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Boeing 737 · Warnings 题库（145 题）

Boeing 737 机型「Warnings」相关知识共 145 道题。想练习或模拟考试，请到 题库 · 模拟考试。
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1.NGs only: With flap 15 selected and landing gear UP, the landing gear warning horn cannot be silenced with the HORN CUTOUT switch if

  1. Both thrust levers are below approx 30 degrees
  2. Either thrust lever is below 20 degrees or an engine not running and the other thrust lever is less than 34 degrees. ✓
  3. Either thrust lever is below 10 degrees or an engine not running and the other thrust lever is less than 30 degrees.
正确答案：Either thrust lever is below 20 degrees or an engine not running and the other thrust lever is less than 34 degrees.　·　737　·　来源 b737.org.uk

2.Classics: The Take-off configuration warning is armed when on the ground and either or both Forward Thrust levers are advanced for takeoff. The Take-off warning horn sounds when

  1. Stab trim is NOT in the green band range, or the trailing edge flaps are NOT in the Flaps 1 through 15 take-off range, or the Parking Brake is NOT set.
  2. Stab trim is in the green band range, or the trailing edge flaps are in the Flaps 1 through 15 take-off range, or the leading edge SLATS are not in the correct position for take-off or the speed brake is NOT in the DOWN position or the Parking Brake is set.
  3. Stab trim is NOT in the green band range, or the trailing edge flaps are NOT in the Flaps 1 through 15 take-off range, or the leading edge FLAPS are NOT in the correct position for take-off or the speed brake is NOT in the DOWN position or the Parking Brake is set. ✓
正确答案：Stab trim is NOT in the green band range, or the trailing edge flaps are NOT in the Flaps 1 through 15 take-off range, or the leading edge FLAPS are NOT in the correct position for take-off or the speed brake is NOT in the DOWN position or the Parking Brake is set.　·　737　·　来源 b737.org.uk

3.Classics: The landing gear warning horn will sound if either or both thrust levers are approximately in the idle position and the flaps are in the

  1. 1 through 10 position. ✓
  2. Up position.
  3. Up through 40 position provided the aircraft in not on the ground.
正确答案：1 through 10 position.　·　737　·　来源 b737.org.uk

4.Classics: The landing gear warning horn cannot be silenced by the Horn Cut-Out switch, regardless of Forward Thrust lever position, when the flaps are

  1. In the 15 position or greater than the 15 position.
  2. In the 15 position.
  3. Greater than the 15 position. ✓
正确答案：Greater than the 15 position.　·　737　·　来源 b737.org.uk

5.The Mach/Airspeed Aural Warning will sound when the Mach number or IAS exceeds

  1. 0.82M or 340 Knots whichever is reached first. ✓
  2. 0.84M above 24,000 feet or 340 knots below 24,000 feet whichever is reached first.
  3. 0.84M or 320 Knots whichever is reached first.
正确答案：0.82M or 340 Knots whichever is reached first.　·　737　·　来源 b737.org.uk

6.The Proximity Switch Electronic Unit (PSEU) light illuminates

  1. If an overwing exit flight lock fails to disengage when commanded at any time.
  2. If a fault is detected in the PSEU at any time.
  3. Is inhibited from thrust lever advance for take-off until 30 seconds after landing. ✓
正确答案：Is inhibited from thrust lever advance for take-off until 30 seconds after landing.　·　737　·　来源 b737.org.uk

7.EGPWS terrain display changes from dotted to solid yellow

  1. 30 - 60 seconds from impact.
  2. 40 - 60 seconds from impact. ✓
  3. 20 - 30 seconds from impact.
正确答案：40 - 60 seconds from impact.　·　737　·　来源 b737.org.uk

8.The 737 NG weather radar Windshear mode will automatically be turned on under the following specific aircraft conditions:

  1. In the air below - 1800 ft. AGL or on the ground - typically with the engines at Take-Off Thrust Setting or both Oil Pressures Active and the Transponder On
  2. In the air below - 1200 ft. AGL or on the ground - typically with the engines at Take-Off Thrust Setting or both Oil Pressures Active and the Transponder On
  3. In the air below - 2300 ft. AGL or on the ground - typically with the engines at Take-Off Thrust Setting or both Oil Pressures Active and the Transponder On ✓
正确答案：In the air below - 2300 ft. AGL or on the ground - typically with the engines at Take-Off Thrust Setting or both Oil Pressures Active and the Transponder On　·　737　·　来源 b737.org.uk

9.With both engines operating and one forward thrust lever set below approximately 20 degrees thrust lever angle, the landing gear warning horn can be silenced with the landing gear warning HORN CUTOUT switch:

  1. It cannot be silenced if the thrust lever angle is less than 20 degrees.
  2. With flaps UP through 10 if below 800 feet RA and above 200 feet RA. ✓
  3. With flaps UP through 25 if below 800 feet RA and above 200 feet RA.
  4. With flaps UP through 10 if below 800 feet RA and above 300 feet RA.
正确答案：With flaps UP through 10 if below 800 feet RA and above 200 feet RA.　·　MAX　·　来源 smartcockpit.com

10.Which two displays cannot be selected and shown simultaneously on the Navigation DU?

  1. Terrain and TCAS.
  2. Weather and Data.
  3. Weather and Terrain. ✓
  4. TCAS and Airport.
正确答案：Weather and Terrain.　·　MAX　·　来源 smartcockpit.com

11.Terrain ahead of the airplane may exceed available climb performance. A ground proximity alert does not guarantee terrain clearance.

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

12.Once an alert has occurred for deviating from the selected altitude, how is it cancelled?

  1. Return to within 300 feet of selected altitude or deviate by more than 900 feet from selected altitude, or select a new altitude. ✓
  2. Return to within 200 feet of selected altitude.
  3. Return to within 200 feet of selected altitude and press the HORN CUTOUT button on the Control Stand.
  4. Press ALT INT to select next FMC target altitude.
正确答案：Return to within 300 feet of selected altitude or deviate by more than 900 feet from selected altitude, or select a new altitude.　·　MAX　·　来源 smartcockpit.com

13.When testing the Mach-Airspeed warning system in flight, the No1 and No2 systems must be tested separately to identify that the clacker sounds for both systems independently.

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

14.What is correct about the color on the terrain display?

  1. Dotted green - terrain 2500 feet below up to 500 feet below. ✓
  2. Dotted amber - terrain 2000 feet below up to 500 feet below.
  3. Dotted red - terrain more than 5000 feet above the aircraft.
  4. Solid red - look ahead terrain warning is active.
正确答案：Dotted green - terrain 2500 feet below up to 500 feet below.　·　MAX　·　来源 smartcockpit.com

15.The GPWS provides a 'BANK ANGLE' warning when the roll rate exceeds 25 degrees, 30 degrees, and 35 degrees.

