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Boeing 737 · General 题库（94 题）

Boeing 737 机型「General」相关知识共 94 道题。想练习或模拟考试，请到 题库 · 模拟考试。
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1.On 2 battery classic series 737s, the two batteries are:

  1. Connected in series at all times.
  2. Connected in parallel at all times.
  3. Connected in parallel when SBY PWR is selected, or the battery switch is on with TR3 not powered. ✓
正确答案：Connected in parallel when SBY PWR is selected, or the battery switch is on with TR3 not powered.　·　737　·　来源 b737.org.uk

2.On 2 battery classic series 737s, the two batteries:

  1. Can be connected in series to power the SBY PWR system.
  2. Are both charged by one battery charger.
  3. Can provide the SBY PWR system for 45 minutes. ✓
正确答案：Can provide the SBY PWR system for 45 minutes.　·　737　·　来源 b737.org.uk

3.On 2 battery classic series 737s, BAT OVHT and APU BAT OVHT lights:

  1. Are located on the forward overhead panel.
  2. When illuminated require crew action in flight.
  3. Are located on the aft overhead panel. ✓
正确答案：Are located on the aft overhead panel.　·　737　·　来源 b737.org.uk

4.On 2 battery classic series 737s, an APU BAT OVHT light when illuminated indicates:

  1. That the exhaust fans have both failed.
  2. That power to the APU battery charger has been discontinued. ✓
  3. That APU battery charging has been transferred to the main battery charger.
正确答案：That power to the APU battery charger has been discontinued.　·　737　·　来源 b737.org.uk

5.On 2 battery classic series 737s, when operating on SBY PWR:

  1. The first officer's EFIS is available.
  2. The captain's EFIS is available. ✓
  3. Captain's and first officer's EFIS are available.
正确答案：The captain's EFIS is available.　·　737　·　来源 b737.org.uk

6.On 2 battery classic series 737s, the source of power for the APU battery charger is:

  1. The ground service bus with alternate supply from main bus 1.
  2. Main bus 1 with alternate supply from Main bus 2.
  3. Main bus 2 with alternate supply fron the ground service bus. ✓
正确答案：Main bus 2 with alternate supply fron the ground service bus.　·　737　·　来源 b737.org.uk

7.When an Annunciator Panel is pressed, all lights on both panel initially illuminate.

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

8.What does a blue light mean on the Nitrogen Generation System (NGS).

  1. Dim blue means NGS valve agrees with commanded position.
  2. Bright blue means NGS valve closed or disagrees with commanded position
  3. Bright blue means NGS valve closed.
  4. NGS system functioning in a degraded condition. ✓
正确答案：NGS system functioning in a degraded condition.　·　NG　·　来源 Chair Flight B737 Question Bank

9.What colour is the route on the Nav display when you activate a route by pressing the R6 switch?

  1. White
  2. Magenta.
  3. Dashed Cyan ✓
  4. Dashed Magenta
正确答案：Dashed Cyan　·　NG　·　来源 Chair Flight B737 Question Bank

10.Which indications are correct for a single FMC failure (left FMC fails)?

  1. FMC P/RST amber light illuminates, A/P P/RST light illuminates, LNAV and VNAV disconnect if engaged, left ND not available.
  2. FMC P/RST amber light illuminates, FAIL light on FMC CDU illuminates, LNAV and VNAV disconnect if engaged, failure information displayed on left ND after delay of 25 to 30 seconds. ✓
  3. FMC CDU FAIL light illuminates, left FMC CDU screen blanks, left ND screen blanks, LNAV diengages with VNAV remaining available.
  4. FMC P/RST amber light illuminates, normal operation continues with remaining functioning FMC automatically driving both ND screens.
正确答案：FMC P/RST amber light illuminates, FAIL light on FMC CDU illuminates, LNAV and VNAV disconnect if engaged, failure information displayed on left ND after delay of 25 to 30 seconds.　·　NG　·　来源 Chair Flight B737 Question Bank

11.When setting up the FMC, what Pre-flight information is required.

  1. Initial Position, Takeoff and Climb Thrust Limits, Route, Cruise Wind.
  2. Initial Position, Performance Data, Route, Takeoff Data. ✓
  3. Performance Data, Navigation Database, Route, Takeoff Data.
  4. Initial Position, SID, Route, Performance Data, Takeoff Data.
正确答案：Initial Position, Performance Data, Route, Takeoff Data.　·　NG　·　来源 Chair Flight B737 Question Bank

12.What are the 2 databases the FMC uses for operation?

  1. Terrain and Airports
  2. Navigation and Performance ✓
  3. Navigation and Airports
  4. Peformance and Terrain
正确答案：Navigation and Performance　·　NG　·　来源 Chair Flight B737 Question Bank

13.On the DEP/ARR page on the FMC, more than one Arrival be entered.

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

14.On aircraft with a mode selector selection of TEST, WX, WX/TURB and MAP, selecting WX/TURB displays what?

