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140  42.9  45.7  48.1  50.1  51.8  53.3  54.6  55.8  56.8  57.7  58.5  59.2  59.8 
160  44.0  46.5  48.5  50.3  51.8  53.2  54.3  55.4  56.3  57.2  57.9  58.6 
180  42.5  44.9  47.0  48.8  50.4  51.8  53.0  54.1  55.1  55.9  56.7  57.5 
200  43.5  45.6  47.5  49.1  50.5  51.7  52.9  53.9  54.8  55.6  56.4 
220  42.2  44.4  46.2  47.8  49.3  50.6  51.7  52.7  53.7  54.5  55.3 
240  43.2  45.0  46.7  48.1  49.4  50.6  51.7  52.6  53.5  54.3 
260  42.0  43.9  45.6  47.1  48.4  49.6  50.7  51.6  52.5  53.4 
280  42.9  44.5  46.0  47.4  48.6  49.7  50.7  51.6  52.4 
300  41.9  43.5  45.1  46.4  47.6  48.8  49.8  50.7  51.6 

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) 
42  46  50  54  58  62  66  70 
30 & BELOW 32 34  0 -0.8 -1.6  0 -0.9 -1.7  0 -1.0 -1.9  0 -1.0 -2.1  0 -1.1 -2.2  0 -1.2 -2.4  0 -1.3 -2.6  0 -1.4 -2.7 
36 38 40  -2.4 -3.2 -4.0  -2.6 -3.5 -4.4  -2.9 -3.8 -4.8  -3.1 -4.2 -5.2  -3.4 -4.5 -5.6  -3.6 -4.8 -6.0  -3.9 -5.2 -6.4  -4.1 -5.5 -6.9 
42 44 46  -4.7 -5.4 -6.1  -5.2 -6.0 -6.7  -5.7 -6.5 -7.4  -6.1 -7.1 -8.0  -6.6 -7.7 -8.7  -7.1 -8.2 -9.3  -7.6 -8.8 -10.0  -8.1 -9.4 -10.6 
48 50  -6.8 -7.5  -7.5 -8.3  -8.3 -9.1  -9.0 -9.9  -9.7 -10.7  -10.4 -11.6  -11.2 -12.4  -11.9 -13.2 

Pressure Altitude Adjustments
ALT (FT)  OAT ADJUSTED OBSTACLE LIMIT WEIGHT (1000 KG) 
42  46  50  54  58  62  66  70 
S.L.& BELOW 1000 2000  0 -0.8 -1.6  0 -0.8 -1.6  0 -0.8 -1.6  0 -0.8 -1.7  0 -0.8 -1.7  0 -0.9 -1.7  0 -0.9 -1.8  0 -0.9 -1.8 
3000 4000 5000  -2.5 -3.4 -5.0  -2.5 -3.5 -5.2  -2.6 -3.6 -5.4  -2.7 -3.7 -5.6  -2.7 -3.7 -5.8  -2.8 -3.8 -6.0  -2.8 -3.9 -6.3  -2.9 -4.0 -6.5 
6000 7000 8000  -6.5 -8.3 -10.0  -6.9 -8.8 -10.8  -7.2 -9.4 -11.5  -7.6 -9.9 -12.3  -7.9 -10.5 -13.0  -8.3 -11.0 -13.7  -8.6 -11.6 -14.5  -9.0 -12.1 -15.2 
9000 10000  -11.5 -13.0  -12.5 -14.3  -13.6 -15.6  -14.6 -17.0  -15.7 -18.3  -16.7 -19.7  -17.7 -21.0  -18.8 -22.3 

Copyright . The Boeing Company. See title page for details.
March 29, 2004  PD.10.7
Performance Dispatch

737-700/CFM56-7B20 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) 
42  46  50  54  58  62  66  70 
15 TW 10 TW 5 TW  -6.9 -4.6 -2.3  -6.5 -4.3 -2.2  -6.2 -4.1 -2.1  -5.8 -3.9 -1.9  -5.5 -3.7 -1.8  -5.1 -3.4 -1.7  -4.8 -3.2 -1.6  -4.5 -3.0 -1.5 
0 10 HW 20 HW  0 0.9 1.8  0 0.8 1.6  0 0.7 1.5  0 0.7 1.3  0 0.6 1.1  0 0.5 1.0  0 0.4 0.8  0 0.3 0.6 
30 HW 40 HW  2.7 3.7  2.5 3.3  2.2 3.0  2.0 2.6  1.7 2.3  1.5 2.0  1.2 1.6  0.9 1.3 

With engine bleed for packs off, increase weight by 900 kg.
With engine anti-ice on, decrease weight by 200 kg.
With engine and wing anti-ice on, decrease weight by 850 kg (optional system).

Copyright . The Boeing Company. See title page for details.
737-700/CFM56-7B20 FAA Category A Brakes 737 Flight Crew Operations Manual

Long Range Cruise Maximum Operating Altitude Max Cruise Thrust ISA + 10°C and Below
WEIGHT (1000 KG)  OPTIMUM ALT (FT)  TAT (°C)  MARGIN TO INITIAL BUFFET 'G' (BANK ANGLE) 
1.20 (33°)  1.25 (36°)  1.30 (39°)  1.40 (44°)  1.50 (48°) 
80 75 70  31000 32400 33900  -8 -11 -14  34400* 35900* 37300*  34400* 35900* 37300*  34400* 35900* 37300*  33500 34800 36300  32100 33500 34900 
　
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