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

16.When performance is limited, such as with an inoperative engine, to prevent receiving RAs beyond the airplane's capabilities:

  1. Select ALT OFF. ✓
  2. Select TCAS OFF.
  3. Select TA/RA.
  4. Select TA.
正确答案：Select ALT OFF.　·　MAX　·　来源 smartcockpit.com

17.Altitude alerting occurs when approaching or departing from the MCP selected altitude. When is the altitude alerting system inhibited?

  1. Leading edge flaps are extended to 25 or greater.
  2. Glide slope is captured, or trailing edge flaps are extended to 25 or greater. ✓
  3. Landing gear is down and locked.
  4. Leading edge flaps are extended to 25 or greater and the landing gear is extended.
正确答案：Glide slope is captured, or trailing edge flaps are extended to 25 or greater.　·　MAX　·　来源 smartcockpit.com

18.What does the TCAS Symbol that is a solid amber circle indicate?

  1. Results in aural alert of 'TRAFFIC, TRAFFIC' when within 6nm with 1200 feet or less of vertical seperation of other traffic.
  2. Advises that the proximate traffic is descending at more than 500 fpm.
  3. Advises of traffic with potential impact on 25 seconds.
  4. Advises of traffic with potential impact in 40 seconds. ✓
正确答案：Advises of traffic with potential impact in 40 seconds.　·　MAX　·　来源 smartcockpit.com

19.When will the landing gear config warning horn give an intermittent warning sound?

  1. Flaps up through 10, below 800 feet RA, either forward thrust lever at 20 degrees or less (or less than 34 degrees if only 1 engine running).rn
  2. Never. ✓
  3. Flaps greater than 25, below 800 feet RA, regardless of forward thrust lever position.
  4. Flaps 1 through 10, below 800 feet RA, either forward thrust lever at 20 degrees or less (or less than 34 degrees if only 1 engine running).
正确答案：Never.　·　MAX　·　来源 smartcockpit.com

20.While flying an ILS approach below 1, 000 feet Radio Altitude, a BELOW G/S alert occurs. To cancel the alert:

  1. Press RECALL.
  2. Push either pilot's BELOW GS P-INHIBIT light, or correct the flight path back to the glide slope. ✓
  3. The alert cannot be cancelled.
  4. Select another mode on MCP.
正确答案：Push either pilot's BELOW GS P-INHIBIT light, or correct the flight path back to the glide slope.　·　MAX　·　来源 smartcockpit.com

21.When are the GPWS windshear warnings available?

  1. Below 1500 feet AGL. ✓
  2. Below 2500 feet AGL.
  3. Below 3000 feet AGL.
  4. Below 5000 feet AGL.
正确答案：Below 1500 feet AGL.　·　MAX　·　来源 smartcockpit.com

22.How far from projected impact will the 'TERRAIN, TERRAIN, PULL UP' aural warning be given?

  1. Whenever descending below unsafe RA while too far from any airport in the terrain database.
  2. 1.2 nm to 1.5 nm.
  3. 20 to 30 seconds. ✓
  4. 1.2nm to 1.5nm or 20 to 30 seconds whichever limit occurs first.
正确答案：20 to 30 seconds.　·　MAX　·　来源 smartcockpit.com

23.The Ground Proximity Warning System Test:

  1. Can be performed only on the ground.
  2. Is inhibited from liftoff to 1,000 feet Radio Altitude. ✓
  3. Can be performed only above 1,000 feet Radio Altitude.
  4. Can be performed anytime.
正确答案：Is inhibited from liftoff to 1,000 feet Radio Altitude.　·　MAX　·　来源 smartcockpit.com

24.The MAINT light:

  1. Is never inhibited.
  2. Is inhibited from 80 kt until 30 seconds after landing.
  3. Is inhibited from engine start until 30 seconds after landing. ✓
正确答案：Is inhibited from engine start until 30 seconds after landing.　·　MAX　·　来源 smartcockpit.com

25.The RA aural alert 'CLIMB CLIMB NOW' means:

  1. Increase climb rate from initial pitch attitude.
  2. Climb at displayed pitch. Airplane climbs through traffic's altitude.
  3. Climb at the displayed pitch.
  4. Reversal maneuver from initial descent RA. ✓
正确答案：Reversal maneuver from initial descent RA.　·　MAX　·　来源 smartcockpit.com

26.The Stall Warning requirement is determined by what system component?rn rn rn rn

  1. A single stall management configuration computer.
  2. Two independent SMYD Computers. ✓
  3. The Captain's or F/O's Alpha Vane.
  4. Two independent ADIRUs.
正确答案：Two independent SMYD Computers.　·　MAX　·　来源 smartcockpit.com

27.Hydraulic pressure is removed from the landing gear system by the PSEU _____ after all gear are up and locked.

  1. 10 seconds. ✓
  2. 20 seconds.
  3. 30 seconds.
正确答案：10 seconds.　·　MAX　·　来源 smartcockpit.com

28.Pushing the ground proximity BELOW G/S P-INHIBIT light cancels or inhibits the alert when below 1,000 feet RA.

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

29.The Cabin Altitude and Takeoff Configuration Warnings use the same intermittent tone when activated.

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

30.The terrain displayed in the Look-Ahead Terrain Alerting system is generated from:

  1. Weather Radar correlated with IRS position.
  2. GPWS nav database correlated with IRS position.
  3. GPWS nav database correlated with GPS position. ✓
  4. FMC nav database correlated with GPS position.rn
正确答案：GPWS nav database correlated with GPS position.　·　MAX　·　来源 smartcockpit.com

31.How are crew alerted to a deviation from the selected altitude?

  1. A warning tone sounds once deviation is 300 feet from selected altitude, the current altitude box turns red and begins to flash.
  2. A warning tone sounds once deviation is 300 feet from selected altitude, the current altitude box turns amber and begins to flash. ✓
  3. A warning tone sounds once deviation is 900 feet from selected altitude, the current altitude box turns red and begins to flash.
  4. A warning tone sounds once deviation is 300 feet from selected altitude, the current altitude box begins to flash.
正确答案：A warning tone sounds once deviation is 300 feet from selected altitude, the current altitude box turns amber and begins to flash.　·　MAX　·　来源 smartcockpit.com

32.The predictive windshear aural alerts will be heard through flightdeck speakers and the headsets at a pre-set volume. They cannot be controlled or turned off by the crew.

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

33.When configured for landing, the GPWS will NOT alert if attempting an off-airport landing.