  1. Weather radar returns, and turbulence out to 10 miles whilst on the ground only.
  2. Weather radar returns and turbulence within 40 miles. ✓
  3. Weather radar returns, turbulence out to 40 miles, and windshear out to 20 miles.
  4. Weather radar returns, and windshear out to 40 miles.
正确答案：Weather radar returns and turbulence within 40 miles.　·　NG　·　来源 Chair Flight B737 Question Bank

15.In turbulence mode, at what velocity of horizontal flow of precipitation towards or away from the weather radar will the target display turn magenta?

  1. 10 meters per second or greater.
  2. 7.5 meters per second or greater
  3. 2.5 meters per second or greater
  4. 5 meters per second or greater. ✓
正确答案：5 meters per second or greater.　·　NG　·　来源 Chair Flight B737 Question Bank

16.What forward arc does the weather radar antenna sweep?

  1. 165
  2. 160
  3. 185
  4. 180 ✓
正确答案：180　·　NG　·　来源 Chair Flight B737 Question Bank

17.The IntuVue weather radar fitted in aircraft gives clutter-free viewing of significant weather out to what range?

  1. 320 nautical miles ✓
  2. 120 nautical miles.
  3. 220 nautical miles
  4. 420 nautical miles.
正确答案：320 nautical miles　·　NG　·　来源 Chair Flight B737 Question Bank

18.For the IntuVue Radar, Predictive Windshear mode is automatically turned on in which of the following specific aircraft conditions?

  1. In flight below 1800 feet AGL, on ground with throttle levers set for takeoff. ✓
  2. In flight below 2300 feet AGL, on ground with throttle levers at takeoff position setting.
  3. In flight above 1200 feet RA, on ground with throttle levers at takeoff position setting.
  4. In flight below 1500 feet AGL, on ground with both engines running.
正确答案：In flight below 1800 feet AGL, on ground with throttle levers set for takeoff.　·　NG　·　来源 Chair Flight B737 Question Bank

19.Some weather radar (WXR) panels have an manual altitude control switch (ALT) - when in MAN mode, this can be used to achieve which of the following:

  1. Controls weather analysis altitude from 0 - 60,000 MSL in 1000 feet increments ✓
  2. Manual altitude control is NOT available on any WXR control panels.
  3. Controls weather analysis alitude from 0 - 41,000 feet MSL in 100 feet increments
  4. Controls weather analysis alitude from 500 - 60,000 feet MSL in 100 feet increments
正确答案：Controls weather analysis altitude from 0 - 60,000 MSL in 1000 feet increments　·　NG　·　来源 Chair Flight B737 Question Bank

20.If the aircraft present position cannot be entered through the FMC CDU, it can be entered using the ISDU keyboard.

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

21.If alignment is lost in flight, what action can be taken?

  1. ATT mode can be selected to relevel the system and attain attitude reference, the system can then be returned to ALIGN for the 30 second Fast Align, then returned to NAV once the ALIGN light extinguishes.
  2. IRS mode selector can be selected to ALIGN for 30 seconds then back to NAV to reset the system.
  3. The IRS mode selectors must be moved to OFF to allow FMC to hold all GPS and navigation data for remainder of the flight.
  4. The navigation mode remains unavailable for the rest of the flight, but ALIGN mode can be selected to provide attitude reference.
  5. The navigation mode remains unavailable for the rest of the flight, but ATT mode can be selected to provide attitude reference. ✓
正确答案：The navigation mode remains unavailable for the rest of the flight, but ATT mode can be selected to provide attitude reference.　·　NG　·　来源 Chair Flight B737 Question Bank

22.What components comprise the Flight Management System?

  1. FMCS, AFDS, A/T, MCP, EFIS, ADIRS.
  2. FMCS, AFDS, MCP, IRS, GPS.
  3. FMCS, AFDS, A/T, IRS, GPS. ✓
  4. FMCS, A/P, A/T, MCP, EFIS, IRS.
正确答案：FMCS, AFDS, A/T, IRS, GPS.　·　NG　·　来源 Chair Flight B737 Question Bank

23.What does the top of the amber bar indicate at the lower end of the speed tape?

  1. Minimum manoeuvre speed (1.3g manoeuvre capability to stick shaker below approximately 20,000 feet) - (1.3g manoeuvre capability to low speed buffet above approximately 20,000 feet). ✓
  2. Minimum manoeuvre speed (1.3g manoeuvre capability to stick shaker above approximately 30,000 feet) - (1.3g manoeuvre capability to low speed buffet below approximately 30,000 feet).
  3. Minimum manoeuvre speed (1.3g manoeuvre capability to stick shaker above approximately 20,000 feet) - (1.3g manoeuvre capability to low speed buffet below approximately 20,000 feet).
  4. Minimum manoeuvre speed (1.3g manoeuvre capability to stick shaker below approximately 30,000 feet) - (1.3g manoeuvre capability to low speed buffet above approximately 30,000 feet).
正确答案：Minimum manoeuvre speed (1.3g manoeuvre capability to stick shaker below approximately 20,000 feet) - (1.3g manoeuvre capability to low speed buffet above approximately 20,000 feet).　·　NG　·　来源 Chair Flight B737 Question Bank

24.What does the Magenta figure displayed above the Speed Tape signify?

