B737ng Limitations Study # 1

1. Autobrakes arming is required on all takeoffs, if operable?

YES

NO

Flight Manual, Sec. 1, Page 14
Rev. 11/30/11 # 12

Explanation

Flight Manual, Sec. 1, Page 14
Rev. 11/30/11 # 12

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

YES

NO

Flight Manual, Sec. 1, Page 7
Rev. 10/30/09 # 10

Explanation

Flight Manual, Sec. 1, Page 7
Rev. 10/30/09 # 10

3. Landing gear placard speed

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

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

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

Flight Manual, Sec. 1, Page 14
Rev. 11/30/11 # 12

Explanation

Flight Manual, Sec. 1, Page 14
Rev. 11/30/11 # 12

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

YES

NO

Flight Manual, Sec. 1, Page 7
Rev. 10/30/09 # 10

Explanation

Flight Manual, Sec. 1, Page 7
Rev. 10/30/09 # 10

5. The maximum start engine EGT:

710 degrees C

725 degrees C

760 degrees C

Flight Manual, Sec. 1, Page 15
Rev. 10/20/05 # 8

Explanation

Flight Manual, Sec. 1, Page 15
Rev. 10/20/05 # 8

6. The Boeing 737-700/800 category for instrument approach is:

Category A

Category C

Category D

Flight Manual, Sec. 1, Page 1
Rev. 10/20/05 # 8

Explanation

Flight Manual, Sec. 1, Page 1
Rev. 10/20/05 # 8

7. The following HF frequencies are prohibited>

11.133 MHZ and 22.434 MHZ

22.638 MHZ and 22.766 MHZ

11.133 MHZ, 22.434 MHZ, 22.638 MHZ and 22.766 MHZ

Flight Manual, Sec. 1, Page 9
Rev. 10/30/09 # 10

Explanation

Flight Manual, Sec. 1, Page 9
Rev. 10/30/09 # 10

8. Do not use VHF-3 for ATC communication with:

ACARS operational

If audio entertainment system is not in use

All of the above

Flight Manual, Sec. 1, Page 8
Rev. 10/30/09 # 10

Explanation

Flight Manual, Sec. 1, Page 8
Rev. 10/30/09 # 10

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

Three times to minimize residual fluids in balance bay during flight

Five times to minimize residual fluids in balance bay during flight

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

Flight Manual, Sec. 1, Page 13
Rev. 11/30/12 # 13

Explanation

Flight Manual, Sec. 1, Page 13
Rev. 11/30/12 # 13

10. 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

40 degrees C OAT

- 40 degrees C SAT

- 40 degrees C TAT

Flight Manual, Sec. 1, Page 13
Rev. 11/30/12 # 13

Explanation

Flight Manual, Sec. 1, Page 13
Rev. 11/30/12 # 13

11. The maximum landing weight of the B737-700 and B737-800:

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

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

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

Flight Manual, Sec. 1, Page 5
Rev. 10/30/09 # 10

Explanation

Flight Manual, Sec. 1, Page 5
Rev. 10/30/09 # 10

12. Maximum allowable difference for RVSM on ground:

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

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

All of the above

Flight Manual, Sec. 1, Page 14
Rev. 11/30/11 # 12

Explanation

Flight Manual, Sec. 1, Page 14
Rev. 11/30/11 # 12

13. If frequency 120.00 MHZ is required use:

VHF COMM # 1

VHF COMM # 2

VHF COMM # 3

Flight Manual, Sec. 1, Page 8
Rev. 10/30/09 # 10

Explanation

Flight Manual, Sec. 1, Page 8
Rev. 10/30/09 # 10

14. The minimum engine oil pressure:

13 psi and normal range for takeoff

14 psi and normal range for takeoff

13 psi

Flight Manual, Sec. 1, Page 15
Rev. 10/20/05 # 8

Explanation

Flight Manual, Sec. 1, Page 15
Rev. 10/20/05 # 8

15. The flap 15 speed limit:

195Kts Boeing 737-700 and 800

210Kts Boeing 737-700 and 800

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

Flight Manual, Sec. 1, Page 9
Rev. 10/30/09 # 10

Explanation

Flight Manual, Sec. 1, Page 9
Rev. 10/30/09 # 10

16. 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:

During fuel low indication

Any fuel pump fail

Center tank quantity is less than 2000 pounds

Flight Manual, Sec. 1, Page 12
Rev. 10/30/11 # 12

Explanation

Flight Manual, Sec. 1, Page 12
Rev. 10/30/11 # 12

17. Maximum N1 and N2 RPM:

104% and 106%

104% and 105%

105% and 106%

Flight Manual, Sec. 1, Page 15
Rev. 10/20/05 # 8

Explanation

Flight Manual, Sec. 1, Page 15
Rev. 10/20/05 # 8

18. Max allowable winds for autoland:

Headwind 25 knots, tailwind 15 knots and crosswind 20 knots

Headwind 20 knots, tailwind 10 knots and crosswind 20 knots

Headwind 25 knots, tailwind 10 knots and crosswind 20 knots

Flight Manual, Sec. 1, Page 8
Rev. 10/30/09 # 10

Explanation

Flight Manual, Sec. 1, Page 8
Rev. 10/30/09 # 10

19. Do not accomplish fuel CONFIG if:

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

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

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

Flight Manual, Sec. 1, Page 11
TR 13-05 09/13/13

Explanation

Flight Manual, Sec. 1, Page 11
TR 13-05 09/13/13

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

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

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

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

Flight Manual, Sec. 1, Page 3
TR 13-03 05/10/13

Explanation

Flight Manual, Sec. 1, Page 3
TR 13-03 05/10/13

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

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

First indication of fuel low pressure

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

Flight Manual, Sec. 1, Page 10
TR 13-05 09/13/13

Explanation

Flight Manual, Sec. 1, Page 10
TR 13-05 09/13/13

22. The maximum single drive generator load:

45 KVA -100 amps on ground operation

75 KVA -215 amps on ground operation

75 KVA -215 amps on flight operation

Flight Manual, Sec. 1, Page 9
Rev. 10/30/09 # 10

Explanation

Flight Manual, Sec. 1, Page 9
Rev. 10/30/09 # 10

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

Takeoff dispatch requirements

Landing dispatch requirements

Takeoff and Landing dispatch requirements

Flight Manual, Sec. 1, Page 3
TR 13-03 05/10/13

Explanation

Flight Manual, Sec. 1, Page 3
TR 13-03 05/10/13

24. The maximum altitude for takeoff and landing:

7,800 feet

8,400 feet

10,000 feet

Flight Manual, Sec. 1, Page 3
TR 13-03 05/10/13

Explanation

Flight Manual, Sec. 1, Page 3
TR 13-03 05/10/13

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

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

For ditching, or other off-airport landings.

All of the above.

Flight Manual, Sec. 1, Page 8
Rev. 10/30/09 # 10

Explanation

Flight Manual, Sec. 1, Page 8
Rev. 10/30/09 # 10