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Boeing 737 · Flight Controls 题库（192 题）

Boeing 737 机型「Flight Controls」相关知识共 192 道题。想练习或模拟考试，请到 题库 · 模拟考试。
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1.One of the conditions for the 737NG speed trim system to operate is

  1. At least 10 seconds after take-off. ✓
  2. Autopilot engaged.
  3. The flaps are not up.
正确答案：At least 10 seconds after take-off.　·　737　·　来源 b737.org.uk

2.Illumination of the Speed Trim Fail light (Master Caution Annunciator recall is not activated)

  1. Indicates failure of both FCC channels. ✓
  2. Indicates failure of a single FCC channel.
  3. Indicates failure of the elevator feel computer.
正确答案：Indicates failure of both FCC channels.　·　737　·　来源 b737.org.uk

3.Illumination of the Speed Trim Fail light when Master Caution recall is activated

  1. Indicates failure of the elevator feel computer.
  2. Indicates failure of both FCC channels and the elevator feel computer.
  3. Indicates failure of a single FCC channel. ✓
正确答案：Indicates failure of a single FCC channel.　·　737　·　来源 b737.org.uk

4.Illumination of the Auto Slat Fail light when Master Caution recall is activated

  1. Indicates failure of a FCC channel or both autoslat computers.
  2. Indicates failure of a single autoslat computer. ✓
  3. Indicates failure of the elevator feel computer.
正确答案：Indicates failure of a single autoslat computer.　·　737　·　来源 b737.org.uk

5.Illumination of the Auto Slat Fail light (Master Caution Annunciator recall is not activated)

  1. Indicates failure of a single FCC channel.
  2. Indicates failure of a single autoslat computer.
  3. Indicates failure of both autoslat computers. ✓
正确答案：Indicates failure of both autoslat computers.　·　737　·　来源 b737.org.uk

6.The Feel Differential Pressure amber light is

  1. Armed when the trailing edge flaps are up.
  2. Armed when the trailing edge flaps are up or down. ✓
  3. Armed when the trailing edge flaps are not up.
正确答案：Armed when the trailing edge flaps are up or down.　·　737　·　来源 b737.org.uk

7.A single autoslat channel failure is indicated

  1. By the immediate illumination of the Auto Slat Fail light.
  2. By the illumination of the Auto Slat Fail light on a Master Caution annunciator recall. ✓
  3. By pressing to test the Auto Slat Fail light.
正确答案：By the illumination of the Auto Slat Fail light on a Master Caution annunciator recall.　·　737　·　来源 b737.org.uk

8.A single mach trim FCC channel failure is indicated

  1. By the illumination of the Mach Trim Fail light on a Master Caution annunciator recall. ✓
  2. By the immediate illumination of the Mach trim Fail light.
  3. By pressing to test the Mach Trim Fail light.
正确答案：By the illumination of the Mach Trim Fail light on a Master Caution annunciator recall.　·　737　·　来源 b737.org.uk

9.Positioning the FLT CONTROL A switch to STBY RUD

  1. Arms the STANDBY HYD Low Qantity light.
  2. Arms the STANDBY HYD Low Pressure light. ✓
  3. Arms the Alternate Flaps Master switch.
正确答案：Arms the STANDBY HYD Low Pressure light.　·　737　·　来源 b737.org.uk

10.The Yaw Damper operation results in

  1. No rudder pedal movement. ✓
  2. Rudder pedal movement.
  3. No rudder pedal movement provided the autopilot is engaged.
正确答案：No rudder pedal movement.　·　737　·　来源 b737.org.uk

11.Rudder Trim control requires

  1. Both hydraulic and electrical power to trim the rudder. ✓
  2. Electrical power only to trim the rudder.
  3. Hydraulic power only to trim the rudder.
正确答案：Both hydraulic and electrical power to trim the rudder.　·　737　·　来源 b737.org.uk

12.The main Yaw Damper will provide yaw damper inputs to:

  1. The main rudder Power Control Unit. ✓
  2. The standby rudder Power Control Unit.
  3. Both main and standby rudder Power Control Units as appropriate.
正确答案：The main rudder Power Control Unit.　·　737　·　来源 b737.org.uk

13.Loss of hydraulic system B pressure

  1. Does not cause yaw damper disengagement but will illuminate the amber YAW DAMPER light.
  2. Causes yaw damper disengagement and illumination of the YAW DAMPER light.
  3. Does not cause yaw damper disengagement or illumination of the amber YAW DAMPER light. ✓
正确答案：Does not cause yaw damper disengagement or illumination of the amber YAW DAMPER light.　·　737　·　来源 b737.org.uk

14.The Yaw Damper uses

  1. Both hydraulic systems A and B pressure.
  2. Hydraulic system A pressure only.
  3. Hydraulic system B pressure only. ✓
正确答案：Hydraulic system B pressure only.　·　737　·　来源 b737.org.uk

15.Aileron trim is accomplished by

  1. Simultaneous operation of the trim switches located on the control stand. ✓
  2. Operation of either trim switch located on the control stand.
  3. Operation of the aileron trim knob located on the control stand.
正确答案：Simultaneous operation of the trim switches located on the control stand.　·　737　·　来源 b737.org.uk

16.The amount of aileron trim set by a pilot

  1. Is indicated on the graduated scale of the rudder/aileron trim indicator.
  2. Is indicated by the amount of control column deflection. ✓
  3. Is not indicated.
正确答案：Is indicated by the amount of control column deflection.　·　737　·　来源 b737.org.uk

17.Operation of the Rudder Trim Control switch

  1. Hydraulically repositions the rudder feel mechanism which results in a shift in the rudder position.
  2. Electrically repositions the rudder trim tab and centring mechanism which results in a shift in both the rudder and tab positions.
  3. Electrically repositions the rudder feel and centring mechanism which results in a shift in the rudder neutral position. ✓
正确答案：Electrically repositions the rudder feel and centring mechanism which results in a shift in the rudder neutral position.　·　737　·　来源 b737.org.uk

18.The Rudder Trim Control is

  1. Spring-loaded to neutral and must be pushed down before rotating left or right.
  2. Spring-loaded to neutral and may be rotated left or right. ✓
  3. Spring-loaded to neutral and may be rotated left or right provided the autopilot is disengaged.
正确答案：Spring-loaded to neutral and may be rotated left or right.　·　737　·　来源 b737.org.uk

19.If the speed brake lever is not ARMED prior to landing. All the spoiler panels will

  1. Automatically extend after landing when thrust levers are positioned for reverse thrust. ✓
  2. Remain retracted after landing even when thrust levers are positioned for reverse thrust.
  3. Automatically extend after landing when thrust levers are positioned for reverse thrust, provided the Autobrake system is in use.
正确答案：Automatically extend after landing when thrust levers are positioned for reverse thrust.　·　737　·　来源 b737.org.uk

20.If the speed brake lever is used in-flight (ie ARMED) and then returned to DOWN prior to landing (SPEED BRAKE ARMED light extinguished). All the spoiler panels will

  1. Automatically extend after landing when thrust levers are positioned for reverse thrust. ✓
  2. Remain retracted after landing when thrust levers are positioned for reverse thrust.
  3. Automatically extend after landing when thrust levers are positioned for reverse thrust, provided the Autobrake system is in use.
正确答案：Automatically extend after landing when thrust levers are positioned for reverse thrust.　·　737　·　来源 b737.org.uk

21.The Speed Brake Test switches (if installed)

  1. Are used as a cockpit pre-flight check of the auto brake system.
  2. Are used as a cockpit pre-flight check of the auto spoiler system.
  3. Are used for maintenance test purposes only. ✓
正确答案：Are used for maintenance test purposes only.　·　737　·　来源 b737.org.uk

22.The LE FLAPS TRANSIT amber light on the centre instrument panel

  1. Is inhibited during flap load relief operation.
  2. Is not inhibited during autoslat operation in flight.
  3. Is inhibited during autoslat operation in flight. ✓
正确答案：Is inhibited during autoslat operation in flight.　·　737　·　来源 b737.org.uk

23.Auto Slat operation can be monitored

  1. By reference to the LE FLAPS TRANSIT amber light.
  2. By reference to the Flap Position indicator.
  3. By reference to the LEADING EDGE DEVICES ANNUNCIATOR panel. ✓
正确答案：By reference to the LEADING EDGE DEVICES ANNUNCIATOR panel.　·　737　·　来源 b737.org.uk

24.The Ground Spoilers are powered by

  1. Both A and B hydraulic systems.
  2. The B hydraulic system.
  3. The A hydraulic system. ✓
正确答案：The A hydraulic system.　·　737　·　来源 b737.org.uk

25.The autoslat system is armed

  1. During take-off or approach to landing with the trailing edge flaps selected 10 through 25.
  2. During take-off or approach to landing with the trailing edge flaps selected 1 through 5. ✓
  3. At all times in flight irrespective of the flap position.
正确答案：During take-off or approach to landing with the trailing edge flaps selected 1 through 5.　·　737　·　来源 b737.org.uk

26.The Auto Slat system will move

  1. Leading edge slats from the EXTEND to the FULL EXTEND position and back to the EXTEND position again. ✓
  2. Leading edge slats from the RETRACT to the FULL EXTEND position and back to the RETRACT position again.
  3. Leading edge slats from the RETRACT to the EXTEND position and back to the RETRACT position again.
正确答案：Leading edge slats from the EXTEND to the FULL EXTEND position and back to the EXTEND position again.　·　737　·　来源 b737.org.uk

27.How many Ground Spoiler panels are there ?