  1. FMC computed airspeed if the IAS/MACH window is blank.
  2. Airspeed manually selected in the IAS/MACH window.
  3. Current or next speed restriction in the FMC.
  4. Airspeed manually selected in the IAS/MACH window and FMC computed airspeed if the IAS/MACH window is blank. ✓
正确答案：Airspeed manually selected in the IAS/MACH window and FMC computed airspeed if the IAS/MACH window is blank.　·　NG　·　来源 Chair Flight B737 Question Bank

25.The amber annunciation "INSTR SWITCH" indicates what?

  1. The IRS switch on the Forward Overhead panel is not selected to NORMAL ✓
  2. Captain's and First Officer's displays are using separate sources of IRU data.
  3. The IRS switch on the Aft Overhead panel is not selected to NORMAL.
  4. Captain's and First Officer's displays are using the same source of IRU data with the IRS switch selected to OFF.
正确答案：The IRS switch on the Forward Overhead panel is not selected to NORMAL　·　NG　·　来源 Chair Flight B737 Question Bank

26.The bug below that indicates V2 + 15 is displayed at what stage of flight, and when is it removed?

  1. Displayed at Takeoff, removed at first flap retraction or when Vref entered in CDU. ✓
  2. Displayed at takeoff, removed when Pitch Flight director moves to 15 degrees nose up.
  3. Displayed at Approach, removed when flaps at Flap 1 or greater.
  4. Displayed on Approach, removed once right main landing gear is compressed, throttle levers at Idle, and engines have spooled down from Approach Idle to Ground Idle.
正确答案：Displayed at Takeoff, removed at first flap retraction or when Vref entered in CDU.　·　NG　·　来源 Chair Flight B737 Question Bank

27.During approach the Captain observes his BARO minimum reference/altitude turns from green to flashing amber for three seconds, what does this means?

  1. The aircraft has descended below the Captain's selected minimum altitude (DA). ✓
  2. A windshear has been encountered.
  3. Radio altitude data is unreliable.
  4. The aircraft has descended below 1000 feet
正确答案：The aircraft has descended below the Captain's selected minimum altitude (DA).　·　NG　·　来源 Chair Flight B737 Question Bank

28.What does an amber ALT DISAGREE in the bottom of the altimeter tape indicate?

  1. The captain's and first officer's altitude indications differ more than 200 feet for more than 5 seconds ✓
  2. The captains altitude reading and the standby altimeter disagree by more than 200ft for more than 5 seconds
  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 captain's and first officer's altitude indications differ more than 200 feet for more than 5 seconds　·　NG　·　来源 Chair Flight B737 Question Bank

29.What condition causes an Amber IAS DISAGREE alert to appear at the bottom of the speed tape?

  1. Captain's and First Officer's airspeeds disagree by more than 5 kts for more than 5 seconds. ✓
  2. V Ref has not been entered
  3. Difference of more than 10 kts for more than 10 seconds between Captain's and First Officer's airspeed indications.
  4. Selected V Ref is not correct for current aircraft configuration.
正确答案：Captain's and First Officer's airspeeds disagree by more than 5 kts for more than 5 seconds.　·　NG　·　来源 Chair Flight B737 Question Bank

30.How does the Stall Identification system help the pilot identify and prevent further movement into a stalled condition?

  1. The elevator feel shift module prevents the yaw damper from making any rudder movement, and the stick shaker activates.
  2. Elevator Feel Shift Module increase, hydraulic system A pressure to the Elevator Feel and Centering Unit, moving the elevator to provide at least 15 degrees of nose down pitch.
  3. The yaw damper provides 2 degrees of rudder movement, and the speed trim system automatically pushes the control column forward to warn the pilot that a stall condition was being approached.
  4. Elevator Feel Shift Module increase, hydraulic system A pressure to the Elevator Feel and Centering Unit, significantly increasing the force required to move the control column rearwards to continue into a stalled condition. ✓
正确答案：Elevator Feel Shift Module increase, hydraulic system A pressure to the Elevator Feel and Centering Unit, significantly increasing the force required to move the control column rearwards to continue into a stalled condition.　·　NG　·　来源 Chair Flight B737 Question Bank

31.What does a FLT CONTROL "LOW PRESSURE" light illuminated amber indicate?

  1. The STBY RUD system pressure is low.
  2. Both hydraulic systems pressure to ailerons, elevator and rudder are low.
  3. Related hydraulic system pressure to ailerons, elevator and rudder is low. ✓
  4. This light is illuminated whenever the associated FLT CONTROL switch is in the OFF position.
正确答案：Related hydraulic system pressure to ailerons, elevator and rudder is low.　·　NG　·　来源 Chair Flight B737 Question Bank

32.With A/T engaged, what condition could cause the throttles to be separated (not aligned).

  1. One EEC in ON, one EEC in ALTN. ✓
  2. Throttle stagger cannot occur with A/T engaged as both throttle servo motors work identically to position the throttles symetrically.
  3. Both EECs in ALTN.
  4. One engine A/T suffering a system fault.
正确答案：One EEC in ON, one EEC in ALTN.　·　NG　·　来源 Chair Flight B737 Question Bank

33.If both the ON and ALTN lights in the EEC switch are illuminated, what does this indicate?