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

34.The Look-Ahead Terrain alerting system will show for terrain:

  1. Within 2,000 feet RA.
  2. Below 1,000 feet barometric altitude.
  3. Above 1,000 feet RA.
  4. Within 2,000 feet barometric altitude. ✓
正确答案：Within 2,000 feet barometric altitude.　·　MAX　·　来源 smartcockpit.com

35.All TCAS alerts are inhibited:

  1. Below approximately 500 feet radio altitude.
  2. By GPWS and windshear warnings. ✓
  3. Below approximately 1,100 feet radio altitude.
  4. Until the flaps are fully retracted after takeoff.
正确答案：By GPWS and windshear warnings.　·　MAX　·　来源 smartcockpit.com

36.RAs are indicated by one or more aural listed in the RA aural table. The TRAFFIC annunciation and RA symbol which depicts the traffic's relative bearing, range, altitude, and vertical motion are on the navigation display similar to the TA symbol.

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

37.The stall warning test can only be carried out on the ground, the No1 and No2 systems must be carried out separately to ensure the clacker sounds when each system is tested.

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

38.In what mode will the TCAS automatically show if a TA/RA occurs and the TFC switches are selected OFF.

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

39.The EGPWS displays terrain within 2,500 feet of the aircraft barometric altitude on the Navigation display.

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

40.At what altitude (in feet) do the RA callouts begin?

  1. Fifteen hundred.
  2. Two thousand.
  3. One thousand.
  4. Twenty five hundred. ✓
正确答案：Twenty five hundred.　·　MAX　·　来源 smartcockpit.com

41.TCAS TEST is displayed on the navigation display during the test followed by TCAS TEST PASSED or TCAS TEST FAILED. This test remains in view for _____ then blanks. An aural annunciation sounds at the completion of the test.

  1. 3 seconds.
  2. 5 seconds.
  3. 8 seconds. ✓
  4. 10 seconds.
正确答案：8 seconds.　·　MAX　·　来源 smartcockpit.com

42.Takeoff configuration warning is armed when the airplane is on the ground and either or both forward thrust levers are advanced for takeoff.

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

43.All TCAS voice annunciations are inhibited below approximately:

  1. 500 feet radio altitude. ✓
  2. 300 feet radio altitude.
  3. 50 feet radio altitude.
  4. 100 feet radio altitude.
正确答案：500 feet radio altitude.　·　MAX　·　来源 smartcockpit.com

44.The TCAS symbol for proximate traffic is:

  1. A red square.
  2. An amber circle.
  3. A white solid diamond. ✓
  4. A white hollow diamond
正确答案：A white solid diamond.　·　MAX　·　来源 smartcockpit.com

45.Which statement is correct?

  1. When the RHS pilot omits to set the minima on the baro, but the LHS pilot sets the minima correctly, there will be no GPWS minimums callouts.
  2. When the RHS pilot omits to set the minima on the baro, but the LHS pilot sets the minima correctly, there will be a GPWS minimums callouts, since the callouts are based on the captains minimums selector. ✓
  3. It is impossible to omit to set the minima before any approach, because the aircraft GPWS will remind you in time.
  4. There is no correct statement.
正确答案：When the RHS pilot omits to set the minima on the baro, but the LHS pilot sets the minima correctly, there will be a GPWS minimums callouts, since the callouts are based on the captains minimums selector.　·　MAX　·　来源 smartcockpit.com

46.Serviceability of the tailskid cartridge is shown by:

  1. A green decal.
  2. A green indicator light.
  3. Wear dimples.
  4. A green and red decal. ✓
正确答案：A green and red decal.　·　MAX　·　来源 smartcockpit.com

47.What is the first Radio Altitude Callout given during the approach?

  1. 2500 feet - 'Twenty Five Hundred'. ✓
  2. 1000 feet - 'One Thousand'.
  3. 2000 feet - 'Two thousand'.
  4. 50 feet - 'Fifty'.
正确答案：2500 feet - 'Twenty Five Hundred'.　·　MAX　·　来源 smartcockpit.com

48.The PSEU light will illuminate along with a Master Caution and an OVERHEAD annunciator light, under which of the following situations?

  1. Illuminates as soon as the ground/air system senses ground mode, if an emergency exit flight lock has failed locked or a fault is detected.
  2. Illuminates 30 seconds after the ground/air system senses ground mode, if an emergency exit flight lock has failed locked or a fault is detected. ✓
  3. Illuminates 30 seconds after the ground/air system senses air mode, if an emergency exit flight lock has failed locked or a fault is detected.
  4. Illuminates whenever ground/air system senses air mode, and an emergency exit flight lock has failed locke
正确答案：Illuminates 30 seconds after the ground/air system senses ground mode, if an emergency exit flight lock has failed locked or a fault is detected.　·　MAX　·　来源 smartcockpit.com

49.The Stall Warning System Stick Shaker can be tested by pressing the STALL WARNING TEST buttons on the AFT overhead panel. Pressing No1 switch will activate the Captain's Stick Shaker and the Captain's column will vibrate. Pressing N02 switch will activate the FO's Stick Shaker and the FO's column will vibrate.

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

50.The Predictive Windshear alerts are issued:

  1. When TERR switch on EFIS control panel is pressed.
  2. When WPT switch on EFIS control panel is pressed.
  3. Automatically below 1, 200 feet RA. ✓
  4. Automatically below 2, 500 feet RA.
正确答案：Automatically below 1, 200 feet RA.　·　MAX　·　来源 smartcockpit.com

51.The windshear warning mode of the GPWS has priority over all other GPWS modes.

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

52.Predictive windshear alerts are triggered from the:

  1. EGPWS.
  2. Weather Radar System. ✓
  3. Aural Warning Module.
  4. EGPWS and the Aural Warning Module.
正确答案：Weather Radar System.　·　MAX　·　来源 smartcockpit.com

53.Which of the following is NOT a GPWS mode?

  1. Excessive descent rate.
  2. Excessive terrain closure.
  3. Unsafe terrain clearance when in the landing configuration. ✓
  4. Windshear.
正确答案：Unsafe terrain clearance when in the landing configuration.　·　MAX　·　来源 smartcockpit.com

54.Which systems does the Proximity Switch Electronic Unit (PSEU) monitor?

  1. Takeoff-Landing Configuration Warnings, Landing Gear and Air-Ground sensing. ✓
  2. Takeoff-Landing Configuration Warnings, Landing Gear and Anti-Skid
  3. Air-Ground sensing, Landing Gear and Air/Ground sensing.
  4. Air-Ground sensing, Landing Gear and Anti-Skid.
正确答案：Takeoff-Landing Configuration Warnings, Landing Gear and Air-Ground sensing.　·　MAX　·　来源 smartcockpit.com

55.As well as providing outputs for all stall warnings, the SMYD computers also provide outputs for GPWS Windshear Detection and Alert.