  1. Classics: 6 - NG: 6
  2. Classics: 6 - NG: 4 ✓
  3. Classics: 4 - NG: 4
正确答案：Classics: 6 - NG: 4　·　737　·　来源 b737.org.uk

28.The Auto Slat system is normally powered by

  1. System A hydraulics.
  2. System B hydraulics. ✓
  3. The Standby Hydraulic system.
正确答案：System B hydraulics.　·　737　·　来源 b737.org.uk

29.An alternate source of power for Autoslat operation is

  1. System A hydraulics through a power transfer unit if a loss of system B pressure is sensed. ✓
  2. The Standby Hydraulic system.
  3. System B hydraulics through a power transfer unit if a loss of system A pressure is sensed.
正确答案：System A hydraulics through a power transfer unit if a loss of system B pressure is sensed.　·　737　·　来源 b737.org.uk

30.The 737NG (Non SFP) Flap Load Relief will retract the trailing edge flaps from the 40 position to the 30 position if the airspeed exceeds

  1. 176 knots.
  2. 163 knots. ✓
  3. 158 knots.
正确答案：163 knots.　·　737　·　来源 b737.org.uk

31.Using Main electric trim, the 737NG stabiliser trim authority is

  1. 3.95 - 14.5 units (flaps extended).
  2. 0.05 - 14.5 units (flaps extended). ✓
  3. 2.5 - 12.5 units (flaps retracted).
正确答案：0.05 - 14.5 units (flaps extended).　·　737　·　来源 b737.org.uk

32.Using Autopilot trim, the 737NG stabiliser trim authority is

  1. 0.05 - 14.5 units (flaps retracted or extended). ✓
  2. 0.25 - 14.0 units (flaps retracted or extended).
  3. 0.05 - 14.5 units (flaps extended).
正确答案：0.05 - 14.5 units (flaps retracted or extended).　·　737　·　来源 b737.org.uk

33.With the Stabilizer Trim Override Switch in the OVERRIDE position

  1. The control column actuated stabiliser trim cutout switches are bypassed to restore power to the electric trim switch. ✓
  2. The control column actuated stabiliser trim cutout switches are bypassed to restore power to the autopilot trim motor.
  3. Cuts power to all electric trim motors and engages the trim clutch allowing manual trimming of the stabiliser.
正确答案：The control column actuated stabiliser trim cutout switches are bypassed to restore power to the electric trim switch.　·　737　·　来源 b737.org.uk

34.A condition for speed trim operation is

  1. N1 above 45% RPM
  2. N1 above 60% RPM ✓
  3. N2 above 60% RPM
正确答案：N1 above 60% RPM　·　737　·　来源 b737.org.uk

35.The maximum altitude for flap extension is

  1. 10,000 Feet.
  2. 15,000 Feet.
  3. 20,000 Feet. ✓
正确答案：20,000 Feet.　·　737　·　来源 b737.org.uk

36.The Speed Brake should not be deployed in flight at radio altitudes of less than

  1. 2500 Feet.
  2. 1500 Feet.
  3. 1000 Feet. ✓
正确答案：1000 Feet.　·　737　·　来源 b737.org.uk

37.The maximum speed for lowering the flaps using the alternate system is

  1. 230 knots. ✓
  2. 210 knots.
  3. 220 knots.
正确答案：230 knots.　·　737　·　来源 b737.org.uk

38.If the MACH TRIM FAIL light is illuminated, limit mach number to

  1. Classics: 0.74 - NG's: 0.82 ✓
  2. Classics: 0.70 - NG's: 0.80
  3. Classics: 0.65 - NG's: 0.78
正确答案：Classics: 0.74 - NG's: 0.82　·　737　·　来源 b737.org.uk

39.The primary flight controls are

  1. Ailerons, Spoilers, Elevators and Rudder.
  2. Ailerons, Elevators and Rudder. ✓
  3. Ailerons, Horizontal Stabiliser, Elevators and Rudder.
正确答案：Ailerons, Elevators and Rudder.　·　737　·　来源 b737.org.uk

40.Power for the Flight Spoilers is supplied by

  1. Hydraulic System A for the inboard spoilers. Hydraulic System B or the Standby hydraulic pump for the outboard spoilers.
  2. Hydraulic System B for the inboard spoilers. Hydraulic System A for the outboard spoilers.
  3. Hydraulic System A for the inboard spoilers. Hydraulic System B for the outboard spoilers. ✓
正确答案：Hydraulic System A for the inboard spoilers. Hydraulic System B for the outboard spoilers.　·　737　·　来源 b737.org.uk

41.Selecting either FLT CONTROL switch to OFF will

  1. Activate the standby pump which will supply hydraulic pressure to the ailerons, elevator and rudder.
  2. Cause both hydraulic systems pressure to be isolated from the ailerons, elevator and rudder.
  3. Cause the corresponding hydraulic system pressure to be isolated from the ailerons, elevator and rudder. ✓
正确答案：Cause the corresponding hydraulic system pressure to be isolated from the ailerons, elevator and rudder.　·　737　·　来源 b737.org.uk

42.FLT CONTROL LOW PRESSURE amber lights indicate

  1. Low hydraulic system pressure to rudder only, and are deactivated when the corresponding FLT CONTROL switch is positioned to STBY RUD and standby rudder SOV opens.
  2. Low hydraulic system pressure to ailerons, elevators and rudder, and the lights are deactivated when the corresponding FLT CONTROL switch is positioned to STBY RUD and standby rudder SOV opens. ✓
  3. Low hydraulic system pressure to corresponding ailerons, elevators and rudder.
正确答案：Low hydraulic system pressure to ailerons, elevators and rudder, and the lights are deactivated when the corresponding FLT CONTROL switch is positioned to STBY RUD and standby rudder SOV opens.　·　737　·　来源 b737.org.uk

43.The Alternate Flaps Position switch when selected to the UP position will

  1. Electrically retract the trailing edge flaps. ✓
  2. Electrically retract the leading and trailing edge flaps.
  3. Hydraulically retract the trailing edge flaps.
正确答案：Electrically retract the trailing edge flaps.　·　737　·　来源 b737.org.uk

44.The elevator Feel Differential Pressure light illuminated indicates that there is

  1. Excessive differential pressure in the elevator feel computer. ✓
  2. Normal pressure in the elevator feel computer.
  3. A failure of an FCC channel.
正确答案：Excessive differential pressure in the elevator feel computer.　·　737　·　来源 b737.org.uk

45.The stabiliser Trim switches are located on

  1. Each pilot's control wheel. ✓
  2. Each pilot's control wheel with alternate trim switches on the centre pedestal.
  3. Each pilot's control wheel with alternate trim levers on the centre pedestal.
正确答案：Each pilot's control wheel.　·　737　·　来源 b737.org.uk

46.In the event of a runaway stabilizer first

  1. Grasp and hold the stabilizer trim wheel.
  2. Hold the control column firmly and disengage the autopilot (if engaged). ✓
  3. Select the Column Activated Stabilizer trim switch to NORMAL.
正确答案：Hold the control column firmly and disengage the autopilot (if engaged).　·　737　·　来源 b737.org.uk

47.The range of stabilizer movement using the main electric trim switches is

  1. Smaller than the auto-pilot range. ✓
  2. Greater than the manual trim range.
  3. Greater than the auto-pilot range.
正确答案：Smaller than the auto-pilot range.　·　737　·　来源 b737.org.uk

48.The STAB OUT OF TRIM amber light when illuminated

  1. Indicates the Speed Trim system is operating.
  2. Indicates the autopilot or pilot is not trimming the stabilizer properly.
  3. Indicates the autopilot is not trimming the stabilizer properly. ✓
正确答案：Indicates the autopilot is not trimming the stabilizer properly.　·　737　·　来源 b737.org.uk