  1. The EEC is inoperative for that engines.
  2. The soft alternate mode is armed.
  3. The EEC has automatically switched to the soft alternate mode. ✓
  4. The EEC has been manually switched to the soft alternate mode
正确答案：The EEC has automatically switched to the soft alternate mode.　·　NG　·　来源 Chair Flight B737 Question Bank

34.Approach idle is selected in flight by the EECs under what normal conditions(s)?

  1. Below 2,000 feet
  2. Below 15,000 feet
  3. Landing gear extended
  4. Flaps are in landing configuration or engine anti-ice is ON ✓
正确答案：Flaps are in landing configuration or engine anti-ice is ON　·　NG　·　来源 Chair Flight B737 Question Bank

35.What is the indication of an impending oil filter bypass due to contamination?

  1. Illumination of the Master Caution and ENG system annunciator lights.
  2. An amber OIL FILTER BYPASS alert illuminates on the upper display unit. ✓
  3. An amber OIL FILTER BYPASS alert illuminates on the upper display unit and illumination of the Master Caution and ENG system annunciator lights.
  4. Illumination of the FILTER BYPASS warning light on the Fuel Panel.
正确答案：An amber OIL FILTER BYPASS alert illuminates on the upper display unit.　·　NG　·　来源 Chair Flight B737 Question Bank

36.How is the EEC affected the failure of one DEU (Display Electronic Unit) ?

  1. Failure of a single DUE has no effect on the EECs.
  2. Both EECs are rendered inoperative and the EEC ON indication extinguishes.
  3. Both EECs revert to soft alternate mode and the ALTN switch illuminates. ✓
  4. The EEC for the related side reverts to soft alternate mode and the ALTN switch illuminates.
正确答案：Both EECs revert to soft alternate mode and the ALTN switch illuminates.　·　NG　·　来源 Chair Flight B737 Question Bank

37.When does the OIL FILTER BYPASS alert illuminate on the upper display unit?

  1. Illuminates just prior to oil pump bypass opening as pressure gets near to pressure required to open the bypass.
  2. Once the oil filter bypass has opened and oil is bypassing the filter.
  3. If the oil filter bypass has failed in the closed position and oil pressure is beginning to increase.
  4. Illuminates prior to oil bypassing the scavenge filter. ✓
正确答案：Illuminates prior to oil bypassing the scavenge filter.　·　NG　·　来源 Chair Flight B737 Question Bank

38.What condition causes the A/T LIM indication to illuminate WHITE on the upper centre display panel?

  1. The FMC is not providing the A/T system with N1 limit values ✓
  2. The Forward Thrust Levers have been advanced to the fully forward position by the A/T system.
  3. The Forward Thrust Levers have been manually advanced to the fully forward position.
  4. The A/T system is no longer sending an EGT limit values to the FMC.
正确答案：The FMC is not providing the A/T system with N1 limit values　·　NG　·　来源 Chair Flight B737 Question Bank

39.At what rotational speed is the Start Lever moved to the IDLE position?

  1. Max Motoring - 25% N2. ✓
  2. Starter cutout speed - 56% N1.
  3. Max motoring - 56% N1.
  4. Starter cutout speed - 56% N2.
正确答案：Max Motoring - 25% N2.　·　NG　·　来源 Chair Flight B737 Question Bank

40.The B737-800 has no In-Flight Abnormal Start Protection.

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

41.When GRD is selected and the eng start switch is selected to either 1 or 2, how are the crew alerted to the start valve opening?

  1. An amber START VALVE OPEN alert is displayed on the lower DU.
  2. A START VALVE OPEN alert is displayed on the upper DU. ✓
  3. The only indication is the N2 gauge increasing to Max Motoring (25%).
  4. The blue START VALVE light illuminates bright blue then goes dim blue once the start valve is fully open.
正确答案：A START VALVE OPEN alert is displayed on the upper DU.　·　NG　·　来源 Chair Flight B737 Question Bank

42.Which of the following is NOT powered by the standby Power system?

  1. AC Standby Bus
  2. Battery Bus.
  3. Static Inverter
  4. Transformer Rectifier 1. ✓
正确答案：Transformer Rectifier 1.　·　NG　·　来源 Chair Flight B737 Question Bank

43.The DC standby Bus is powered from the batteries through the static Inverter. Select one:

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

44.If all AC generated power fails, how long can the batteries (if fully charged) supply standby power?

  1. Up to 60 minutes.
  2. A minimum of 30 minutes.
  3. A minimum of 60 minutes. ✓
  4. Up to 30 minutes.
正确答案：A minimum of 60 minutes.　·　NG　·　来源 Chair Flight B737 Question Bank

45.With the BUS TRANSFER switch in the AUTO position; how do the BTBs operate?