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

56.Which of the following statements is true for the CABIN ALTITUDE Warning?

  1. An intermittent warning horn sounds and the red CABIN ALTITUDE lights illuminate when the cabin altitude exceeds 10000 feet. ✓
  2. An intermittent warning horn sounds and the amber CABIN ALTITUDE warning lights illuminate when the cabin altitude exceeds 10000 feet.
  3. A steady warning horn sounds and the amber CABIN ALTITUDE lights illuminate when the cabin altitude exceeds 14000 feet.
  4. A steady warning horn sounds and the red CABIN ALTITUDE warning lights illuminate when the cabin altitude exceeds 14000 feet.
正确答案：An intermittent warning horn sounds and the red CABIN ALTITUDE lights illuminate when the cabin altitude exceeds 10000 feet.　·　MAX　·　来源 smartcockpit.com

57.On takeoff the config warning sounds. What can be the cause?

  1. Trailing edge flaps set to 2.
  2. Trailing edge flaps are in a skew condition. ✓
  3. Stabilizer set in the takeoff range.
  4. Takeoff power not set on both engines.
正确答案：Trailing edge flaps are in a skew condition.　·　MAX　·　来源 smartcockpit.com

58.The TCAS system generates a Traffic Advisory, whenever another aircraft is what distance from point of closest approach?

  1. 40 seconds. ✓
  2. Less than 6 nm separation with less than 1200 feet vertical separation.
  3. More than 6 nm separation with more than 1200 feet vertical separation.
  4. 25 seconds.
正确答案：40 seconds.　·　MAX　·　来源 smartcockpit.com

59.What is significant about the layout of the Annunciator Panel lights?

  1. The lights on the Captain's side show the systems that the Captain is responsible for monitoring, and the lights of the F/Os side show the systems the F/O is responsible for monitoring.
  2. The lights are arranged in order of priority to be dealt with in case of multiple system failures.
  3. The lights are arranged to reflect the position of the systems panels on the Overhead Panels. ✓
  4. The lights are arranged in no significant order.
正确答案：The lights are arranged to reflect the position of the systems panels on the Overhead Panels.　·　MAX　·　来源 smartcockpit.com

60.When carrying out the Stall Warning Test, which of the following statements is correct?

  1. The test cannot be completed until the DC Busses have been powered for up to 4 minutes.
  2. The test can be completed once AC power is available.
  3. The test cannot be completed until the AC Transfer Busses have been powered for up to 4 minutes. ✓
  4. The test can be completed on DC power.
正确答案：The test cannot be completed until the AC Transfer Busses have been powered for up to 4 minutes.　·　MAX　·　来源 smartcockpit.com

61.What is true about the MAINT light?

  1. It replaces the PSEU light that is available on the Boeing 737NG. ✓
  2. It is a customer option on the B737 MAX.
  3. It is in addition to the PSEU light.
正确答案：It replaces the PSEU light that is available on the Boeing 737NG.　·　MAX　·　来源 smartcockpit.com

62.The EGPWS contains a terrain database, which it uses for look-ahead terrain alerting. Which of the following statements is correct for this terrain database?

  1. All EGPWS terrain databases account for man-made obstructions over 100 feet high, in the more detailed areas of the database near major airports.
  2. Man-made obstructions are not accounted for in all EGPWS terrain databases ✓
  3. All man-made obstructions are accounted for in the detailed areas of the EGPWS terrain database in areas close to major airports.
  4. All EGPWS terrain databases account for man-made obstructions over 100 feet high, throughout the whole database area.
正确答案：Man-made obstructions are not accounted for in all EGPWS terrain databases　·　MAX　·　来源 smartcockpit.com

63.A TA symbol showing on the ND has, alongside it, a down arrow and '-07'. What does it mean?

  1. The traffic is descending at 700fpm. ✓
  2. You should descend at 700fpm.
  3. The traffic is descending at minimum 500fpm.
  4. You should descend at minimum 500fpm.
正确答案：The traffic is descending at 700fpm.　·　MAX　·　来源 smartcockpit.com

64.Altitude alerting, consisting of a tone and highlighted boxes, occurs at a set distance before reaching the selected attitude. How many feet before the selected altitude do the altitude alert highlighted boxes no longer show?

  1. 600 feet.
  2. 1000 feet to go.
  3. 300 feet. ✓
  4. 900 feet.
正确答案：300 feet.　·　MAX　·　来源 smartcockpit.com

65.When is a traffic advisory issued?

  1. When the other aircraft is within 20 NM
  2. When the aircraft is within 20 seconds of the closest approach.
  3. When the other aircraft is within 40 NM.
  4. When the aircraft is within 40 seconds of the closest approach. ✓
正确答案：When the aircraft is within 40 seconds of the closest approach.　·　MAX　·　来源 smartcockpit.com

66.RAs can only be generated if the other airplane has a working:

  1. Mode A transponder.
  2. Mode C transponder. ✓
  3. Mode S transponder.
  4. TCAS system. rn
正确答案：Mode C transponder.　·　MAX　·　来源 smartcockpit.com

67.At what altitude are the TCAS INCREASE DESCENT RAs inhibited?

  1. 1,100 feet RA.
  2. 1500 feet AGL.
  3. 1,100 feet AGL.
  4. 1500 feet RA. ✓
正确答案：1500 feet RA.　·　MAX　·　来源 smartcockpit.com

68.How can the Fire Warning Bell be silenced on the flight deck?

  1. Fire bell can only be silenced by pressing either master fire warn light.
  2. Push the master fire warn lights, press the horn cutout of the APU ground control panel, push fire warning bell cutout switch.
  3. Push the Master Fire Warn lights, press the Horn Cutout of the APU Ground Control Panel.
  4. Push the master fire warn lights, push fire warning bell cutout switch. ✓
正确答案：Push the master fire warn lights, push fire warning bell cutout switch.　·　MAX　·　来源 smartcockpit.com

69.The GPWS will provide an aural alert of 'BANK ANGLE, BANK ANGLE' under which of the following circumstances?

  1. Whenever trailing edge flaps are at 1 or greater and roll angle exceeds 35 degrees.
  2. When roll angle exceeds the maximum of 45 degrees.
  3. When roll angle exceeding 35, 40 and 45 degrees. ✓
  4. Whenever the bank angle exceeds the setting on the Bank Angle Selector.
正确答案：When roll angle exceeding 35, 40 and 45 degrees.　·　MAX　·　来源 smartcockpit.com

70.The predictive windshear symbol radials, which extend from the predictive winsdshear symbol to help identify the location of a windshear event, are displayed in what colours?