49.In event of a jammed stabilizer

  1. Plan for a flaps 5 landing.
  2. Plan for a flaps 15 landing. ✓
  3. Plan for a flaps 30 landing.
正确答案：Plan for a flaps 15 landing.　·　737　·　来源 b737.org.uk

50.The SPEED BRAKE DO NOT ARM light

  1. When illuminated indicates that the landing gear is not down with the Speed Brake in the ARMED position.
  2. Is green and is de-activated when the Speed Brake Lever is in the DOWN position. Selecting the gear lever to down will extinguish the light.
  3. Is amber and is de-activated when the Speed Brake Lever is in the DOWN position. ✓
正确答案：Is amber and is de-activated when the Speed Brake Lever is in the DOWN position.　·　737　·　来源 b737.org.uk

51.The SPEED BRAKE ARMED light

  1. Is green and should be illuminated when the Speed Brake is moved to the ARMED position indicating valid automatic Speed Brake system inputs. ✓
  2. Is amber and should be illuminated when the Speed Brake is moved to the ARMED position indicating valid automatic Speed Brake system inputs.
  3. Is de-activated when the Speed Brake Lever is in the UP position.
正确答案：Is green and should be illuminated when the Speed Brake is moved to the ARMED position indicating valid automatic Speed Brake system inputs.　·　737　·　来源 b737.org.uk

52.The LE FLAPS TRANSIT light will illuminate when

  1. Any leading edge device is in transit only.
  2. Any leading edge device is in transit or not in the programmed position with respect to trailing edge flaps. ✓
  3. The Leading Edge Annunciator Panel TEST switch has been pressed.
正确答案：Any leading edge device is in transit or not in the programmed position with respect to trailing edge flaps.　·　737　·　来源 b737.org.uk

53.In the event of total hydraulic power failure, rotation of the pilots' control wheels mechanically positions the

  1. Flight Spoilers.
  2. Aileron tabs.
  3. Ailerons ✓
正确答案：Ailerons　·　737　·　来源 b737.org.uk

54.In the event of jammed aileron system, rotation of the co-pilot's control wheel operates the

  1. Aileron tabs for roll control.
  2. Flight Spoilers for roll control. ✓
  3. Ailerons for roll control.
正确答案：Flight Spoilers for roll control.　·　737　·　来源 b737.org.uk

55.Caution should be exercised when using flight spoilers during a turn as

  1. They greatly increase roll rate. ✓
  2. They greatly reduce roll rate.
  3. They cause such a demand on the hydraulic system that the Autopilot may trip off.
正确答案：They greatly increase roll rate.　·　737　·　来源 b737.org.uk

56.If the SPEED BRAKE DO NOT ARM light illuminates when the speed brake lever is selected to the ARMED position

  1. Then the speed brake lever must be restricted to the DOWN position and not used on touchdown.
  2. Then manually deploy the speed brakes immediately on touchdown. ✓
  3. Then ensure the landing gear lever is selected DOWN before arming the speed brake again.
正确答案：Then manually deploy the speed brakes immediately on touchdown.　·　737　·　来源 b737.org.uk

57.If an asymmetric condition develops between the right and left wing trailing edge flaps

  1. The FSEU shuts down the TE drive unit.
  2. The FSEU closes the TE flap bypass valve. ✓
  3. The FSEU shuts down the LE control.
正确答案：The FSEU closes the TE flap bypass valve.　·　737　·　来源 b737.org.uk

58.The FSEU provides Flap Load Relief by:

  1. Retracting the flaps to 25 (flap lever in the 30 position) when the airspeed is in excess of 176 knots ✓
  2. Retracting the flaps to 25 (flap lever in the 30 position) when the airspeed is in excess of 171 knots.
  3. Retracting the flaps to 25 (flap lever in the 30 position) when the airspeed is in excess of 163 knots.
正确答案：Retracting the flaps to 25 (flap lever in the 30 position) when the airspeed is in excess of 176 knots　·　737　·　来源 b737.org.uk

59.The Alternate Flaps switch is selected momentarily to the DOWN position (Alternate Flaps Master Switch in ARM) and the

  1. Leading edge devices are driven out to EXTEND or FULL EXTEND depending on T.E.Flaps position.
  2. Leading edge devices are driven to the EXTEND position.
  3. Leading edge devices are driven to the FULL EXTEND position. ✓
正确答案：Leading edge devices are driven to the FULL EXTEND position.　·　737　·　来源 b737.org.uk

60.The main and standby rudder power control units (PCUs) are powered by

  1. System A and standby pump for the main rudder PCU and system B for the standby rudder PCU.
  2. System A and system B for the main rudder PCU and standby pump for the standby rudder PCU. ✓
  3. System B and standby pump for the main rudder PCU and system A for the standby rudder PCU.
正确答案：System A and system B for the main rudder PCU and standby pump for the standby rudder PCU.　·　737　·　来源 b737.org.uk

61.Elevator balance tabs

  1. Operate continuously during normal or manual reversion operations. ✓
  2. Operate during manual reversion operations only.
  3. Are not fitted to the B737.
正确答案：Operate continuously during normal or manual reversion operations.　·　737　·　来源 b737.org.uk

62.When the Trailing Edge Flaps are selected from UP to the Flap 1 position

  1. The Leading Edge Flaps drive to their fully extended position and the Leading Edge Slats drive to the FULL EXTEND position.
  2. The Leading Edge Flaps drive to their fully extended position and the Leading Edge Slats drive to the EXTEND position. ✓
  3. The Leading Edge Flaps drive to an intermediate position and the Leading Edge Slats drive to the EXTEND position.
正确答案：The Leading Edge Flaps drive to their fully extended position and the Leading Edge Slats drive to the EXTEND position.　·　737　·　来源 b737.org.uk

63.Tabs are fitted to the

  1. Ailerons and Elevators. ✓
  2. Rudder, Ailerons and Elevator.
  3. Rudder and Elevator.
正确答案：Ailerons and Elevators.　·　737　·　来源 b737.org.uk

64.The Leading Edge devices are normally powered by Hydraulic system

  1. A
  2. B ✓
  3. A and B
正确答案：B　·　737　·　来源 b737.org.uk

65.At what setting(s) should the leading edge FLAPS be partially extended

  1. flap position 10.
  2. flap positions 1 to 5.
  3. The leading edge FLAPS should never be partially extended (always retracted or at full extend). ✓
正确答案：The leading edge FLAPS should never be partially extended (always retracted or at full extend).　·　737　·　来源 b737.org.uk

66.The 737NG Takeoff Configuration Warning system monitors the L/E devices for

  1. L/E devices are not configured for take-off or have uncommanded motion. ✓
  2. L/E devices are not configured for take-off.
  3. L/E devices are not monitored by the Takeoff Configuration Warning system.
正确答案：L/E devices are not configured for take-off or have uncommanded motion.　·　737　·　来源 b737.org.uk

67.The SPEED BRAKE DO NOT ARM light indicates that the speedbrake is not usable.

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

68.Concerning Mach Trim operation, FCCs use Mach information from the ADC / ADIRU, to compute a Mach trim actuator position whih repositions the elevator feel and centering unit, which adjusts the control column neutral position (column will not move).

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

69.The Autoslat system:

  1. Drives the slats to FULL EXTEND when TE Flaps 1 through 5 are selected and the airplane approaches a stall ✓
  2. Provides for slat deployment above VMO/MMO.
  3. Is normally powered by Hydraulic System A.
  4. Is normally powered by Transfer Bus No.2.
正确答案：Drives the slats to FULL EXTEND when TE Flaps 1 through 5 are selected and the airplane approaches a stall　·　MAX　·　来源 smartcockpit.com

70.If the difference in AoAs exceeds 5.5 degrees, what will happen?

  1. The MCAS and STS functions will be disabled for the remainder of the flight and SPEED TRIM FAIL will illuminate immediately ✓
  2. The MCAS and STS functions will be disabled for the remainder of the flight and SPEED TRIM FAIL will illuminate when on ground and below 30 knots
  3. The MCAS and STS functions will be disabled for the remainder of the flight and SPEED TRIM FAIL will illuminate on recall
正确答案：The MCAS and STS functions will be disabled for the remainder of the flight and SPEED TRIM FAIL will illuminate immediately　·　MAX　·　来源 smartcockpit.com

71.The number of slats located on each wing are:

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

72.The amber FEEL DIFF PRESS light illuminates when the:

  1. Flaps are up and a pressure imbalance between hydraulic systems A & B is detected or if one of the elevator feel pitot systems fails ✓
  2. Flaps are not up and a hydraulic pressure imbalance is detected or one of the elevator feel pitot systems fails
  3. Flaps are up or down and a hydraulic pressure imbalance is detected or if one of the elevator pitot systems fails.
  4. Flaps are not up (more than 5) and a hydraulic pressure imbalance is detected or one of the elevator feel pitot systems fails.
正确答案：Flaps are up and a pressure imbalance between hydraulic systems A & B is detected or if one of the elevator feel pitot systems fails　·　MAX　·　来源 smartcockpit.com

73.What is the correct flap setting for a jammed stabilizer landing?