  1. BTBs automatically maintain power to DC Bus 1 and DC Bus 2 through the DC Cross Tie Relay.
  2. BTBs isolate Transfer Bus 1 from Transfer Bus 2, if only 1 IDG is supplying power, DC Cross Tie Relay closes to connect DC Bus 1 to DC Bus 2.
  3. BTBs automatically maintain power to AC Transfer busses from any operating generator or external power. ✓
  4. BTBs isolate Transfer Bus 1 from Transfer Bus 2, if only 1 IDG is supplying power, DC Cross Tie Relay opens to isolate DC Bus 1 from DC Bus 2.
正确答案：BTBs automatically maintain power to AC Transfer busses from any operating generator or external power.　·　NG　·　来源 Chair Flight B737 Question Bank

46.The amber TR UNIT light illuminated while in-flight indicates if?

  1. TR1 and TR2 have failed, or TR3 has failed.
  2. One TR has failed.
  3. TR1 has failed, or TR2 and TR3 have failed. ✓
  4. All three TRs have failed.
正确答案：TR1 has failed, or TR2 and TR3 have failed.　·　NG　·　来源 Chair Flight B737 Question Bank

47.The amber TR UNIT light illuminated while on the ground indicates if?

  1. TR1 and TR2 have failed, or TR3 has failed.
  2. One TR has failed. ✓
  3. TR1 has failed, or TR2 and TR3 have failed.
  4. All three TRs have failed.
正确答案：One TR has failed.　·　NG　·　来源 Chair Flight B737 Question Bank

48.When external ground power is connected to the aircraft through the External AC Receptacle, the GRD POWER AVAILABLE light does not illuminate unless the power supplied meets the quality requirements of 115v AC, 200 Hz, 3 phase.

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

49.An illuminated amber ELEC light on the AC and DC Metering Panel indicates?

  1. A fault exists in the DC power system or the Standby power system ✓
  2. A fault exists in the AC power system or the DC power system
  3. A fault exists in the AC power system and the DC power system
  4. A fault exists in the DC power system and the Standby power system
正确答案：A fault exists in the DC power system or the Standby power system　·　NG　·　来源 Chair Flight B737 Question Bank

50.Why are the covers on the Drive DISCONNECT switches red?

  1. For easy identification of an emergency operation in low light conditions.
  2. To identify switch action is irreversible in flight. ✓
  3. To identify an emergency operation control switch.
  4. To identify a NNP memory item.
正确答案：To identify switch action is irreversible in flight.　·　NG　·　来源 Chair Flight B737 Question Bank

51.What is the normal source of power for the DC Standby bus?

  1. The battery
  2. DC bus 1 and DC bus 2
  3. TR1, TR2 and TR3 ✓
  4. TR2 and TR3
正确答案：TR1, TR2 and TR3　·　NG　·　来源 Chair Flight B737 Question Bank

52.What is the purpose of the Ground Service switch on the forward attendant's panel?

  1. Energises the No1 and No2 115V GND SERVICE BUS, to allow the galleys water heaters to be powered whilst the aircraft is connected to ground power.
  2. Powers and sounds external horn through the AC ground services bus to attract attention of ground servicing personnel.
  3. Provides ground power directly to the AC ground services bus for utility outlets, cabin lighting, and battery charger without powering all aircraft electrical busses. ✓
  4. Provides power to external services used by ground servicing personnel.
正确答案：Provides ground power directly to the AC ground services bus for utility outlets, cabin lighting, and battery charger without powering all aircraft electrical busses.　·　NG　·　来源 Chair Flight B737 Question Bank

53.What is the effect of selecting the Drive Disconnect switch to DISCONNECT?

  1. AC Standby Bus is immediately powered by Inverter from batteries.
  2. No effects take place until STANBY POWER switch is also moved to BAT.
  3. DRIVE light illuminates, AC electrical power is lost on associated Transfer Bus, AC Standby Bus powered from opposite Transfer Bus.
  4. IDG is disconnected if running, and DRIVE light illuminates. ✓
正确答案：IDG is disconnected if running, and DRIVE light illuminates.　·　NG　·　来源 Chair Flight B737 Question Bank

54.What is the source of power for the AC Standby bus if all AC power is lost.

  1. The TRs
  2. The Static Inverter ✓
  3. The DC Standby Bus
  4. The Battery Charger
正确答案：The Static Inverter　·　NG　·　来源 Chair Flight B737 Question Bank

55.The TR UNIT light illuminated when on the ground indicates:

  1. any two TRs have failed
  2. TR1 has failed or TR2 and TR3 have failed
  3. any TR has failed ✓
  4. All three TRs have failed
正确答案：any TR has failed　·　NG　·　来源 Chair Flight B737 Question Bank

56.The TR UNIT light illuminated when on the air indicates:

  1. any two TRs have failed
  2. TR1 has failed or TR2 and TR3 have failed ✓
  3. any TR has failed
  4. All three TRs have failed
正确答案：TR1 has failed or TR2 and TR3 have failed　·　NG　·　来源 Chair Flight B737 Question Bank

57.What is the normal source of power for the AC Standby Bus?