  1. Amber. ✓
  2. Red.
  3. Displayed amber when a predictive winshear caution is active, and displayed red when a predictive windshear warning is active.
  4. Red and Black banded.
正确答案：Amber.　·　MAX　·　来源 smartcockpit.com

71.Crew are warned of exceeding the maximum allowed airspeed by which of the following?

  1. Aural Clacker, speedtape red and black band, speedtape amber band, stick shaker.
  2. Aural Clacker, speedtape red and black band. ✓
  3. Aural Clacker, speedtape red and black band, stick shaker.
  4. Aural Clacker.
正确答案：Aural Clacker, speedtape red and black band.　·　MAX　·　来源 smartcockpit.com

72.Which of the following will cause activation of the takeoff configuration warning system?

  1. Leading edge flaps in the extend position and trailing edge flaps at flaps 5.
  2. Leading edge flpas in the full extend position and trailing edge flaps at 15.
  3. Spoilers partially extended. ✓
  4. SPEED BRAKE lever in the DOWN position.
正确答案：Spoilers partially extended.　·　MAX　·　来源 smartcockpit.com

73.On airplanes with Airspeed Low aural, an alert 'AIRSPEED LOW, AIRSPEED LOW' provides the flight crew with low airspeed awareness. The aural annunciates when the current airspeed decreases into the minimum maneuver speed amber bar.

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

74.In the event of an over rotation, which part of the tailskid structure contacts the runway?

  1. The skirt.
  2. The fairing.
  3. The shoe. ✓
  4. The cartridge.
正确答案：The shoe.　·　MAX　·　来源 smartcockpit.com

75.Vertical motion information is indicated by an arrow depicting a climb or descent if a change of greater than _____ is detected.

  1. 250 feet per minute.
  2. 500 feet per minute. ✓
  3. 750 feet per minute.
  4. 800 feet per minute.
正确答案：500 feet per minute.　·　MAX　·　来源 smartcockpit.com

76.The predictive windshear aural alerts will be heard through flightdeck speakers and the headsets at a pre-set volume. They cannot be controlled or turned off by the crew.

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

77.Terrain ahead of the airplane may exceed available climb performance. A ground proximity alert does not guarantee terrain clearance.

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

78.On airplanes with Airspeed Low aural, an alert 'AIRSPEED LOW, AIRSPEED LOW' provides the flight crew with low airspeed awareness. The aural annunciates when the current airspeed decreases into the minimum maneuver speed amber bar.

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

79.When are the GPWS windshear warnings available?

  1. Below 1500 feet AGL. ✓
  2. Below 2500 feet AGL.
  3. Below 3000 feet AGL.
  4. Below 5000 feet AGL.
正确答案：Below 1500 feet AGL.　·　NG　·　来源 smartcockpit.com

80.Serviceability of the tailskid cartridge is shown by:

  1. A green decal.
  2. A green indicator light.
  3. Wear dimples.
  4. A green and red decal. ✓
正确答案：A green and red decal.　·　NG　·　来源 smartcockpit.com

81.The EGPWS displays terrain within 2,500 feet of the aircraft barometric altitude on the Navigation display.

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

82.The windshear warning mode of the GPWS has priority over all other GPWS modes.

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

83.All TCAS voice annunciations are inhibited below approximately:

  1. 500 feet radio altitude. ✓
  2. 300 feet radio altitude.
  3. 50 feet radio altitude.
  4. 100 feet radio altitude.
正确答案：500 feet radio altitude.　·　NG　·　来源 smartcockpit.com

84.The stall warning test can only be carried out on the ground, the No1 and No2 systems must be carried out separately to ensure the clacker sounds when each system is tested.

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

85.What does the TCAS Symbol that is a solid amber circle indicate?

  1. Results in aural alert of 'TRAFFIC, TRAFFIC' when within 6nm with 1200 feet or less of vertical seperation of other traffic.
  2. Advises that the proximate traffic is descending at more than 500 fpm.
  3. Advises of traffic with potential impact on 25 seconds.
  4. Advises of traffic with potential impact in 40 seconds. ✓
正确答案：Advises of traffic with potential impact in 40 seconds.　·　NG　·　来源 smartcockpit.com

86.RAs are indicated by one or more aural listed in the RA aural table. The TRAFFIC annunciation and RA symbol which depicts the traffic’s relative bearing, range, altitude, and vertical motion are on the navigation display similar to the TA symbol.

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

87.At what altitude are the TCAS INCREASE DESCENT RAs inhibited?

  1. 1,100 feet RA.
  2. 1500 feet AGL.
  3. 1,100 feet AGL.
  4. 1500 feet RA. ✓
正确答案：1500 feet RA.　·　NG　·　来源 smartcockpit.com

88.Pushing the ground proximity BELOW G/S P-INHIBIT light cancels or inhibits the alert when below 1,000 feet RA.

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

89.Which of the following is NOT a GPWS mode?

  1. Excessive descent rate.
  2. Excessive terrain closure.
  3. Unsafe terrain clearance when in the landing configuration. ✓
  4. Windshear.
正确答案：Unsafe terrain clearance when in the landing configuration.　·　NG　·　来源 smartcockpit.com

90.The RA aural alert 'CLIMB - CLIMB NOW' means:

  1. Increase climb rate from initial pitch attitude.
  2. Climb at displayed pitch. Airplane climbs through traffic’s altitude.
  3. Climb at the displayed pitch.
  4. Reversal maneuver from initial descent RA. ✓
正确答案：Reversal maneuver from initial descent RA.　·　NG　·　来源 smartcockpit.com

91.The Look-Ahead Terrain alerting system will show for terrain:

  1. Within 2,000 feet RA.
  2. Below 1,000 feet barometric altitude.
  3. Above 1,000 feet RA.
  4. Within 2,000 feet barometric altitude. ✓
正确答案：Within 2,000 feet barometric altitude.　·　NG　·　来源 smartcockpit.com

92.Crew are warned of exceeding the maximum allowed airspeed by which of the following?

  1. Aural Clacker, speedtape red and black band, speedtape amber band, stick shaker.
  2. Aural Clacker, speedtape red and black band. ✓
  3. Aural Clacker, speedtape red and black band, stick shaker.
  4. Aural Clacker.
正确答案：Aural Clacker, speedtape red and black band.　·　NG　·　来源 smartcockpit.com

93.When carrying out the Stall Warning Test, which of the following statements is correct?

