B737ng Limitations Study # 1

25 Questions | Total Attempts: 137

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Airplane Quizzes & Trivia

The information contained in this study material meets or exceeds all requirements of the FAA approved Airplane Flight Manual. Flight Crews are responsible for committing all information to memory. Submit your questions or feedback to: [email protected] Com


Questions and Answers
  • 1. 
    The Boeing 737-700/800 category for instrument approach is:
    • A. 

      Category A

    • B. 

      Category C

    • C. 

      Category D

  • 2. 
    If landing weight exceeds the chart value in the Maximum Quick Turn Around Weight Limit Chart, section 4:
    • A. 

      Wait at least 62 minutes on Boeing 737-700 and Boeing 737-800 (carbon brakes 48 minutes)

    • B. 

      Wait at least 62 minutes on Boeing 737-700 and 67 minutes on Boeing 737-800 (carbon brakes 48 minutes)

    • C. 

      Wait at least 67 minutes on Boeing 737-700 and Boeing 737-800 (carbon brakes 48 minutes)

  • 3. 
    Runway clear and dry, Anti-skid and Thrust reverse fully operational. Max Thrust rate and Auto spoilers operational are:
    • A. 

      Takeoff dispatch requirements

    • B. 

      Landing dispatch requirements

    • C. 

      Takeoff and Landing dispatch requirements

  • 4. 
    The maximum landing weight of the B737-700 and B737-800:
    • A. 

      129,200 lbs (700) and 138,300 lbs (800)

    • B. 

      120,500 lbs (700) and 146,300 lbs (800)

    • C. 

      129,200 lbs (700) and 146,300 lbs (800)

  • 5. 
    The maximum altitude for takeoff and landing:
    • A. 

      7,800 feet

    • B. 

      8,400 feet

    • C. 

      10,000 feet

  • 6. 
    Coupled single channel approach with electronic glideslope, the autopilot should not remain engaged below 50 feet AGL.
    • A. 

      YES

    • B. 

      NO

  • 7. 
    The autopilot use is prohibited below 100 feet RA at airport pressure altitudes above 8,400 feet.
    • A. 

      YES

    • B. 

      NO

  • 8. 
    Max allowable winds for autoland:
    • A. 

      Headwind 25 knots, tailwind 15 knots and crosswind 20 knots

    • B. 

      Headwind 20 knots, tailwind 10 knots and crosswind 20 knots

    • C. 

      Headwind 25 knots, tailwind 10 knots and crosswind 20 knots

  • 9. 
    When the Terrain awareness alerting and terrain display function should be inhibited by selecting the TERRAIN INHIBIT switch in INHIBIT?
    • A. 

      Within 15 NM and approaching to land at an airport not contained in the GPWS terrain data base.

    • B. 

      For ditching, or other off-airport landings.

    • C. 

      All of the above.

  • 10. 
    Do not use VHF-3 for ATC communication with:
    • A. 

      ACARS operational

    • B. 

      If audio entertainment system is not in use

    • C. 

      All of the above

  • 11. 
    If frequency 120.00 MHZ is required use: 
    • A. 

      VHF COMM # 1

    • B. 

      VHF COMM # 2

    • C. 

      VHF COMM # 3

  • 12. 
    The following HF frequencies are prohibited>
    • A. 

      11.133 MHZ and 22.434 MHZ

    • B. 

      22.638 MHZ and 22.766 MHZ

    • C. 

      11.133 MHZ, 22.434 MHZ, 22.638 MHZ and 22.766 MHZ

  • 13. 
    The maximum single drive generator load:
    • A. 

      45 KVA -100 amps on ground operation

    • B. 

      75 KVA -215 amps on ground operation

    • C. 

      75 KVA -215 amps on flight operation

  • 14. 
    The flap 15 speed limit:
    • A. 

      195Kts Boeing 737-700 and 800

    • B. 

      210Kts Boeing 737-700 and 800

    • C. 

      195Kts Boeing 737-700 and 200Kts Boeing 737-800

  • 15. 
    Per AD 2001-08-24, Center tank fuel pump switch(es) must be turned off during flight at:
    • A. 

      First indication of fuel low pressure, including as result of attitude pitch change

    • B. 

      First indication of fuel low pressure

    • C. 

      First indication of fuel low pressure, not including as result of attitude pitch change

  • 16. 
    If aircraft has been de-iced, smoothly and slowly cycle full aft to full forward the control column a minimum of:
    • A. 

      Three times to minimize residual fluids in balance bay during flight

    • B. 

      Five times to minimize residual fluids in balance bay during flight

    • C. 

      Every three minutes to minimize residual fluids in balance bay during flight

  • 17. 
    The engine thermal anti-ice must be on when icing conditions exist or are anticipated, except during climb or cruise when the temperature is below
    • A. 

      40 degrees C OAT

    • B. 

      - 40 degrees C SAT

    • C. 

      - 40 degrees C TAT

  • 18. 
    Do not accomplish fuel CONFIG if:
    • A. 

      On takeoff or landing with less than 5000 pounds of fuel in center tank

    • B. 

      On takeoff with less than 5000 pounds or during descent or landing with less than 3000 pounds of fuel in center tank

    • C. 

      On takeoff or landing with less than 3000 pounds of fuel in center tank

  • 19. 
    Both center tanks fuel pumps may be selected ON and all center tank fuel may be used regardless of the amount of fuel remaining in tank when:
    • A. 

      During fuel low indication

    • B. 

      Any fuel pump fail

    • C. 

      Center tank quantity is less than 2000 pounds

  • 20. 
    Maximum allowable difference for RVSM on ground:
    • A. 

      Sea level to 5000 feet, 50 feet between Captain and First Officer

    • B. 

      Sea level to 5000 feet, 75 feet between Captain and field elevation

    • C. 

      All of the above

  • 21. 
    Landing gear placard speed
    • A. 

      Retract 235kts / Extend 235kts/.82M and Extended 320kts/.82M

    • B. 

      Retract 235kts / Extend 235kts/.82M and Extended 270kts/.82M

    • C. 

      Retract 235kts / Extend 270kts/.82M and Extended 320kts/.82M

  • 22. 
    Autobrakes arming is required on all takeoffs, if operable?
    • A. 

      YES

    • B. 

      NO

  • 23. 
    The maximum start engine EGT:
    • A. 

      710 degrees C

    • B. 

      725 degrees C

    • C. 

      760 degrees C

  • 24. 
    The minimum engine oil pressure:
    • A. 

      13 psi and normal range for takeoff

    • B. 

      14 psi and normal range for takeoff

    • C. 

      13 psi

  • 25. 
    Maximum N1 and N2 RPM:
    • A. 

      104% and 106%

    • B. 

      104% and 105%

    • C. 

      105% and 106%