  1. AC Transfer Bus 1 ✓
  2. The Static Inverter
  3. Ground Service Bus 1
  4. AC Transfer Bus 2
正确答案：AC Transfer Bus 1　·　NG　·　来源 Chair Flight B737 Question Bank

58.Maintaining uninterrupted power on both AC Transfer Busses is primarily the function of:

  1. The IDGs
  2. The Ground Service Busses
  3. The Bus Tie Breakers (BTBs) ✓
  4. The Transfer Busses
正确答案：The Bus Tie Breakers (BTBs)　·　NG　·　来源 Chair Flight B737 Question Bank

59.What microphone options are available to the flight crew?

  1. Headset boom microphone, oxygen mask microphone, ceiling speakers microphone.
  2. Headset boom microphone and hand microphone.
  3. Hand microphone, headset boom microphone, oxygen mask microphone, overhead speaker microphone.
  4. Hand microphone, headset boom microphone, oxygen mask microphone. ✓
正确答案：Hand microphone, headset boom microphone, oxygen mask microphone.　·　NG　·　来源 Chair Flight B737 Question Bank

60.When the ALT-NORM switch on the Audio Control Panel (ACP) is selected to ALT, what is the result?

  1. ACP operates in a degraded mode, VHF-1 for Captain, HF-1 for Observer and VHF-2 for First Officer.
  2. ACP operates in a degraded mode, VHF-1 for Captain and Observer, VHF-2 for First Officer. ✓
  3. All communications are routed through the ACP on the AFT Overhead Panel.
  4. ACP operates in a degraded mode, VHF-2 for Captain, HF-2 for Observer, and VHF-1 for First Officer.
正确答案：ACP operates in a degraded mode, VHF-1 for Captain and Observer, VHF-2 for First Officer.　·　NG　·　来源 Chair Flight B737 Question Bank

61.Selecting the Cockpit Voice Recorder to ON has what effect?

  1. Powers the cockpit voice recorder until 5 after the last engine shutdown.
  2. Powers the cockpit voice recorder until the switch is moved to OFF
  3. Powers the cockpit voice recorder until first engine is started, then trips to AUTO. ✓
  4. Powers the cockpit voice recorder after the first engine is started until 5 minutes after last engine shutdown.
正确答案：Powers the cockpit voice recorder until first engine is started, then trips to AUTO.　·　NG　·　来源 Chair Flight B737 Question Bank

62.What is the effect of pushing the Pilot Call switch?

  1. Two-tone chime in flight deck.
  2. Two-tone chime in passenger cabin, with both pink master call lights illuminated.
  3. Single-tone chime in passenger cabin with both pink call lights illuminated.
  4. Single-tone chime in flight deck. ✓
正确答案：Single-tone chime in flight deck.　·　NG　·　来源 Chair Flight B737 Question Bank

63.What are the 3 positions For the Audio Control Panel Filter switch?

  1. V, B, R, Voice, Both, Range. ✓
  2. Pushed to select filtering ON, Pushed again for filtering OFF, rotated to increase or decrease amount of filtering.
  3. V, B, R, Voice, Both, Radio.
  4. R, G, B, Radio, Ground, Both.
正确答案：V, B, R, Voice, Both, Range.　·　NG　·　来源 Chair Flight B737 Question Bank

64.Which Statements are correct?

  1. The A/T automatically disengages approximately 2 seconds after touchdown.
  2. The A/P must be manually disengaged after touchdown.
  3. Landing roll-out is executed manually after disengaging the A/P.
  4. The A/T must be manually disengaged after touchdown.
  5. ABC ✓
正确答案：ABC　·　NG　·　来源 Chair Flight B737 Question Bank

65.What components make up the Automatic Flight System (AFS)?

  1. Flight directors, MCP mode selector system, autothrottles.
  2. Autopilot, MCP mode selector system, autothrottles.
  3. Autothrottles and autopilot flight director system. ✓
  4. AFDS, MCP mode selector system, autothrottles.
正确答案：Autothrottles and autopilot flight director system.　·　NG　·　来源 Chair Flight B737 Question Bank

66.What does an illuminated green light mean in the MCP buttons?

  1. That mode is currently engaged and active.
  2. The switch is available to be selected.
  3. That mode is currently de-selected and inactive.
  4. That switch can be de-selected. ✓
正确答案：That switch can be de-selected.　·　NG　·　来源 Chair Flight B737 Question Bank

67.If you engage Level Change by pressing the LVL CHG switch on the MCP and the green light illuminates, what other indications will occur as this mode engages?

  1. Speed window blanks, MCP SPD annunciated for pitch mode, N1 annunciated for thrust mode.
  2. Speed window blanks, MCP SPD annunciated for pitch mode, N1 or RETARD/ARM annunciated for thrust mode.
  3. Speed window opens to show target speed, MCP SPD annunciated for thrust mode, N1 annunciated for pitch mode.
  4. Speed window opens to show target speed, MCP SPD annunciated for pitch mode, N1 or RETARD/ARM annunciated for thrust mode. ✓
正确答案：Speed window opens to show target speed, MCP SPD annunciated for pitch mode, N1 or RETARD/ARM annunciated for thrust mode.　·　NG　·　来源 Chair Flight B737 Question Bank

68.What does a flashing "A" displayed to the left of the selected MCP speed indicate?

