B737ng Limitations Study # 1
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: b737study@icloud. Com
- 1.
The Boeing 737-700/800 category for instrument approach is:
- A.
Category A
- B.
Category C
- C.
Category D
Correct Answer
B. Category CExplanation
Flight Manual, Sec. 1, Page 1
Rev. 10/20/05 # 8Rate this question:
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- 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)
Correct Answer
B. Wait at least 62 minutes on Boeing 737-700 and 67 minutes on Boeing 737-800 (carbon brakes 48 minutes)Explanation
Flight Manual, Sec. 1, Page 3
TR 13-03 05/10/13Rate this question:
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- 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
Correct Answer
A. Takeoff dispatch requirementsExplanation
Flight Manual, Sec. 1, Page 3
TR 13-03 05/10/13Rate this question:
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- 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)
Correct Answer
C. 129,200 lbs (700) and 146,300 lbs (800)Explanation
Flight Manual, Sec. 1, Page 5
Rev. 10/30/09 # 10Rate this question:
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- 5.
The maximum altitude for takeoff and landing:
- A.
7,800 feet
- B.
8,400 feet
- C.
10,000 feet
Correct Answer
C. 10,000 feetExplanation
Flight Manual, Sec. 1, Page 3
TR 13-03 05/10/13Rate this question:
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- 6.
Coupled single channel approach with electronic glideslope, the autopilot should not remain engaged below 50 feet AGL.
- A.
YES
- B.
NO
Correct Answer
A. YESExplanation
Flight Manual, Sec. 1, Page 7
Rev. 10/30/09 # 10Rate this question:
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- 7.
The autopilot use is prohibited below 100 feet RA at airport pressure altitudes above 8,400 feet.
- A.
YES
- B.
NO
Correct Answer
A. YESExplanation
Flight Manual, Sec. 1, Page 7
Rev. 10/30/09 # 10Rate this question:
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- 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
Correct Answer
A. Headwind 25 knots, tailwind 15 knots and crosswind 20 knotsExplanation
Flight Manual, Sec. 1, Page 8
Rev. 10/30/09 # 10Rate this question:
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- 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.
Correct Answer
B. For ditching, or other off-airport landings.Explanation
Flight Manual, Sec. 1, Page 8
Rev. 10/30/09 # 10Rate this question:
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- 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
Correct Answer
A. ACARS operationalExplanation
Flight Manual, Sec. 1, Page 8
Rev. 10/30/09 # 10Rate this question:
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- 11.
If frequency 120.00 MHZ is required use:
- A.
VHF COMM # 1
- B.
VHF COMM # 2
- C.
VHF COMM # 3
Correct Answer
A. VHF COMM # 1Explanation
Flight Manual, Sec. 1, Page 8
Rev. 10/30/09 # 10Rate this question:
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- 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
Correct Answer
C. 11.133 MHZ, 22.434 MHZ, 22.638 MHZ and 22.766 MHZExplanation
Flight Manual, Sec. 1, Page 9
Rev. 10/30/09 # 10Rate this question:
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- 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
Correct Answer
B. 75 KVA -215 amps on ground operationExplanation
Flight Manual, Sec. 1, Page 9
Rev. 10/30/09 # 10Rate this question:
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- 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
Correct Answer
C. 195Kts Boeing 737-700 and 200Kts Boeing 737-800Explanation
Flight Manual, Sec. 1, Page 9
Rev. 10/30/09 # 10Rate this question:
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- 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
Correct Answer
A. First indication of fuel low pressure, including as result of attitude pitch changeExplanation
Flight Manual, Sec. 1, Page 10
TR 13-05 09/13/13Rate this question:
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- 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
Correct Answer
A. Three times to minimize residual fluids in balance bay during flightExplanation
Flight Manual, Sec. 1, Page 13
Rev. 11/30/12 # 13Rate this question:
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- 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
Correct Answer
B. - 40 degrees C SATExplanation
Flight Manual, Sec. 1, Page 13
Rev. 11/30/12 # 13Rate this question:
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- 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
Correct Answer
B. On takeoff with less than 5000 pounds or during descent or landing with less than 3000 pounds of fuel in center tankExplanation
Flight Manual, Sec. 1, Page 11
TR 13-05 09/13/13Rate this question:
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- 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
Correct Answer
A. During fuel low indicationExplanation
Flight Manual, Sec. 1, Page 12
Rev. 10/30/11 # 12Rate this question:
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- 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
Correct Answer
C. All of the aboveExplanation
Flight Manual, Sec. 1, Page 14
Rev. 11/30/11 # 12Rate this question:
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- 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
Correct Answer
C. Retract 235kts / Extend 270kts/.82M and Extended 320kts/.82MExplanation
Flight Manual, Sec. 1, Page 14
Rev. 11/30/11 # 12Rate this question:
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- 22.
Autobrakes arming is required on all takeoffs, if operable?
- A.
YES
- B.
NO
Correct Answer
A. YESExplanation
Flight Manual, Sec. 1, Page 14
Rev. 11/30/11 # 12Rate this question:
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- 23.
The maximum start engine EGT:
- A.
710 degrees C
- B.
725 degrees C
- C.
760 degrees C
Correct Answer
B. 725 degrees CExplanation
Flight Manual, Sec. 1, Page 15
Rev. 10/20/05 # 8Rate this question:
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- 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
Correct Answer
A. 13 psi and normal range for takeoffExplanation
Flight Manual, Sec. 1, Page 15
Rev. 10/20/05 # 8Rate this question:
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- 25.
Maximum N1 and N2 RPM:
- A.
104% and 106%
- B.
104% and 105%
- C.
105% and 106%
Correct Answer
B. 104% and 105%Explanation
Flight Manual, Sec. 1, Page 15
Rev. 10/20/05 # 8Rate this question:
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