  1. The test cannot be completed until the DC Busses have been powered for up to 4 minutes.
  2. The test can be completed once AC power is available.
  3. The test cannot be completed until the AC Transfer Busses have been powered for up to 4 minutes. ✓
  4. The test can be completed on DC power.
正确答案：The test cannot be completed until the AC Transfer Busses have been powered for up to 4 minutes.　·　NG　·　来源 smartcockpit.com

94.In the event of an over rotation, which part of the tailskid structure contacts the runway?

  1. The skirt.
  2. The fairing.
  3. The shoe. ✓
  4. The cartridge.
正确答案：The shoe.　·　NG　·　来源 smartcockpit.com

95.The EGPWS contains a terrain database, which it uses for look-ahead terrain alerting. Which of the following statements is correct for this terrain database?

  1. All EGPWS terrain databases account for man-made obstructions over 100 feet high, in the more detailed areas of the database near major airports.
  2. Man-made obstructions are not accounted for in all EGPWS terrain databases ✓
  3. All man-made obstructions are accounted for in the detailed areas of the EGPWS terrain database in areas close to major airports.
  4. All EGPWS terrain databases account for man-made obstructions over 100 feet high, throughout the whole database area.
正确答案：Man-made obstructions are not accounted for in all EGPWS terrain databases　·　NG　·　来源 smartcockpit.com

96.In what mode will the TCAS automatically show if a TA/RA occurs and the TFC switches are selected OFF.

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

97.The Predictive Windshear alerts are issued:

  1. When TERR switch on EFIS control panel is pressed.
  2. When WPT switch on EFIS control panel is pressed.
  3. Automatically below 1, 200 feet RA. ✓
  4. Automatically below 2, 500 feet RA.
正确答案：Automatically below 1, 200 feet RA.　·　NG　·　来源 smartcockpit.com

98.When configured for landing, the GPWS will NOT alert if attempting an off-airport landing.

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

99.TCAS TEST is displayed on the navigation display during the test followed by TCAS TEST PASSED or TCAS TEST FAILED. This test remains in view for _____ then blanks. An aural annunciation sounds at the completion of the test.

  1. 3 seconds.
  2. 5 seconds.
  3. 8 seconds. ✓
  4. 10 seconds.
正确答案：8 seconds.　·　NG　·　来源 smartcockpit.com

100.How far from projected impact will the 'TERRAIN, TERRAIN, PULL UP' aural warning be given?

  1. Whenever descending below unsafe RA while too far from any airport in the terrain database.
  2. 1.2 nm to 1.5 nm.
  3. 20 to 30 seconds. ✓
  4. 1.2nm to 1.5nm or 20 to 30 seconds whichever limit occurs first.
正确答案：20 to 30 seconds.　·　NG　·　来源 smartcockpit.com

101.On takeoff the config warning sounds. What can be the cause?

  1. Trailing edge flaps set to 2.
  2. Trailing edge flaps are in a skew condition. ✓
  3. Stabilizer set in the takeoff range.
  4. Takeoff power not set on both engines.
正确答案：Trailing edge flaps are in a skew condition.　·　NG　·　来源 smartcockpit.com

102.Predictive windshear alerts are triggered from the:

  1. EGPWS.
  2. Weather Radar System. ✓
  3. Aural Warning Module.
  4. EGPWS and the Aural Warning Module.
正确答案：Weather Radar System.　·　NG　·　来源 smartcockpit.com

103.The PSEU light will illuminate along with a Master Caution and an OVERHEAD annunciator light, under which of the following situations?

  1. Illuminates as soon as the ground/air system senses ground mode, if an emergency exit flight lock has failed locked or a fault is detected.
  2. Illuminates 30 seconds after the ground/air system senses ground mode, if an emergency exit flight lock has failed locked or a fault is detected. ✓
  3. Illuminates 30 seconds after the ground/air system senses air mode, if an emergency exit flight lock has failed locked or a fault is detected.
  4. Illuminates whenever ground/air system senses air mode, and an emergency exit flight lock has failed locke
正确答案：Illuminates 30 seconds after the ground/air system senses ground mode, if an emergency exit flight lock has failed locked or a fault is detected.　·　NG　·　来源 smartcockpit.com

104.Illumination of the PSEU light on the aft overhead panel will activate the MASTER CAUTION system.

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

105.The TCAS symbol for proximate traffic is:

  1. A red square.
  2. An amber circle.
  3. A white solid diamond. ✓
  4. A white hollow diamond
正确答案：A white solid diamond.　·　NG　·　来源 smartcockpit.com

106.What is significant about the layout of the Annunciator Panel lights.

  1. The lights on the Captain's side show the systems that the Captain is responsible for monitoring, and the lights of the F/Os side show the systems the F/O is responsible for monitoring.
  2. The lights are arranged in order of priority to be dealt with in case of multiple system failures.
  3. The lights are arranged to reflect the position of the systems panels on the Overhead Panels. ✓
  4. The lights are arranged in no significant order.
正确答案：The lights are arranged to reflect the position of the systems panels on the Overhead Panels.　·　NG　·　来源 smartcockpit.com

107.Altitude alerting, consisting of a tone and highlighted boxes, occurs at a set distance before reaching the selected attitude. How many feet before the selected altitude do the altitude alert highlighted boxes no longer show?

  1. 600 feet.
  2. 1000 feet to go.
  3. 300 feet. ✓
  4. 900 feet.
正确答案：300 feet.　·　NG　·　来源 smartcockpit.com

108.How are crew alerted to a deviation from the selected altitude?

  1. A warning tone sounds once deviation is 300 feet from selected altitude, the current altitude box turns red and begins to flash.
  2. A warning tone sounds once deviation is 300 feet from selected altitude, the current altitude box turns amber and begins to flash. ✓
  3. A warning tone sounds once deviation is 900 feet from selected altitude, the current altitude box turns red and begins to flash.
  4. A warning tone sounds once deviation is 300 feet from selected altitude, the current altitude box begins to flash.
正确答案：A warning tone sounds once deviation is 300 feet from selected altitude, the current altitude box turns amber and begins to flash.　·　NG　·　来源 smartcockpit.com

109.Once an alert has occurred for deviating from the selected altitude, how is it cancelled?

