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40  58.3  63.0  66.6  69.5  71.8  73.6  74.9  76.0  76.9  77.6  78.2 
60  54.6  59.1  62.8  65.7  68.1  70.1  71.7  73.1  74.2  75.1  75.9 
80  51.5  56.0  59.7  62.6  65.1  67.2  69.0  70.4  71.7  72.8  73.7 
100  48.9  53.3  57.0  60.0  62.5  64.7  66.5  68.1  69.5  70.6  71.7 
120  46.6  51.0  54.6  57.7  60.3  62.4  64.3  66.0  67.4  68.7  69.8 
140  44.5  48.9  52.5  55.6  58.2  60.4  62.4  64.0  65.5  66.8  68.0 
160  42.6  47.0  50.6  53.7  56.3  58.6  60.6  62.3  63.8  65.2  66.4 
180  45.3  48.9  51.9  54.6  56.9  58.9  60.7  62.2  63.6  64.9 
200  43.7  47.3  50.3  53.0  55.3  57.3  59.1  60.7  62.1  63.4 
220  42.2  45.8  48.8  51.5  53.8  55.9  57.7  59.3  60.8  62.1 
240  44.4  47.4  50.1  52.4  54.5  56.3  58.0  59.5  60.8 
260  43.1  46.1  48.8  51.1  53.2  55.1  56.7  58.2  59.6 
280  41.8  44.9  47.6  49.9  52.0  53.9  55.5  57.1  58.4 
300  43.7  46.4  48.7  50.8  52.7  54.4  55.9  57.3 

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) 
40  50  60  70  80 
30 & BELOW 32 34  0 -0.6 -1.2  0 -0.8 -1.6  0 -1.0 -2.0  0 -1.2 -2.4  0 -1.4 -2.7 
36 38 40  -1.8 -2.4 -3.0  -2.4 -3.2 -4.0  -3.0 -3.9 -4.9  -3.5 -4.7 -5.9  -4.1 -5.5 -6.8 
42 44 46  -3.6 -4.1 -4.7  -4.7 -5.5 -6.3  -5.9 -6.8 -7.8  -7.0 -8.2 -9.4  -8.2 -9.6 -10.9 
48 50  -5.3 -5.8  -7.0 -7.8  -8.8 -9.7  -10.5 -11.7  -12.3 -13.6 

Pressure Altitude Adjustments
ALT (FT)  OAT ADJUSTED OBSTACLE LIMIT WEIGHT (1000 KG) 
40  50  60  70  80 
S.L & BELOW 1000 2000 3000  0 -1.5 -2.9 -4.3  0 -1.8 -3.7 -5.4  0 -2.2 -4.4 -6.5  0 -2.6 -5.2 -7.6  0 -3.0 -5.9 -8.8 

Copyright . The Boeing Company. See title page for details.
September 27, 2004  PD.30.7
Performance Dispatch

737-800/CFM56-7B24 Takeoff
FAA Category C 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) 
40  50  60  70  80 
15 TW 10 TW 5 TW  -5.4 -3.6 -1.8  -5.7 -3.8 -1.9  -5.9 -4.0 -2.0  -6.2 -4.1 -2.1  -6.5 -4.3 -2.2 
0 10 HW 20 HW  0 1.2 2.4  0 1.0 2.0  0 0.8 1.6  0 0.6 1.2  0 0.4 0.9 
30 HW 40 HW  3.6 4.8  3.0 4.0  2.4 3.3  1.9 2.5  1.3 1.7 

With engine bleed for packs off, increase weight by 750 kg.
With engine anti-ice on, decrease weight by 200 kg.
With engine and wing anti-ice on, decrease weight by 950 kg (optional system).

Copyright . The Boeing Company. See title page for details.
737-800/CFM56-7B24 FAA Category C 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°) 
85 80 75  30300 31600 33000  -5 -8 -11  32800* 34400* 35900*  32800* 34400* 35900*  32800* 34400* 35900*  32100 33400 34800  30700 32000 33400 
70 65 60  34500 36000 37700  -15 -18 -18  37300* 38700* 40200*  37300* 38700* 40200*  37300* 38700* 40200*  36200 37800 39400  34900 36400 38100 
55 50 45 40  39500 41000 41000 41000  -18 -18 -18 -18  41000 41000 41000 41000  41000 41000 41000 41000  41000 41000 41000 41000  41000 41000 41000 41000  39900 41000 41000 41000 

ISA + 15°C
WEIGHT  OPTIMUM  TAT  MARGIN TO INITIAL BUFFET 'G' (BANK ANGLE) 
　
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