  1. Underspeed limiting, FMC speed or MCP selected speed cannot be reached. ✓
  2. limiting for maximum speed for current flap setting.
  3. Overspeeed limiting at Mmo limit
  4. Overspeed limititing at Vmo Limit
正确答案：Underspeed limiting, FMC speed or MCP selected speed cannot be reached.　·　NG　·　来源 Chair Flight B737 Question Bank

69.An altitude restriction is entered at the top of descent, the aircraft will not now follow the Idle Descent path but will descend to meet the altitude restriction. After achieving the altitude restriction which of the indicated flight paths will the aircraft follow for the rest of the decent?

  1. Descends to achieve restriction then maintains level flight until intercepts the original idle descent path. (A) ✓
  2. Descends to achieve restriction, then continues steady descent to End of Descent. (C)
  3. None of the options
  4. Descends to achieve restriction then descends at 1000 fpm until intercepting original idle descent path. (B)
正确答案：Descends to achieve restriction then maintains level flight until intercepts the original idle descent path. (A)　·　NG　·　来源 Chair Flight B737 Question Bank

70.If an altitude restriction is entered before TOD, the aircraft will commence the descent early to follow a new idle descent path to achieve the descent restriction. If ALT INTV is then selected after the descent restriction, which of the paths will the aircraft follow?

  1. Path A. Descends to achieve restriction then maintains level flight until intercepts the original idle descent path.
  2. Path C. Descends to achieve restriction, then continues steady descent to End of Descent.
  3. Path D. Descends to achieve restriction, then continues on that new idle descent path until new commands are entered.
  4. Path B. Descends to achieve restriction then descends at 1000 fpm until intercepting original idle descent path. ✓
正确答案：Path B. Descends to achieve restriction then descends at 1000 fpm until intercepting original idle descent path.　·　NG　·　来源 Chair Flight B737 Question Bank

71.With VNAV engaged, pushing the SPD INTV switch has what effect?

  1. IAS/MACH window blanks and next FMC speed restriction becomes active, magenta target speed displayed above speed tape on PFD.
  2. IAS/MACH window opens up showing current FMC target speed, and IAS/MACH selector can be used to set new desired speed. ✓
  3. Current or next speed restriction deleted from FMC, IAS/MACH window opens up showing previous FMC target speed, and IAS/MACH selector can be used to set new desired speed.
  4. No effect, VNAV remains enagaged with the FMC controlling target speed.
正确答案：IAS/MACH window opens up showing current FMC target speed, and IAS/MACH selector can be used to set new desired speed.　·　NG　·　来源 Chair Flight B737 Question Bank

72.Why do we check that FLARE mode is armed at 500 feet RA?

  1. To allow start of the flare manoeuvre at 350 feet RA.
  2. To allow APP mode to be selected at this point if FLARE not armed.
  3. To be aware that A/P will disengage at 350 feet RA if not armed. ✓
  4. To allow the second A/P to be engaged at this point.
正确答案：To be aware that A/P will disengage at 350 feet RA if not armed.　·　NG　·　来源 Chair Flight B737 Question Bank

73.What will cause the A/T to disengage?

  1. Push Either A/T Disengage switch and Move A/T ARM switch to OFF
  2. Push Either A/T Disengage switch and An A/T system fault is detected
  3. Immediately the left main landing gear is compressed, Push Either A/T Disengage switch and Move A/T ARM switch to OFF.
  4. Move A/T ARM switch to OFF, Push Either A/T Disengage switch and An A/T system fault is detected ✓
正确答案：Move A/T ARM switch to OFF, Push Either A/T Disengage switch and An A/T system fault is detected　·　NG　·　来源 Chair Flight B737 Question Bank

74.What are the indications for A/T disconnected.

  1. A/T P/RST disenage light illuminates steady.
  2. Tone sounds and A/T P/RST disengage light illuminates steady
  3. A/T P/RST disengage light flashes. ✓
  4. Tone sounds and A/T P/RST disengage light flashes
正确答案：A/T P/RST disengage light flashes.　·　NG　·　来源 Chair Flight B737 Question Bank

75.The A/T is controlled by FCC A only.

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

76.During THR HLD (Throttle Hold), if you manually move the throttle levers, the A/T will try to return them to their original position.

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

77.Which statement is correct for when the window heat Test Switch is put into the OVHT position?

  1. Simulates an overheat condition in order to test the system ✓
  2. Performs a voltage check of the power supplies.
  3. Checks for the presence of the window heat elements
  4. Can only be used if all green lights are on.
正确答案：Simulates an overheat condition in order to test the system　·　NG　·　来源 Chair Flight B737 Question Bank

78.In an emergency, the Emergency Lights and Forward Airstairs can be operated from the Aft Attendant's panel.

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

79.What is the minimum distance required to make a turn away from an obstacle to the front of the aircraft?

  1. 9.8m
  2. 5.4m
  3. 12.5m
  4. 7.4m ✓
正确答案：7.4m　·　NG　·　来源 Chair Flight B737 Question Bank

80.Where is the circuit breaker light control located?