  1. 1
  2. 5
  3. 15 ✓
  4. 30 or 40
正确答案：15　·　MAX　·　来源 smartcockpit.com

74.Speed Trim Failure (SPEED TRIM FAIL) Light - If illuminated (amber) this indicates a:

  1. Failure of the speed trim system.
  2. Failure of the speed trim system but also indicates a failure of a single FCC channel when MASTER CAUTION light recall is activated and light extinguishes when Master Caution System is reset. ✓
  3. Failure of the speed trim system but also indicates failure of the elevator system if the MASTER WARNING cannot be reset.
  4. Partial failure of the speed trim system if the MASTER CAUTION can be reset.
正确答案：Failure of the speed trim system but also indicates a failure of a single FCC channel when MASTER CAUTION light recall is activated and light extinguishes when Master Caution System is reset.　·　MAX　·　来源 smartcockpit.com

75.What is the number of flight spoilers located on each wing?

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

76.If the flight crew selects the ALTERNATE FLAPS to the ARM position:

  1. Trailing Edge flap bypass valve closes, standby pump activates and ALTERNATE FLAPS position switch is armed. ✓
  2. Trailing Edge flap bypass valve closes and standby pump activates.
  3. Standby pump is armed while the Trailing Edge flap bypass valve is de-energized.
  4. Standby pump is armed while the Trailing Edge flap bypass valve is energized.
正确答案：Trailing Edge flap bypass valve closes, standby pump activates and ALTERNATE FLAPS position switch is armed.　·　MAX　·　来源 smartcockpit.com

77.During an ALL FLAPS UP LANDING, the speed to be maintained is:

  1. VREF40 + 15
  2. VREF40 + 30
  3. VREF40 + 55 ✓
  4. VREF40 + 60
正确答案：VREF40 + 55　·　MAX　·　来源 smartcockpit.com

78.Emergency Descent Speedbrakes are armed when is above 30,000 ft and:

  1. the cabin altitude warning is active. ✓
  2. the cabin altitude is above 14,000ft.
  3. the flight spoilers are used.
正确答案：the cabin altitude warning is active.　·　MAX　·　来源 smartcockpit.com

79.The trailing edge flaps are at 15 units. The correct indication on the aft overhead panel for the leading edge devices is:

  1. All amber TRANSIT lights illuminated
  2. All LE devices FULL EXT lights illuminated ✓
  3. All LE devices EXT lights illuminated
  4. LE slats EXT lights and LE flaps FULL EXT lights illuminated.
正确答案：All LE devices FULL EXT lights illuminated　·　MAX　·　来源 smartcockpit.com

80.With the loss of hydraulic system B, (system A operating normally):

  1. Main yaw damper functions are available as long as hydraulic system A is providing normal pressure and the yaw damper switch is ON.
  2. Standby yaw damper functions are available as long as hydraulic system A is providing normal pressure and the yaw damper switch is ON.
  3. Main & standby yaw damper functions are lost. ✓
  4. Standby yaw damper functions are available if the FLT CONTROL B switch is placed to STBY RUD and the YAW DAMPER switch is reset to ON.
正确答案：Main & standby yaw damper functions are lost.　·　MAX　·　来源 smartcockpit.com

81.If the flight crew activates the FLT CONTROL switch Overhead panel to STBY RUD, it activates the:

  1. Standby hydraulic systemp pump.
  2. Standby hydraulic system pump and closes flight control shutoff valve, isolating ailerons and elevators.
  3. Standby hydraulic system pump and opens the standby rudder shutoff valve to pressurize standby rudder power control unit. ✓
  4. Standby hydraulic system pump and closes the standby rudder shutoff valve
正确答案：Standby hydraulic system pump and opens the standby rudder shutoff valve to pressurize standby rudder power control unit.　·　MAX　·　来源 smartcockpit.com

82.Elevator Feel provides simulated aero forces using airspeed from elevator pitot & stabilizer position.

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

83.If a failed AOA circuit is detected, what will happen?

  1. SPEED TRIM FAIL will illuminate immediately.
  2. The Split Vane Monitor and MVS will be bypassed. ✓
  3. The MCAS and STS functions will be disabled for the remainder of the flight
正确答案：The Split Vane Monitor and MVS will be bypassed.　·　MAX　·　来源 smartcockpit.com

84.The FEEL DIFF PRESS light indicates:

  1. A loss of pressure in the elvator feel computer.
  2. An excessive differential pressure in the elevator feel computer. ✓
  3. An excessive temperature in the elevator feel computer
  4. A data loss in the elevator feel computer.
正确答案：An excessive differential pressure in the elevator feel computer.　·　MAX　·　来源 smartcockpit.com

85.The Speed Trim System (STS) operates most frequently during takeoffs & go-arounds. Conditions for speed trim operation are:

  1. Airspeed between 100 KIAS and Mach 0.68, 10 seconds after takeoff, 5 seconds following release of trim switches, N1 above 60%, autopilot not engaged, sensing of trim requirement. ✓
  2. Airspeed between 100 KIAS and Mach 0.68, 10 seconds after takeoff, 5 seconds following release of trim switches, N1 above 40%, sensing of trim requirement.
  3. Airspeed between 100 KIAS and Mach 0.68, 15 seconds after takeoff, 5 seconds following release of trim switches, N1 above 60%, sensing of trim requirement.
  4. Airspeed between 100 KIAS and Mach 0.68, 10 seconds after takeoff, 5 seconds following release of trim switches, N1 above 40%, autopilot not engaged, sensing of trim requirement.
正确答案：Airspeed between 100 KIAS and Mach 0.68, 10 seconds after takeoff, 5 seconds following release of trim switches, N1 above 60%, autopilot not engaged, sensing of trim requirement.　·　MAX　·　来源 smartcockpit.com

86.Landing flap 40 selected and in position. An IAS of 178kts is flown due to a highwind gust. Would you expect:

  1. Flaps to retract to 30. ✓
  2. Flaps to retract to 25.
  3. Flaps to remain in the current configuration.
  4. Flaps to retract to 15.
正确答案：Flaps to retract to 30.　·　MAX　·　来源 smartcockpit.com

87.With a loss of both system A & B, the elevator FEEL DIFF PRESS light will illuminate.

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

88.The Flap/Slat Electronics Unit (FSEU) provides:

  1. LE skew detection for slats 2 through 7 except during autoslat operation
  2. TE asymetry protection by removing hydraulic pressure to the TE flaps if an asymetry is detected
  3. Uncommanded motion protection for LE devices and TE flaps.
  4. All statements are correct. ✓
正确答案：All statements are correct.　·　MAX　·　来源 smartcockpit.com

89.During a steady right-handed turn on the ground, correct indications of the Yaw Damper indicator would be?

  1. Steady full scale left deflection. ✓
  2. Steady full scale right deflection
  3. Steady in the center position.
正确答案：Steady full scale left deflection.　·　MAX　·　来源 smartcockpit.com

90.At what flap setting(s) should the leading edge slats be in the FULL EXTEND position?

  1. 1
  2. 1 to 5
  3. Greater than 5 ✓
  4. 5 to 40.
正确答案：Greater than 5　·　MAX　·　来源 smartcockpit.com

91.The primary flight controls consist of rudder, ailerons and ______

  1. Spoilers
  2. Flaps
  3. Elevators ✓
  4. Speedbrakes
正确答案：Elevators　·　MAX　·　来源 smartcockpit.com

92.During flight with both hydraulic systems A & B inoperative:

  1. The standby hydraulic system operates the trailing edge flaps normally
  2. The standby hydraulic system operates the flaps flaps system normally
  3. Trim is available for the stabilizer and rudder only. Aileron trim is inoperative with the autopilots disengaged. ✓
  4. The autoslat system is still functional through the operation of the PTU
正确答案：Trim is available for the stabilizer and rudder only. Aileron trim is inoperative with the autopilots disengaged.　·　MAX　·　来源 smartcockpit.com

93.The trailing edge flaps devices consist of double slotted flaps inboard outboard of each engine.