  1. Return to within 300 feet of selected altitude or deviate by more than 900 feet from selected altitude, or select a new altitude. ✓
  2. Return to within 200 feet of selected altitude.
  3. Return to within 200 feet of selected altitude and press the HORN CUTOUT button on the Control Stand.
  4. Press ALT INT to select next FMC target altitude.
正确答案：Return to within 300 feet of selected altitude or deviate by more than 900 feet from selected altitude, or select a new altitude.　·　NG　·　来源 smartcockpit.com

110.Which systems does the Proximity Switch Electronic Unit (PSEU) monitor

  1. Takeoff-Landing Configuration Warnings, Landing Gear and Air-Ground sensing. ✓
  2. Takeoff-Landing Configuration Warnings, Landing Gear and Anti-Skid
  3. Air-Ground sensing, Landing Gear and Air/Ground sensing.
  4. Air-Ground sensing, Landing Gear and Anti-Skid.
正确答案：Takeoff-Landing Configuration Warnings, Landing Gear and Air-Ground sensing.　·　NG　·　来源 smartcockpit.com

111.The Stall Warning System Stick Shaker can be tested by pressing the STALL WARNING TEST buttons on the AFT overhead panel. Pressing No1 switch will activate the Captain's Stick Shaker and the Captain's column will vibrate. Pressing N02 switch will activate the FO's Stick Shaker and the FO's column will vibrate.

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

112.Takeoff configuration warning is armed when the airplane is on the ground and either or both forward thrust levers are advanced for takeoff.

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

113.When is a traffic advisory issued?

  1. When the other aircraft is within 20 NM
  2. When the aircraft is within 20 seconds of the closest approach.
  3. When the other aircraft is within 40 NM.
  4. When the aircraft is within 40 seconds of the closest approach. ✓
正确答案：When the aircraft is within 40 seconds of the closest approach.　·　NG　·　来源 smartcockpit.com

114.When testing the Mach-Airspeed warning system in flight, the No1 and No2 systems must be tested separately to identify that the clacker sounds for both systems independently.

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

115.The predictive windshear symbol radials, which extend from the predictive winsdshear symbol to help identify the location of a windshear event, are displayed in what colours?

  1. Amber. ✓
  2. Red.
  3. Displayed amber when a predictive winshear caution is active, and displayed red when a predictive windshear warning is active.
  4. Red and Black banded.
正确答案：Amber.　·　NG　·　来源 smartcockpit.com

116.RAs can only be generated if the other airplane has a working:

  1. Mode A transponder.
  2. Mode C transponder. ✓
  3. Mode S transponder.
  4. TCAS system.
正确答案：Mode C transponder.　·　NG　·　来源 smartcockpit.com

117.While flying an ILS approach below 1, 000 feet Radio Altitude, a BELOW G/S alert occurs. To cancel the alert:

  1. Press RECALL.
  2. Push either pilot's BELOW GS P-INHIBIT light, or correct the flight path back to the glide slope. ✓
  3. The alert cannot be cancelled.
  4. Select another mode on MCP.
正确答案：Push either pilot's BELOW GS P-INHIBIT light, or correct the flight path back to the glide slope.　·　NG　·　来源 smartcockpit.com

118.With both engines operating and one forward thrust lever set below approximately 20 degrees thrust lever angle, the landing gear warning horn can be silenced with the landing gear warning HORN CUTOUT switch:

  1. It cannot be silenced if the thrust lever angle is less than 20 degrees.
  2. With flaps UP through 10 if below 800 feet RA and above 200 feet RA. ✓
  3. With flaps UP through 25 if below 800 feet RA and above 200 feet RA.
  4. With flaps UP through 10 if below 800 feet RA and above 300 feet RA.
正确答案：With flaps UP through 10 if below 800 feet RA and above 200 feet RA.　·　NG　·　来源 smartcockpit.com

119.The Cabin Altitude and Takeoff Configuration Warnings use the same intermittent tone when activated.

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

120.The TCAS system generates a Traffic Advisory, whenever another aircraft is what distance from point of closest approach?

  1. 40 seconds. ✓
  2. Less than 6 nm separation with less than 1200 feet vertical separation.
  3. More than 6 nm separation with more than 1200 feet vertical separation.
  4. 25 seconds.
正确答案：40 seconds.　·　NG　·　来源 smartcockpit.com

121.The terrain displayed in the Look-Ahead Terrain Alerting system is generated from:

  1. Weather Radar correlated with IRS position.
  2. GPWS nav database correlated with IRS position.
  3. GPWS nav database correlated with GPS position. ✓
  4. FMC nav database correlated with GPS position.
正确答案：GPWS nav database correlated with GPS position.　·　NG　·　来源 smartcockpit.com

122.Vertical motion information is indicated by an arrow depicting a climb or descent if a change of greater than _____ is detected.

  1. 250 feet per minute.
  2. 500 feet per minute. ✓
  3. 750 feet per minute.
  4. 800 feet per minute.
正确答案：500 feet per minute.　·　NG　·　来源 smartcockpit.com

123.The GPWS will provide an aural alert of 'BANK ANGLE, BANK ANGLE' under which of the following circumstances?

  1. Whenever trailing edge flaps are at 1 or greater and roll angle exceeds 35 degrees.
  2. When roll angle exceeds the maximum of 45 degrees.
  3. When roll angle exceeding 35, 40 and 45 degrees. ✓
  4. Whenever the bank angle exceeds the setting on the Bank Angle Selector.
正确答案：When roll angle exceeding 35, 40 and 45 degrees.　·　NG　·　来源 smartcockpit.com

124.Which of the following will cause activation of the takeoff configuration warning system?

  1. Leading edge flaps in the extend position and trailing edge flaps at flaps 5.
  2. Leading edge flpas in the full extend position and trailing edge flaps at 15.
  3. Spoilers partially extended. ✓
  4. SPEED BRAKE lever in the DOWN position.
正确答案：Spoilers partially extended.　·　NG　·　来源 smartcockpit.com

125.Which two displays cannot be selected and shown simultaneously on the Navigation DU?

  1. Terrain and TCAS.
  2. Weather and Data.
  3. Weather and Terrain. ✓
  4. TCAS and Airport.
正确答案：Weather and Terrain.　·　NG　·　来源 smartcockpit.com

126.Altitude alerting occurs when approaching or departing from the MCP selected altitude. When is the altitude alerting system inhibited?

  1. Leading edge flaps are extended to 25 or greater.
  2. Glide slope is captured, or trailing edge flaps are extended to 25 or greater. ✓
  3. Landing gear is down and locked.
  4. Leading edge flaps are extended to 25 or greater and the landing gear is extended.
正确答案：Glide slope is captured, or trailing edge flaps are extended to 25 or greater.　·　NG　·　来源 smartcockpit.com

127.When will the landing gear config warning horn give an intermittent warning sound?

