet for more than 5 continuous seconds.
  3. More than 100 feet for more than 5 continuous seconds.
  4. More than 300 feet for more than 5 continuous seconds.
正确答案：More than 200 feet for more than 5 continuous seconds.　·　NG　·　来源 smartcockpit.com

126.The Static Air temperature is displayed on:

  1. The CDU IDENT page.
  2. The CDU PERF INIT page.
  3. The CDU CLB page.
  4. The CDU PROGRESS page. ✓
正确答案：The CDU PROGRESS page.　·　NG　·　来源 smartcockpit.com

127.An airspeed trend vector indicates predicted airspeed in:

  1. 5 seconds.
  2. 10 seconds. ✓
  3. 15 seconds.
  4. 20 seconds.
正确答案：10 seconds.　·　NG　·　来源 smartcockpit.com

128.Vertical speed is displayed in white and it shows vertical speed when greater than _____. The display is located above the vertical speed indication when climbing and below when descending.

  1. 100 fpm.
  2. 500 fpm.
  3. 80 fpm.
  4. 400 fpm. ✓
正确答案：400 fpm.　·　NG　·　来源 smartcockpit.com

129.What colour is the Outer Marker Beacon (OM) displayed on the PFD?

  1. OM appears White in top right corner of AI
  2. OM appears Magenta in lower right corner of Attitude Indicator.
  3. OM appears Cyan in top right corner of AI. ✓
  4. OM appears in Magenta in top right corner of the Attitude Indicator.
正确答案：OM appears Cyan in top right corner of AI.　·　NG　·　来源 Chair Flight B737 Question Bank

130.What does a white CDS MAINT message in the lower left corner of the PFD indicate?

  1. A non-dispatchable CDS fault has occurred post second engine start.
  2. A dispatchable CDS fault has occurred prior to first engine start.
  3. A non-dispatchable CDS fault has occurred prior to second engine start
  4. A dispatchable CDS fault has occurred prior to second engine start. ✓
正确答案：A dispatchable CDS fault has occurred prior to second engine start.　·　NG　·　来源 Chair Flight B737 Question Bank

131.On the PFD, what does the amber annunciation "DISPLAYS CONTROL PANEL" indicate?

  1. The PFD the annunciation is displayed on has an error and information displayed may be erroneous.
  2. The Displays Source Control Panel on the side the annunciation is displayed has failed.
  3. The EFIS control panel on the side the annunciation is displayed has failed ✓
  4. The Display Select Panel on the the side the annunciation is displayed has failed.
正确答案：The EFIS control panel on the side the annunciation is displayed has failed　·　NG　·　来源 Chair Flight B737 Question Bank

132.What does an amber MAP RANGE DISAGREE annunciation on the ND indicate?

  1. The selected range on the EFIS control panel is different from the map display range. ✓
  2. Range information is not being fed to the map display.
  3. There is a difference of more than 10 HPa between the selected QNH
  4. The captains and first officer's altitude indications differ more than 50 feet for more than 5 seconds
正确答案：The selected range on the EFIS control panel is different from the map display range.　·　NG　·　来源 Chair Flight B737 Question Bank

133.When operating on standby power only the Captain's pitot probe is still heated; If the Captain's pitot probe heating fails in this condition, there is no CAPT PITOT alert given.

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