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

94.The Power Transfer Unit provides an alternate source of power for the Autoslat System if:

  1. A loss of Hydraulic System A pressure is sensed
  2. Hydraulic System A engine driven pump is inoperative
  3. The Alternate Flaps Position Switch is momentarily held down
  4. A loss of pressure from the Hydraulic System B engine pump is sensed. ✓
正确答案：A loss of pressure from the Hydraulic System B engine pump is sensed.　·　MAX　·　来源 smartcockpit.com

95.The flight spoilers rise on the wing with up aileron and remain faired on the wing with down aileron. When the control wheel is displaced more than approximately ____ degrees, spoiler deflection is initiated.

  1. 6,5
  2. 8
  3. 10 ✓
  4. 12
正确答案：10　·　MAX　·　来源 smartcockpit.com

96.The speedbrake lever will move forward and all spoilers will retract if either thrust lever is advanced after landing.

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

97.The amber LE FLAPS TRANSIT light:

  1. Indicates all LE Devices are fully extended
  2. Indicates LE Slats are fully extended
  3. Is inhibited during Autoslat operation inflight ✓
  4. Provides TE Flaps asymetry protection.
正确答案：Is inhibited during Autoslat operation inflight　·　MAX　·　来源 smartcockpit.com

98.Why are mechanical gates installed on the flap selector unit?

  1. To prevent inadvertent flap lever movement beyond F1 and F15 during G/A ✓
  2. To hinder flap movement beyond F15 until gear down is selected.
  3. Prevent flap movement to UP position when speed is too low.
  4. Prevent flap movement to UP position
正确答案：To prevent inadvertent flap lever movement beyond F1 and F15 during G/A　·　MAX　·　来源 smartcockpit.com

99.During the ALTERNATE FLAPS OPERATION procedure, the flight crew should plan a Flaps 15 landing. After arming the ALTERNATE FLAPS MASTER SWITCH (230 kt max), the flight crew set the flaps to desired flap position and extend flaps on maneuvering speed schedule. The LE FLAPS TRANSIT light will remain illuminates until the flaps approach the:

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

100.The flap load relief system is operational at:

  1. All flap settings.
  2. Flaps 15, 30 & 40.
  3. Flaps 30 & 40. ✓
  4. Flaps 40 only.
正确答案：Flaps 30 & 40.　·　MAX　·　来源 smartcockpit.com

101.What is number of ground spoilers on each wing?

  1. Two. ✓
  2. Three.
  3. Four.
  4. Five.
正确答案：Two.　·　MAX　·　来源 smartcockpit.com

102.Elevator system feel is provided by the elevator feel computer. This computer receives inputs of:

  1. Altitude & elevator position
  2. Elevator balance tabs position
  3. Only System A hydraulic pressure
  4. Airspeed & stabilzer position. ✓
正确答案：Airspeed & stabilzer position.　·　MAX　·　来源 smartcockpit.com

103.Leading Edge devices are normally operated by ______

  1. Hydraulic System A
  2. Hydraulic System B ✓
  3. Hydraulic Systems A & B
  4. Standby Hydraulic system.
正确答案：Hydraulic System B　·　MAX　·　来源 smartcockpit.com

104.The ALTERNATE FLAPS Master Switch:

  1. Arms the Alternate Flaps Position Switch, activates the Standby Hydraulic Pump, and closes the Trailing. ✓
  2. Fully extends the LE Devices using Standby Hydraulic pressure, and electrically extends the TE Flaps
  3. Closes the Flight Spoiler Shutoff valve
  4. Activates the Standby Hydraulic Pump and pressurizes the STANDBY Rudder Power Control Unit.
正确答案：Arms the Alternate Flaps Position Switch, activates the Standby Hydraulic Pump, and closes the Trailing.　·　MAX　·　来源 smartcockpit.com

105.Roll control is provided by the ailerons, assisted by the _____

  1. Flight spoilers ✓
  2. Ground spoilers
  3. Flight spoilers & ground spoilers
  4. Flight spoilers or ground spoilers (depending on speed)
正确答案：Flight spoilers　·　MAX　·　来源 smartcockpit.com

106.Dual AILERON trim switches, located on the aft electronic panel, must be pushed simultaneously to command trim changes. The trim electrically repositions the aileron feel and centering unit, which causes the control wheel to rotate and redefines the aileron neutral position.

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

107.Yaw damper inputs (main or standby) can be overriden:

  1. Only when the yaw damper switch is off.
  2. By trim inputs but not rudder pedal inputs.
  3. By rudder pedal inputs but not trim inputs.
  4. By either trim or rudder pedal inputs. ✓
正确答案：By either trim or rudder pedal inputs.　·　MAX　·　来源 smartcockpit.com

108.The amber ASSIST ON light indicates:

  1. The elevator jam landing asist system is active and flight spoilers must not be used.
  2. The elevator jam landing asist system is active.
  3. The elevator jam landing asist system is active and flight spoilers are extended. ✓
正确答案：The elevator jam landing asist system is active and flight spoilers are extended.　·　MAX　·　来源 smartcockpit.com

109.The Speed Trim System (STS) is a speed stability augmentation system designed to improve flight characteristics during operation with a low gross weight, aft center of gravity and high thrust when the autopilot is not engaged.

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

110.The flight control computers use Mach Information from the _____ to compute a Mach trim actuator position.

  1. ADIRU. ✓
  2. Airspeed Indicator.
  3. Mach/Airspeed Indicator and thrust levers position.
  4. Airspeed Indicator and any thrust lever position.
正确答案：ADIRU.　·　MAX　·　来源 smartcockpit.com

111.Extending the flaps to flaps 15 using ALTERNATE FLAPS takes approximately _______

  1. 30 seconds.
  2. 1 minute.
  3. 2 minutes. ✓
  4. 4 minutes.
正确答案：2 minutes.　·　MAX　·　来源 smartcockpit.com

112.The amber SPOLIERS light is located on the bottom right of the Flight Control Panel and indicates:

  1. It indicates a spoiler fault as sensed by the SCE unit, and that spoilers are inoperative.
  2. It indicates a spoiler fault as sensed by the SCE unit, and that speedbrake must not be used.
  3. It indicates a spoiler fault as sensed by the SCE unit, and that one or more spoiler pairs are inoperative. ✓
正确答案：It indicates a spoiler fault as sensed by the SCE unit, and that one or more spoiler pairs are inoperative.　·　MAX　·　来源 smartcockpit.com

113.In addition to Hydraulic System A & B, the rudder can also be powered by the Standby Hydraulic System through the:

  1. System A Standby Rudder Power Control Unit
  2. System B Standby Rudder Power Control Unit
  3. Standby Rudder Power Control Unit ✓
  4. Main Rudder Power Control Unit
正确答案：Standby Rudder Power Control Unit　·　MAX　·　来源 smartcockpit.com

114.If wheel spinup is not detected on landing with the speed brake armed the flight spoilers will deploy automatically :

  1. When the air/ground system senses the ground mode (any strut compresses). ✓
  2. Only when the RIGHT main landing gear strut compresses.
  3. When the ground spoilers deploy.
  4. Flight spoilers do not deploy on landing, only ground spoilers deploy.
正确答案：When the air/ground system senses the ground mode (any strut compresses).　·　MAX　·　来源 smartcockpit.com

115.If the spoilers become jammed:

  1. The first officer's control wheel operates the ailerons
  2. The captain's control wheel operates the ailerons ✓
  3. The ALT spoiler system is selected
  4. The first officer's control wheel operates the spoilers and ailerons
正确答案：The captain's control wheel operates the ailerons　·　MAX　·　来源 smartcockpit.com

116.Loss of Hydraulic System B pressure does not cause illumination of the amber YAW DAMPER light or yaw damper disengagement.

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

117.What is the maximum flap extension altitude?

  1. 10 000 feet
  2. 17 000 feet
  3. 20 000 feet ✓
  4. 23 000 feet
正确答案：20 000 feet　·　MAX　·　来源 smartcockpit.com

118.A Mach Trim system provides speed stability at the higher Mach numbers.Mach trim is automatically accomplished above:

  1. Mach 0.50
  2. Mach 0.615 ✓
  3. Mach 0.655
  4. Mach 0.70
正确答案：Mach 0.615　·　MAX　·　来源 smartcockpit.com

119.Mach Trim system corrects for Mach tuck by moving stabilizer up.

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

120.In the event of hydraulic Systems A & B fail, ailerons, elevators, and rudder can be operated with the Standby system.

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

121.During descent from altitude you need to decrease your aispeed by using your speed brakes. What is the correct position of the SPEED BRAKE LEVER.

