Day 7 - Flight Controls, Navigation

21 Questions

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Navigation Quizzes & Trivia

B737


Questions and Answers
  • 1. 
    What does operation of the aileron trim switches do?
    • A. 

      Repositions the neutral position of the aileron feel and centering unit & displaces both control wheels.

    • B. 

      Repositions the neutral position of the aileron feel and centering unit & displaces FOs control wheels.

    • C. 

      Repositions the neutral position of the aileron feel and centering unit & displaces Cpts control wheels.

    • D. 

      Repositions the up position of the aileron feel and centering unit & displaces both control wheels.

  • 2. 
    During alternate flap extension, when will the LE FLAPS TRANSIT amber light be illuminated?
    • A. 

      It is illuminated until the LEDs are fully extended (trailing edge flaps are greater than 5 units )

    • B. 

      It is illuminated until the LEDs are half extended (trailing edge flaps are greater than 15 units )

    • C. 

      It is illuminated until the LEDs are fully extracted (trailing edge flaps are greater than 5 units )

    • D. 

      Only on Approach

  • 3. 
    The auto-slat system can operate when the aircraft is airborne with flaps ….. selected?
    • A. 

      1 to 5

    • B. 

      5 to 30

    • C. 

      15 to 40

    • D. 

      1 to 15

  • 4. 
    The amber flight control LOW PRESSURE lights are extinguished when the associated flight control switch is in what position?
    • A. 

      STBY RUD and the standby rudder shutoff valve is open

    • B. 

      STBY RUD and the standby rudder shutoff valve is closed

    • C. 

      STBY RUD and the standby rudder shutoff valve is in motion

    • D. 

      In UP position

  • 5. 
    The leading edge slats will be at the EXT position until the trailing edge flaps are beyond which flap position?
    • A. 

      1

    • B. 

      5

    • C. 

      15

    • D. 

      30

  • 6. 
    The leading edge devices are normally operated by which hydraulic system?
    • A. 

      A

    • B. 

      B

    • C. 

      Stb system

    • D. 

      A and B

  • 7. 
    During an RTO with main gear wheel speed more than 60kts, the spoilers will automatically deploy when the thrust levers are at what position?
    • A. 

      Idle and reverser is selected

    • B. 

      At Full stop position

    • C. 

      Idle trust

    • D. 

      Max 20 % N1

  • 8. 
    With regard to the alternate flap duty cycle: after a complete extend/retract cycle what cooling period should be allowed before attempting another cycle?
    • A. 

      Four minutes

    • B. 

      Five minutes.

    • C. 

      Two minutes

    • D. 

      One minutes

  • 9. 
    The flaps/slats electronic unit (FSEU) provides “skew” detection for which devices?
    • A. 

      TE flaps and LE slats but NOT the outer LE slates numbered 1 and 8

    • B. 

      TE flaps and TE slats but NOT the outer LE slates numbered 2 and 7

    • C. 

      TE flaps and LE slats and the outer LE slates numbered 1 and 8

    • D. 

      Only on TE flaps

  • 10. 
    What is the maximum altitude for flap section?
    • A. 

      10 000 ft

    • B. 

      20 000 ft

    • C. 

      30 000 ft

    • D. 

      18 000 ft

  • 11. 
    How is the aileron trim position indicated?
    • A. 

      Displacement of both control wheels, and the indication on the scale on the top of each control column

    • B. 

      On the PFD

    • C. 

      Lower panel

    • D. 

      Displacement of both control wheels, and the indication on the scale on the top of each control column

  • 12. 
    The trailing edge flaps are operated by which systems?
    • A. 

      A system

    • B. 

      A and B system

    • C. 

      B system, with an electrical motor as a backup

    • D. 

      B system, with bleed airfrom the APU as backup

  • 13. 
    What causes the yaw damper to disengage?
    • A. 

      Positioning the B system flight control switch to STBY RUD or OFF, or a SMYD fault or SMYD senses a yaw damper system fault/yaw damper does not respond to a command.

    • B. 

      Positioning the A system flight control switch to STBY RUD or OFF, or a SMYD fault or SMYD senses a yaw damper system fault/yaw damper does not respond to a command.

    • C. 

      Positioning the B system flight control switch to ON, or a SMYD fault or SMYD senses a yaw damper system fault/yaw damper does not respond to a command.

    • D. 

      Extreem turbulence

  • 14. 
    At what speed will the flap load relief system move the trailing edge flaps from 40 to 30?
    • A. 

      163 knots

    • B. 

      145 knots

    • C. 

      122 knots

    • D. 

      165 knots

  • 15. 
    At what Mach number does the Mach trim start to operate?
    • A. 

      0,650 Mach

    • B. 

      0,616 Mach

    • C. 

      0,82 Mach

    • D. 

      0.615 Mach.

  • 16. 
    The Primary (most accurate) mode for updating the FMC position is from?
    • A. 

      Either GPS receiver

    • B. 

      DME DME

    • C. 

      The front GPS receiver

    • D. 

      The aft GPS receiver

  • 17. 
    What does positioning the VHF NAV Transfer switch to BOTH ON 1 do?
    • A. 

      Select No2 VOR receiver to supply data to both FCCs and displays

    • B. 

      Select No1 GPS receiver to supply data to both FCCs and displays

    • C. 

      Uses the NAV info from left EDU on all displays

    • D. 

      Select No1 VOR receiver to supply data to both FCCs and displays

  • 18. 
    What position should be selected on the IRS control panel to initiate a full IRS alignment procedure?
    • A. 

      OFF then ALIGN

    • B. 

      OFF then NAV.

    • C. 

      To ALIGN

    • D. 

      OFF for five minutes

  • 19. 
    The left IRS ON DC light illuminates in flight. AC power is normal. How long will the left IRS operate in this configuration?
    • A. 

      5 minutes

    • B. 

      Indefinitely

    • C. 

      3 minutes

    • D. 

      A half hour

  • 20. 
    Are HDG and WIND displays on the IRS display unit true or magnetic?
    • A. 

      True

    • B. 

      Magnetic

  • 21. 
    Before start with all AC busses powered, the IRSs are selected from OFF to ALIGN. The ON DC light momentarily illuminates. What does this indicate?
    • A. 

      No DC-backup power

    • B. 

      A short DC power test, with no action required.

    • C. 

      A DC power test, wait 5 min before reset to NAV

    • D. 

      Antenna malfunction