  1. Forward overhead panel. ✓
  2. P6 and P18 panels.
  3. Aft overhead panel.
  4. Captain's and First Officer's main panel.
正确答案：Forward overhead panel.　·　NG　·　来源 Chair Flight B737 Question Bank

81.What indication is there on the Flight Deck if a correct emergency access code has been entered in the Flight Deck Door keypad?

  1. LOCK light illuminates.
  2. AUTO UNLK light illuminates
  3. Continuos cabin chime sounds.
  4. Amber light illuminates on Flight Deck Emergency Access Panel.
  5. BC ✓
正确答案：BC　·　NG　·　来源 Chair Flight B737 Question Bank

82.With the EMER EXIT LIGHTS switch in the guarded position, when would the Emergency Exit Lights automatically illuminate?

  1. When DC Bus 1 fails, or AC power is turned off. ✓
  2. Immediately. When guarded the switch is in the ON position
  3. Whenever the FASTEN SEATBELTS signs are illuminated, with the Flaps beyond Flap 15.
  4. Never. When guarded the switch is in the OFF position.
正确答案：When DC Bus 1 fails, or AC power is turned off.　·　NG　·　来源 Chair Flight B737 Question Bank

83.Which statement is correct for the No 2 windows.

  1. The No 2 Windows cannot be opened from outside the aircraft.
  2. The First Officer's No 2 window can be opened from outside the aircraft. ✓
  3. Both the Captain's and First Officer's No 2 Windows can be opened from outside the aircraft.
  4. The Captain's No 2 Window can be opened from outside the aircraft.
正确答案：The First Officer's No 2 window can be opened from outside the aircraft.　·　NG　·　来源 Chair Flight B737 Question Bank

84.How can the Emergency Exit Lights be illuminated?

  1. If the three position switch located on the FWD Overhead panel is selected to ON.
  2. Automatically if the three position switch located on the FWD Overhead panel switch is in the ARMED position and electrical power to DC bus No.1 fails or if AC power turned off.
  3. By lifting the guard and pushing the ON switch located on the Aft Attendant Panel.
  4. All answers are correct. ✓
正确答案：All answers are correct.　·　NG　·　来源 Chair Flight B737 Question Bank

85.Can the Flight Deck No2 windows be opened both on the ground and in flight?

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

86.When operating the Airstairs from outside the aircraft - moving the AIRSTAIRS switch to Extend requires both AC and DC power for the airstairs to extend.

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

87.What is the B737-800 wingspan when fitted with Winglets?

  1. 35.79m ✓
  2. 37.57m
  3. 32.18m
  4. 39.18m
正确答案：35.79m　·　NG　·　来源 Chair Flight B737 Question Bank

88.The flight deck door has one decompression panel that automatically opens during an aircraft rapid decompression, and one emergency egress panel that flight deck crew can manually remove to exit if the door is jammed.

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

89.Where is the potable water contents indicator located?

  1. Gauge located in the Water System Service Panel blow the aft right entry door.
  2. On the aft Attendant's panel. ✓
  3. On the forward Attendant's panel
  4. In the forward galley adjacent to the water heater.
正确答案：On the aft Attendant's panel.　·　NG　·　来源 Chair Flight B737 Question Bank

90.The retractable landing lights may only be extended below the following airspeed.

  1. Can be extended at ANY speed. ✓
  2. At the landing gear extension limit 270 kt.
  3. There are no retractable landing lights fitted on the B737-800.
  4. At the Flap extension limit 250 kt
正确答案：Can be extended at ANY speed.　·　NG　·　来源 Chair Flight B737 Question Bank

91.What does an amber light indicate on the Flight Deck Door Emergency Access Panel?

  1. Incorrect access code entered, after timer expires code can be entered again.
  2. Access denied by Flight Deck.
  3. Electronic door lock inoperative, deadbolt in use.
  4. Correct access code entered, if in AUTO door will unlock after timer expires. ✓
正确答案：Correct access code entered, if in AUTO door will unlock after timer expires.　·　NG　·　来源 Chair Flight B737 Question Bank

92.When operating the forward airstairs, with the external control, what position must the forward entry door be in?

  1. Must be fully open
  2. Can be in any position. ✓
  3. Must be fully closed
  4. Must be partially open
正确答案：Can be in any position.　·　NG　·　来源 Chair Flight B737 Question Bank

93.The water supply in the Lavatories can be manually selected to supply only the toilet or only the sink taps.

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

94.What is the correct method to close the Flight Deck No 2 window?

  1. Pull latch mechanism rod to unlock window. Move window forward whilst depressing trigger mechanism, turn handle forward and outboard, release trigger to lock. ✓
  2. Pull lock trigger to unlock window. Move window forward whilst depressing trigger mechanism, turn handle forward and outboard, release trigger to lock.
  3. Handle must be in the locked position. Without touching the trigger mechanism, ensure channel is clear and push window forward until trigger lock mechanism engages.
  4. Handle must be in the unlocked position. Without touching the trigger mechanism, ensure channel is clear and push window forward until trigger lock mechanism engages.
正确答案：Pull latch mechanism rod to unlock window. Move window forward whilst depressing trigger mechanism, turn handle forward and outboard, release trigger to lock.　·　NG　·　来源 Chair Flight B737 Question Bank
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