  1. ARMED
  2. FLIGHT DETENT ✓
  3. UP
  4. Any intermediate position.
正确答案：FLIGHT DETENT　·　MAX　·　来源 smartcockpit.com

122.If the SPEEDBRAKES EXTENDED light is illuminated in flight. It indicates:

  1. The speed brake lever is beyond the ARMED position with either the TE flaps extended more than Flaps 10 or the Radio altitude is less than 800 ft. ✓
  2. The speed brake lever is beyond the ARMED position with either the TE flaps extended more than Flaps 5 or the Radio altitude is less than 500 ft.
  3. The speed brake lever is beyond the ARMED position with either the TE flaps extended more than Flaps 15 or the Radio altitude is less than 2500 ft.
  4. The speed brake lever is beyond the ARMED position with either the TE flaps extended more than Flaps 1 or the Radio altitude is less than 800 ft.
正确答案：The speed brake lever is beyond the ARMED position with either the TE flaps extended more than Flaps 10 or the Radio altitude is less than 800 ft.　·　MAX　·　来源 smartcockpit.com

123.The elevator transfer mechanism allows:

  1. The elevator feel and centering unit to transfer the source of power for elevator actuators to hydraulic systems A or B, depending upon which is producing higher pressure.
  2. The control column to be physically separated in the event of an elevator jam. ✓
  3. Forces from either control column to be transferred to the stabilizer.
  4. The elevator feel & centering unit to transfer proper aerodynamic forces to the control columns
正确答案：The control column to be physically separated in the event of an elevator jam.　·　MAX　·　来源 smartcockpit.com

124.The airspeed range for trim operation is:

  1. 100-300 KIAS
  2. 158-300 KIAS
  3. 100 KIAS - Mach 0.50 ✓
  4. 100 KIAS - Mach 0.615
正确答案：100 KIAS - Mach 0.50　·　MAX　·　来源 smartcockpit.com

125.To operate the Feel system, the Elevator Feel Computer uses:

  1. Either hydraulics system A or B pressure
  2. Either hydraulics system A or B pressure (whichever is higher) ✓
  3. Hydraulics system A
  4. Hydraulics system B
正确答案：Either hydraulics system A or B pressure (whichever is higher)　·　MAX　·　来源 smartcockpit.com

126.What do the MACH TRIM FAIL, SPEED TRIM FAIL & AUTO SLAT FAIL lights have in common?

  1. Will illuminate if both system computers fail.
  2. Will illuminate during Master Caution Recall if only one computer has failed.
  3. Also illuminates the Master Caution & FLT CONT annunciator lights.
  4. All statements are correct. ✓
正确答案：All statements are correct.　·　MAX　·　来源 smartcockpit.com

127.If the spoilers become jammed:

  1. The first officer’s control wheel operates the ailerons
  2. The captain’s control wheel operates the ailerons ✓
  3. The ALT spoiler system is selected
  4. The first officer’s control wheel operates the spoilers and ailerons
正确答案：The captain’s control wheel operates the ailerons　·　NG　·　来源 smartcockpit.com

128.During flight with both hydraulic systems A & B inoperative:

  1. The standby hydraulic system operates the trailing edge flaps normally
  2. The standby hydraulic system operates the flaps flaps system normally
  3. Trim is available for the stabilizer and rudder only. Aileron trim is inoperative with the autopilots disengaged. ✓
  4. The autoslat system is still functional through the operation of the PTU
正确答案：Trim is available for the stabilizer and rudder only. Aileron trim is inoperative with the autopilots disengaged.　·　NG　·　来源 smartcockpit.com

129.Mach Trim system corrects for Mach tuck by moving stabilizer up.

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

130.What is number of ground spoilers on each wing?

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

131.Loss of Hydraulic System B pressure does not cause illumination of the amber YAW DAMPER light or yaw damper disengagement.

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

132.The flight spoilers rise on the wing with up aileron and remain faired on the wing with down aileron. When the control wheel is displaced more than approximately ____ degrees, spoiler deflection is initiated.

  1. 6,5
  2. 8
  3. 10 ✓
  4. 12
正确答案：10　·　NG　·　来源 smartcockpit.com

133.? With a loss of both system A & B, the elevator FEEL DIFF PRESS light will illuminate:

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

134.Yaw damper inputs (main or standby) can be overriden:

  1. Only when the yaw damper switch is off
  2. By trim inputs but not rudder pedal inputs
  3. By rudder pedal inputs but not trim inputs
  4. By either trim or rudder pedal inputs. ✓
正确答案：By either trim or rudder pedal inputs.　·　NG　·　来源 smartcockpit.com

135.If the flight crew selects the ALTERNATE FLAPS to the ARM position:

  1. Trailing Edge flap bypass valve closes, standby pump activates and ALTERNATE FLAPS position switch is armed ✓
  2. Trailing Edge flap bypass valve closes and standby pump activates.
  3. Standby pump is armed while the Trailing Edge flap bypass valve is de-energized.
  4. Standby pump is armed while the Trailing Edge flap bypass valve is energized.
正确答案：Trailing Edge flap bypass valve closes, standby pump activates and ALTERNATE FLAPS position switch is armed　·　NG　·　来源 smartcockpit.com

136.The trailing edge flaps devices consist of double slotted flaps inboard outboard of each engine.

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

137.During an ALL FLAPS UP LANDING, the speed to be maintained is:

  1. VREF40 + 15
  2. VREF40 + 30
  3. VREF40 + 55 ✓
  4. VREF40 + 60
正确答案：VREF40 + 55　·　NG　·　来源 smartcockpit.com

138.What is the maximum flap extension altitude?

  1. 10 000 feet
  2. 17 000 feet
  3. 20 000 feet ✓
  4. 23 000 feet
正确答案：20 000 feet　·　NG　·　来源 smartcockpit.com

139.The Power Transfer Unit provides an alternate source of power for the Autoslat System if:

  1. A loss of Hydraulic System A pressure is sensed
  2. Hydraulic System A engine driven pump is inoperative
  3. The Alternate Flaps Position Switch is momentarily held down
  4. A loss of pressure from the Hydraulic System B engine pump is sensed. ✓
正确答案：A loss of pressure from the Hydraulic System B engine pump is sensed.　·　NG　·　来源 smartcockpit.com

140.Landing flap 40 selected and in position. An IAS of 178kts is flown due to a highwind gust. Would you expect:

  1. Flaps to retract to 30. ✓
  2. Flaps to retract to 25.
  3. Flaps to remain in the current configuration.
  4. Flaps to retract to 15.
正确答案：Flaps to retract to 30.　·　NG　·　来源 smartcockpit.com

141.The flight control computers use Mach Information from the _____ to compute a Mach trim actuator position.

  1. ADIRU ✓
  2. Airspeed Indicator
  3. Mach/Airspeed Indicator and thrust levers position
  4. Airspeed Indicator and any thrust lever position.
正确答案：ADIRU　·　NG　·　来源 smartcockpit.com

142.Elevator system feel is provided by the elevator feel computer. This computer receives inputs of:

  1. Altitude & elevator position
  2. Elevator balance tabs position
  3. Only System A hydraulic pressure
  4. Airspeed & stabilzer position. ✓
正确答案：Airspeed & stabilzer position.　·　NG　·　来源 smartcockpit.com

143.The Speed Trim System (STS) operates most frequently during takeoffs & go-arounds. Conditions for speed trim operation are:

  1. Airspeed between 100 KIAS and Mach 0.68, 10 seconds after takeoff, 5 seconds following release of trim switches, N1 above 60%, autopilot not engaged, sensing of trim requirement ✓
  2. Airspeed between 100 KIAS and Mach 0.68, 10 seconds after takeoff, 5 seconds following release of trim switches, N1 above 40%, sensing of trim requirement
  3. Airspeed between 100 KIAS and Mach 0.68, 15 seconds after takeoff, 5 seconds following release of trim switches, N1 above 60%, sensing of trim requirement
  4. Airspeed between 100 KIAS and Mach 0.68, 10 seconds after takeoff, 5 seconds following release of trim switches, N1 above 40%, autopilot not engaged, sensing of trim requirement
正确答案：Airspeed between 100 KIAS and Mach 0.68, 10 seconds after takeoff, 5 seconds following release of trim switches, N1 above 60%, autopilot not engaged, sensing of trim requirement　·　NG　·　来源 smartcockpit.com

144.The trailing edge flaps are at 15 units. The correct indication on the aft overhead panel for the leading edge devices is:

  1. All amber TRANSIT lights illuminated
  2. All LE devices FULL EXT lights illuminated ✓
  3. All LE devices EXT lights illuminated
  4. LE slats EXT lights and LE flaps FULL EXT lights illuminated.
正确答案：All LE devices FULL EXT lights illuminated　·　NG　·　来源 smartcockpit.com

145.The primary flight controls consist of rudder, ailerons and ______

  1. Spoilers
  2. Flaps
  3. Elevators ✓
  4. Speedbrakes
正确答案：Elevators　·　NG　·　来源 smartcockpit.com

146.Dual AILERON trim switches, located on the aft electronic panel, must be pushed simultaneously to command trim changes. The trim electrically repositions the aileron feel and centering unit, which causes the control wheel to rotate and redefines the aileron neutral position.

