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120  44.8  48.7  51.8  54.5  56.7  58.6  60.2  61.7  62.9  64.0  65.0  65.8  66.6  67.3 
140  42.8  46.7  49.8  52.5  54.8  56.7  58.4  59.9  61.2  62.3  63.4  64.3  65.1  65.8 
160  44.9  48.0  50.7  53.0  55.0  56.7  58.2  59.6  60.8  61.9  62.8  63.7  64.5 
180  43.2  46.4  49.1  51.4  53.4  55.2  56.7  58.1  59.3  60.4  61.4  62.3  63.2 
200  44.8  47.6  49.9  51.9  53.7  55.3  56.7  58.0  59.1  60.2  61.1  61.9 
220  43.4  46.1  48.5  50.6  52.4  54.0  55.4  56.7  57.9  58.9  59.9  60.8 
240  42.1  44.8  47.2  49.3  51.1  52.7  54.2  55.5  56.7  57.8  58.8  59.7 
260  43.6  46.0  48.0  49.9  51.5  53.0  54.3  55.6  56.7  57.7  58.6 
280  42.5  44.8  46.9  48.8  50.4  51.9  53.3  54.5  55.6  56.6  57.6 
300  41.4  43.7  45.8  47.7  49.3  50.9  52.2  53.5  54.6  55.7  56.6 

Obstacle height must be calculated from lowest point of the runway to conservatively account for runway slope.
OAT Adjustments
OAT (°C)  REFERENCE OBSTACLE LIMIT WEIGHT (1000 KG) 
46  50  54  58  62  66  70  74 
30 & BELOW 32 34  0 -0.8 -1.6  0 -0.9 -1.8  0 -1.0 -2.0  0 -1.1 -2.1  0 -1.1 -2.3  0 -1.2 -2.5  0 -1.3 -2.6  0 -1.4 -2.8 
36 38 40  -2.5 -3.3 -4.1  -2.7 -3.6 -4.5  -2.9 -3.9 -4.9  -3.2 -4.3 -5.3  -3.4 -4.6 -5.7  -3.7 -4.9 -6.2  -3.9 -5.3 -6.6  -4.2 -5.6 -7.0 
42 44 46  -4.9 -5.6 -6.4  -5.3 -6.2 -7.0  -5.8 -6.8 -7.7  -6.3 -7.3 -8.3  -6.8 -7.9 -9.0  -7.3 -8.5 -9.6  -7.8 -9.0 -10.2  -8.3 -9.6 -10.9 
48 50  -7.2 -7.9  -7.9 -8.7  -8.6 -9.5  -9.3 -10.3  -10.0 -11.1  -10.7 -11.9  -11.5 -12.7  -12.2 -13.5 

Pressure Altitude Adjustments
ALT (FT)  OAT ADJUSTED OBSTACLE LIMIT WEIGHT (1000 KG) 
46  50  54  58  62  66  70  74 
S.L.& BELOW 1000 2000  0 -1.6 -3.2  0 -1.7 -3.5  0 -1.9 -3.7  0 -2.0 -4.0  0 -2.1 -4.3  0 -2.3 -4.5  0 -2.4 -4.8  0 -2.5 -5.0 
3000 4000 5000  -4.7 -6.3 -7.9  -5.1 -6.8 -8.5  -5.5 -7.3 -9.2  -5.9 -7.8 -9.8  -6.3 -8.3 -10.4  -6.7 -8.8 -11.1  -7.0 -9.3 -11.7  -7.4 -9.8 -12.3 
6000 7000 8000  -9.5 -11.1 -12.8  -10.3 -12.1 -13.9  -11.0 -13.0 -15.0  -11.8 -13.9 -16.1  -12.6 -14.9 -17.2  -13.3 -15.8 -18.3  -14.1 -16.7 -19.4  -14.9 -17.7 -20.5 
9000 10000  -14.0 -15.2  -15.2 -16.6  -16.5 -18.0  -17.7 -19.4  -19.0 -20.8  -20.2 -22.1  -21.4 -23.5  -22.7 -24.9 

Copyright . The Boeing Company. See title page for details.
September 27, 2004  PD.20.11
Performance Dispatch

737-700/CFM56-7B22 Takeoff
FAA Category A Brakes
737 Flight Crew Operations Manual
Takeoff Obstacle Limit Weight Flaps 5 Sea Level 30°C & Below, Zero Wind Based on engine bleed for packs on and anti-ice off Wind Adjustments
WIND (KTS)  OAT & ALT ADJUSTED OBSTACLE LIMIT WEIGHT (1000 KG) 
46  50  54  58  62  66  70  74 
15 TW 10 TW 5 TW  -7.7 -5.1 -2.6  -7.4 -4.9 -2.5  -7.1 -4.7 -2.4  -6.8 -4.5 -2.3  -6.5 -4.3 -2.2  -6.2 -4.1 -2.1  -5.9 -4.0 -2.0  -5.6 -3.8 -1.9 
0 10 HW 20 HW  0 0.9 1.8  0 0.8 1.7  0 0.8 1.5  0 0.7 1.4  0 0.6 1.3  0 0.6 1.1  0 0.5 1.0  0 0.4 0.8 
30 HW 40 HW  2.8 3.8  2.6 3.5  2.4 3.2  2.1 2.9  1.9 2.6  1.7 2.3  1.5 1.9  1.2 1.6 

With engine bleed for packs off, increase weight by 750 kg.
With engine anti-ice on, decrease weight by 250 kg.
With engine and wing anti-ice on, decrease weight by 1150 kg (optional system).

Copyright . The Boeing Company. See title page for details.
737-700/CFM56-7B22

Performance Dispatch
FAA
Takeoff
Category A Brakes
737 Flight Crew Operations Manual
Takeoff Obstacle Limit Weight - High Altitudes Flaps 5 10000 ft, 10°C & Below, Zero Wind Based on engine bleed for packs on and anti-ice off Reference Obstacle Limit Weight (1000 KG)
　
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