  1. Flaps up through 10, below 800 feet RA, either forward thrust lever at 20 degrees or less (or less than 34 degrees if only 1 engine running).
  2. Never. ✓
  3. Flaps greater than 25, below 800 feet RA, regardless of forward thrust lever position.
  4. Flaps 1 through 10, below 800 feet RA, either forward thrust lever at 20 degrees or less (or less than 34 degrees if only 1 engine running).
正确答案：Never.　·　NG　·　来源 smartcockpit.com

128.All TCAS alerts are inhibited:

  1. Below approximately 500 feet radio altitude.
  2. By GPWS and windshear warnings. ✓
  3. Below approximately 1,100 feet radio altitude.
  4. Until the flaps are fully retracted after takeoff.
正确答案：By GPWS and windshear warnings.　·　NG　·　来源 smartcockpit.com

129.A TA symbol showing on the ND has, alongside it, a down arrow and '-07'. This means:

  1. The traffic is descending at 700fpm. ✓
  2. You should descend at 700fpm.
  3. The traffic is descending at minimum 500fpm.
  4. You should descend at minimum 500fpm.
正确答案：The traffic is descending at 700fpm.　·　NG　·　来源 smartcockpit.com

130.Which of the following statements is true for the CABIN ALTITUDE Warning?

  1. An intermittent warning horn sounds and the red CABIN ALTITUDE lights illuminate when the cabin altitude exceeds 10000 feet. ✓
  2. An intermittent warning horn sounds and the amber CABIN ALTITUDE warning lights illuminate when the cabin altitude exceeds 10000 feet.
  3. A steady warning horn sounds and the amber CABIN ALTITUDE lights illuminate when the cabin altitude exceeds 14000 feet.
  4. A steady warning horn sounds and the red CABIN ALTITUDE warning lights illuminate when the cabin altitude exceeds 14000 feet.
正确答案：An intermittent warning horn sounds and the red CABIN ALTITUDE lights illuminate when the cabin altitude exceeds 10000 feet.　·　NG　·　来源 smartcockpit.com

131.The PSEU light, located on the forward overhead panel, will illuminate on the ground if a fault is detected in the PSEU or if an overwing exit flight lock fails to disengage when commanded.

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

132.The Stall Warning requirement is determined by what system component?

  1. A single stall management configuration computer.
  2. Two independent SMYD Computers. ✓
  3. The Captain's or F/O's Alpha Vane.
  4. Two independent ADIRUs.
正确答案：Two independent SMYD Computers.　·　NG　·　来源 smartcockpit.com

133.What is correct about the color on the terrain display?

  1. Dotted green - terrain 2500 feet below up to 500 feet below. ✓
  2. Dotted amber - terrain 2000 feet below up to 500 feet below.
  3. Dotted red - terrain more than 5000 feet above the aircraft.
  4. Solid red - look ahead terrain warning is active.
正确答案：Dotted green - terrain 2500 feet below up to 500 feet below.　·　NG　·　来源 smartcockpit.com

134.What is the first Radio Altitude Callout given during the approach?

  1. 2500 feet - 'Twenty Five Hundred'. ✓
  2. 1000 feet - 'One Thousand'.
  3. 2000 feet - 'Two thousand'.
  4. 50 feet - 'Fifty'.
正确答案：2500 feet - 'Twenty Five Hundred'.　·　NG　·　来源 smartcockpit.com

135.The GPWS provides a 'BANK ANGLE' warning when the roll rate exceeds 25 degrees, 30 degrees, and 35 degrees.

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

136.Which statement is correct?

  1. When the RHS pilot omits to set the minima on the baro, but the LHS pilot sets the minima correctly, there will be no GPWS minimums callouts.
  2. When the RHS pilot omits to set the minima on the baro, but the LHS pilot sets the minima correctly, there will be a GPWS minimums callouts, since the callouts are based on the captains minimums selector. ✓
  3. It is impossible to omit to set the minima before any approach, because the aircraft GPWS will remind you in time.
  4. There is no correct statement.
正确答案：When the RHS pilot omits to set the minima on the baro, but the LHS pilot sets the minima correctly, there will be a GPWS minimums callouts, since the callouts are based on the captains minimums selector.　·　NG　·　来源 smartcockpit.com

137.When performance is limited, such as with an inoperative engine, to prevent receiving RAs beyond the airplane’s capabilities:

  1. Select ALT OFF. ✓
  2. Select TCAS OFF.
  3. Select TA/RA.
  4. Select TA.
正确答案：Select ALT OFF.　·　NG　·　来源 smartcockpit.com

138.At what altitude (in feet) do the RA callouts begin?

  1. Fifteen hundred.
  2. Two thousand.
  3. One thousand.
  4. Twenty five hundred. ✓
正确答案：Twenty five hundred.　·　NG　·　来源 smartcockpit.com

139.How can the Fire Warning Bell be silenced on the flight deck?

  1. Fire bell can only be silenced by pressing either master fire warn light.
  2. Push the master fire warn lights, press the horn cutout of the APU ground control panel, push fire warning bell cutout switch.
  3. Push the Master Fire Warn lights, press the Horn Cutout of the APU Ground Control Panel.
  4. Push the master fire warn lights, push fire warning bell cutout switch. ✓
正确答案：Push the master fire warn lights, push fire warning bell cutout switch.　·　NG　·　来源 smartcockpit.com

140.As well as providing outputs for all stall warnings, the SMYD computers also provide outputs for GPWS Windshear Detection and Alert.

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

141.The Ground Proximity Warning System Test:

  1. Can be performed only on the ground.
  2. Is inhibited from liftoff to 1,000 feet Radio Altitude. ✓
  3. Can be performed only above 1,000 feet Radio Altitude.
  4. Can be performed anytime.
正确答案：Is inhibited from liftoff to 1,000 feet Radio Altitude.　·　NG　·　来源 smartcockpit.com

142.While performing the LANDING checklist the PSEU light illuminates on recall. This indicates:

  1. A normal condition
  2. A fault is detected in the landing gear locking system or the air/ground sensing systems.
  3. The landing gear configuration warning horn will sound upon landing.
  4. A problem exists in the PSEU system because the light should be inhibited in flight. ✓
正确答案：A problem exists in the PSEU system because the light should be inhibited in flight.　·　NG　·　来源 smartcockpit.com

143.In Flight, the Intuvue radar will provide a windshear warning from 0.5nm to 3nm ahead of the aircraft.

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

144.Below what altitude are windshear alerts available for aircraft fitted with IntuVue weather radar?

  1. 1500 feet AGL and below.
  2. 1200 feet RA and below. ✓
  3. 1800 feet RA and below
  4. 2300 feet AGL and below.
正确答案：1200 feet RA and below.　·　NG　·　来源 Chair Flight B737 Question Bank

145.The Master Caution lights and ENG system annunciator lights will illuminate if the EEC automatically enters the soft alternate mode.

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