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

147.Extending the flaps to flaps 15 using ALTERNATE FLAPS takes approximately _______

  1. 30 seconds
  2. 1 minute
  3. 2 minutes ✓
  4. 4 minutes.
正确答案：2 minutes　·　NG　·　来源 smartcockpit.com

148.The number of slats located on each wing are:

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

149.The airspeed range for trim operation is:

  1. 100-300 KIAS
  2. 158-300 KIAS
  3. 100 KIAS - Mach 0.50 ✓
  4. 100 KIAS - Mach 0.615
正确答案：100 KIAS - Mach 0.50　·　NG　·　来源 smartcockpit.com

150.At what flap setting(s) should the leading edge slats be in the FULL EXTEND position?

  1. 1
  2. 1 to 5
  3. Greater than 5 ✓
  4. 5 to 40.
正确答案：Greater than 5　·　NG　·　来源 smartcockpit.com

151.During the ALTERNATE FLAPS OPERATION procedure, the flight crew should plan a Flaps 15 landing. After arming the ALTERNATE FLAPS MASTER SWITCH (230 kt max), the flight crew set the flaps to desired flap position and extend flaps on maneuvering speed schedule. The LE FLAPS TRANSIT light will remain illuminates until the flaps approach the:

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

152.The Speed Trim System (STS) is a speed stability augmentation system designed to improve flight characteristics during operation with a low gross weight, aft center of gravity and high thrust when the autopilot is not engaged.

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

153.The Autoslat system:

  1. Drives the slats to FULL EXTEND when TE Flaps 1 through 5 are selected and the airplane approaches a stall ✓
  2. Provides for slat deployment above VMO/MMO
  3. Is normally powered by Hydraulic System A
  4. Is normally powered by Transfer Bus No.2
正确答案：Drives the slats to FULL EXTEND when TE Flaps 1 through 5 are selected and the airplane approaches a stall　·　NG　·　来源 smartcockpit.com

154.The amber LE FLAPS TRANSIT light:

  1. Indicates all LE Devices are fully extended
  2. Indicates LE Slats are fully extended
  3. Is inhibited during Autoslat operation inflight ✓
  4. Provides TE Flaps asymetry protection.
正确答案：Is inhibited during Autoslat operation inflight　·　NG　·　来源 smartcockpit.com

155.If wheel spinup is not detected on landing with the speed brake armed the flight spoilers will deploy automatically :

  1. When the air/ground system senses the ground mode (any strut compresses) ✓
  2. Only when the RIGHT main landing gear strut compresses
  3. When the ground spoilers deploy
  4. Flight spoilers do not deploy on landing, only ground spoilers deploy.
正确答案：When the air/ground system senses the ground mode (any strut compresses)　·　NG　·　来源 smartcockpit.com

156.A Mach Trim system provides speed stability at the higher Mach numbers.Mach trim is automatically accomplished above:

  1. Mach 0.50
  2. Mach 0.615 ✓
  3. Mach 0.655
  4. Mach 0.70
正确答案：Mach 0.615　·　NG　·　来源 smartcockpit.com

157.If the SPEEDBRAKES EXTENDED light is illuminated in flight. It indicates:

  1. The speed brake lever is beyond the ARMED position with either the TE flaps extended more than Flaps 10 or the Radio altitude is less than 800 ft ✓
  2. The speed brake lever is beyond the ARMED position with either the TE flaps extended more than Flaps 5 or the Radio altitude is less than 500 ft
  3. The speed brake lever is beyond the ARMED position with either the TE flaps extended more than Flaps 15 or the Radio altitude is less than 2500 ft
  4. The speed brake lever is beyond the ARMED position with either the TE flaps extended more than Flaps 1 or the Radio altitude is less than 800 ft
正确答案：The speed brake lever is beyond the ARMED position with either the TE flaps extended more than Flaps 10 or the Radio altitude is less than 800 ft　·　NG　·　来源 smartcockpit.com

158.The amber FEEL DIFF PRESS light illuminates when the:

  1. Flaps are up and a pressure imbalance between hydraulic systems A & B is detected or if one of the elevator feel pitot systems fails ✓
  2. Flaps are not up and a hydraulic pressure imbalance is detected or one of the elevator feel pitot systems fails
  3. Flaps are up or down and a hydraulic pressure imbalance is detected or if one of the elevator pitot systems fails. - No correct answer is provided.
  4. Flaps are not up (more than 5) and a hydraulic pressure imbalance is detected or one of the elevator feel pitot systems fails
正确答案：Flaps are up and a pressure imbalance between hydraulic systems A & B is detected or if one of the elevator feel pitot systems fails　·　NG　·　来源 smartcockpit.com

159.The flap load relief system is operational at:

  1. All flap settings
  2. Flaps 15, 30 & 40
  3. Flaps 30 & 40 ✓
  4. Flaps 40 only.
正确答案：Flaps 30 & 40　·　NG　·　来源 smartcockpit.com

160.Why are mechanical gates installed on the flap selector unit.

  1. To prevent inadvertent flap lever movement beyond F1 and F15 during G/A ✓
  2. To hinder flap movement beyond F15 until gear down is selected.
  3. Prevent flap movement to UP position when speed is too low.
  4. Prevent flap movement to UP position
正确答案：To prevent inadvertent flap lever movement beyond F1 and F15 during G/A　·　NG　·　来源 smartcockpit.com

161.Speed Trim Failure (SPEED TRIM FAIL) Light - If illuminated (amber) this indicates a:

  1. Failure of the speed trim system
  2. Failure of the speed trim system but also indicates a failure of a single FCC channel when MASTER CAUTION light recall is activated and light extinguishes when Master Caution System is reset. ✓
  3. Failure of the speed trim system but also indicates failure of the elevator system if the MASTER WARNING cannot be reset.
  4. Partial failure of the speed trim system if the MASTER CAUTION can be reset.
正确答案：Failure of the speed trim system but also indicates a failure of a single FCC channel when MASTER CAUTION light recall is activated and light extinguishes when Master Caution System is reset.　·　NG　·　来源 smartcockpit.com

162.With the loss of hydraulic system B, (system A operating normally):

  1. Main yaw damper functions are available as long as hydraulic system A is providing normal pressure and the yaw damper switch is ON.
  2. Standby yaw damper functions are available as long as hydraulic system A is providing normal pressure and the yaw damper switch is ON
  3. Main & standby yaw damper functions are lost ✓
  4. Standby yaw damper functions are available if the FLT CONTROL B switch is placed to STBY RUD and the YAW DAMPER switch is reset to ON
正确答案：Main & standby yaw damper functions are lost　·　NG　·　来源 smartcockpit.com

163.What do the MACH TRIM FAIL, SPEED TRIM FAIL & AUTO SLAT FAIL lights have in common? + All of the above.

  1. Will illuminate if both system computers fail.
  2. Will illuminate during Master Caution Recall if only one computer has failed.
  3. Also illuminates the Master Caution & FLT CONT annunciator lights.
  4. All statements are correct. ✓
正确答案：All statements are correct.　·　NG　·　来源 smartcockpit.com

164.To operate the Feel system, the Elevator Feel Computer uses:

  1. Either hydraulics system A or B pressure
  2. Either hydraulics system A or B pressure (whichever is higher) ✓
  3. Hydraulics system A
  4. Hydraulics system B
正确答案：Either hydraulics system A or B pressure (whichever is higher)　·　NG　·　来源 smartcockpit.com

165.The speedbrake lever will move forward and all spoilers will retract if either thrust lever is advanced after landing.

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

166.The SPEED BRAKE DO NOT ARM light indicates that the speedbrake is not usable.

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

167.During a steady right-handed turn on the ground, correct indications of the Yaw Damper indicator would be?

  1. Steady full scale left deflection. ✓
  2. Steady full scale right deflection
  3. Steady in the center position.
正确答案：Steady full scale left deflection.　·　NG　·　来源 smartcockpit.com

168.In addition to Hydraulic System A & B, the rudder can also be powered by the Standby Hydraulic System through the:

  1. System A Standby Rudder Power Control Unit
  2. System B Standby Rudder Power Control Unit
  3. Standby Rudder Power Control Unit ✓
  4. Main Rudder Power Control Unit
正确答案：Standby Rudder Power Control Unit　·　NG　·　来源 smartcockpit.com

169.The Flap/Slat Electronics Unit (FSEU) provides:

  1. LE skew detection for slats 2 through 7 except during autoslat operation
  2. TE asymetry protection by removing hydraulic pressure to the TE flaps if an asymetry is detected
  3. Uncommanded motion protection for LE devices and TE flaps.
  4. All statements are correct. ✓
正确答案：All statements are correct.　·　NG　·　来源 smartcockpit.com

170.What is the number of flight spoilers located on each wing?

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

171.Leading Edge devices are normally operated by ______

  1. Hydraulic System A
  2. Hydraulic System B ✓
  3. Hydraulic Systems A & B
  4. Standby Hydraulic system.
正确答案：Hydraulic System B　·　NG　·　来源 smartcockpit.com

172.If the flight crew activates the FLT CONTROL switch Overhead panel to STBY RUD, it activates the:

  1. Standby hydraulic systemp pump.
  2. Standby hydraulic system pump and closes flight control shutoff valve, isolating ailerons and elevators.
  3. Standby hydraulic system pump and opens the standby rudder shutoff valve to pressurize standby rudder power control unit. ✓
  4. Standby hydraulic system pump and closes the standby rudder shutoff valve
正确答案：Standby hydraulic system pump and opens the standby rudder shutoff valve to pressurize standby rudder power control unit.　·　NG　·　来源 smartcockpit.com

173.The FEEL DIFF PRESS light indicates:

  1. A loss of pressure in the elvator feel computer.
  2. An excessive differential pressure in the elevator feel computer. ✓
  3. An excessive temperature in the elevator feel computer
  4. A data loss in the elevator feel computer.
正确答案：An excessive differential pressure in the elevator feel computer.　·　NG　·　来源 smartcockpit.com

174.The ALTERNATE FLAPS Master Switch:

  1. Arms the Alternate Flaps Position Switch, activates the Standby Hydraulic Pump, and closes the Trailing ✓
  2. Fully extends the LE Devices using Standby Hydraulic pressure, and electrically extends the TE Flaps
  3. Closes the Flight Spoiler Shutoff valve
  4. Activates the Standby Hydraulic Pump and pressurizes the STANDBY Rudder Power Control Unit.
正确答案：Arms the Alternate Flaps Position Switch, activates the Standby Hydraulic Pump, and closes the Trailing　·　NG　·　来源 smartcockpit.com

175.What is the correct flap setting for a jammed stabilizer landing?

  1. 1
  2. 5
  3. 15 ✓
  4. 30 or 40
正确答案：15　·　NG　·　来源 smartcockpit.com

176.The elevator transfer mechanism allows:

  1. The elevator feel and centering unit to transfer the source of power for elevator actuators to hydraulic systems A or B, depending upon which is producing higher pressure.
  2. The control column to be physically separated in the event of an elevator jam. ✓
  3. Forces from either control column to be transferred to the stabilizer.
  4. The elevator feel & centering unit to transfer proper aerodynamic forces to the control columns
正确答案：The control column to be physically separated in the event of an elevator jam.　·　NG　·　来源 smartcockpit.com

177.During descent from altitude you need to decrease your aispeed by using your speed brakes. What is the correct position of the SPEED BRAKE LEVER.

  1. ARMED
  2. FLIGHT DETENT ✓
  3. UP
  4. Any intermediate position.
正确答案：FLIGHT DETENT　·　NG　·　来源 smartcockpit.com

178.Roll control is provided by the ailerons, assisted by the _____

  1. Flight spoilers ✓
  2. Ground spoilers
  3. Flight spoilers & ground spoilers
  4. Flight spoilers or ground spoilers (depending on speed)
正确答案：Flight spoilers　·　NG　·　来源 smartcockpit.com

179.Elevator Feel provides simulated aero forces using airspeed from elevator pitot & stabilizer position.

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

180.In the event of hydraulic Systems A & B fail, ailerons, elevators, and rudder can be operated with the Standby system.

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

181.Concerning Mach Trim operation, FCCs use Mach information from the ADC / ADIRU, to compute a Mach trim actuator position whih repositions the elevator feel & centering unit, which adjusts the control column neutral position (column will not move).

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

182.Moving the STBY RUD switch to ON activates the standby pump and opens the standby rudder shutoff valve to pressurise the standby power control unit.

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

183.Moving the STBY RUD switch to OFF activates the standby pump and opens the standby rudder shutoff valve to pressurise the standby power control unit.

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

184.The flap slat electronic unit (FSEU) provides flap load relief for all aircraft from Flap 10 through to Flap 40.

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

185.The yaw damper provides inputs to the rudder to provide which of the following, and what effect does it have on the rudder pedals?

  1. Provides Gust Dampening, Dutch roll prevention and Turn coordination. The rudder pedals are not displaced by yaw damper operation. ✓
  2. Provides Gust Dampening and Turn coordination. The rudder pedals are not displaced by yaw damper operation.
  3. Provides Gust Dampening, Dutch roll prevention and Turn coordination. The rudder pedals are displaced by yaw damper operation to provide feedback to the pilot.
  4. Provides Gust Dampening and Turn coordination. The rudder pedals move to match rudder movement for feedback to the pilot.
正确答案：Provides Gust Dampening, Dutch roll prevention and Turn coordination. The rudder pedals are not displaced by yaw damper operation.　·　NG　·　来源 Chair Flight B737 Question Bank

186.Selecting the Flap lever to the FLAP 1 Gate causes the LE Flaps to move to what position?

  1. Flap 1 position
  2. Flap 15 position.
  3. Takeoff setting
  4. Fully Extended ✓
正确答案：Fully Extended　·　NG　·　来源 Chair Flight B737 Question Bank

187.What should the maximum flap extension altitude be?

  1. 41,000 feet
  2. 2500 feet RA
  3. Field elevation plus 1000 feet.
  4. 20,000 feet ✓
正确答案：20,000 feet　·　NG　·　来源 Chair Flight B737 Question Bank

188.On short field performance aircraft the leading edge slats do not move from the extended to the fully extended position until the Flap lever is moved beyond the Flap 25 position.

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

189.What is the purpose of the ALTERNATE FLAPS master switch, and why is the cover red?

  1. Closes the trailing edge flap bypass valve, activates standby pump, and arms ALTERNATE FLAPS position switch. Red because the action of extending the trailing edge devices cannot be reversed in flight.
  2. Closes the trailing edge flap bypass valve, activates standby pump, and arms ALTERNATE FLAPS position switch. Red because the action of extending the leading edge devices cannot be reversed in flight. ✓
  3. Fully extends the leading and trailing edge flaps. Red because the action cannot be reversed, leading and trailing edge devices cannot be retracted once extended.
  4. Fully extends the leading edge devices, and can extend and retract the trailing edge flaps. Red because the action cannot be reversed, leading and trailing edge devices cannot be retracted once extended.
正确答案：Closes the trailing edge flap bypass valve, activates standby pump, and arms ALTERNATE FLAPS position switch. Red because the action of extending the leading edge devices cannot be reversed in flight.　·　NG　·　来源 Chair Flight B737 Question Bank

190.What will cause the STBY RUDDER ON light to illuminate?

  1. Standby rudder system is commanded on, either manually or automatically, to pressurise the standby rudder PCU. ✓
  2. Standby rudder system is commanded on, to pressurise the standby rudder PCU, by selecting YAW DAMPER switch to OFF.
  3. Only illuminated when the standby rudder system has been manually commanded on by selecting a FLT CONTROL switch to STBY RUD - not illuminated when standby rudder system automatically commanded on.
正确答案：Standby rudder system is commanded on, either manually or automatically, to pressurise the standby rudder PCU.　·　NG　·　来源 Chair Flight B737 Question Bank

191.On landing, when do the ground spoilers extend?

  1. Compression of the right main landing gear strut. ✓
  2. Compression of the nose landing gear.
  3. Compression of the left main landing gear strut.
  4. Compression of any landing gear strut.
正确答案：Compression of the right main landing gear strut.　·　NG　·　来源 Chair Flight B737 Question Bank

192.In flight, if a fault prevents the EEC receiving flap or anti-ice signals; at what altitude would the Approach Idle schedule begin?

  1. Below 19,000 MSL. ✓
  2. Approach idle must be selected by the crew in these circumstances.
  3. Below 20,000 feet.
  4. Below 15,000 feet RA
正确答案：Below 19,000 MSL.　·　NG　·　来源 Chair Flight B737 Question Bank
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