737NG机组操作手册Flight Crew Operations Manual FCOM 1(130)

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OBSTACLE  DISTANCE FROM BRAKE RELEASE (100 M) 
HEIGHT (M)  25  30  35  40  45  50  55  60  65  70  75  80  85  90 
5  53.0  56.3  58.4 
20  48.5  51.9  54.6  56.5  57.8  58.8 
40  44.8  48.1  50.7  52.8  54.5  55.8  56.8  57.7  58.4  59.0  59.5  59.9 
60  41.9  45.2  47.8  49.9  51.7  53.1  54.4  55.4  56.3  57.0  57.6  58.1  58.5  59.0 
80  42.8  45.4  47.6  49.4  50.9  52.2  53.3  54.3  55.1  55.8  56.5  57.0  57.5 
100  43.3  45.5  47.4  49.0  50.3  51.5  52.5  53.4  54.2  54.9  55.5  56.1 
120  41.5  43.7  45.6  47.2  48.6  49.9  50.9  51.9  52.7  53.5  54.1  54.7 
140  42.1  44.0  45.7  47.1  48.4  49.5  50.5  51.3  52.1  52.8  53.5 
160  42.6  44.3  45.7  47.0  48.1  49.2  50.1  50.9  51.6  52.3 
180  41.3  42.9  44.4  45.7  46.9  47.9  48.9  49.7  50.5  51.2 
200  41.7  43.2  44.6  45.7  46.8  47.8  48.6  49.4  50.2 
220  42.1  43.4  44.7  45.7  46.7  47.6  48.4  49.2 
240  41.1  42.4  43.6  44.7  45.7  46.6  47.5  48.2 
260  42.7  43.8  44.8  45.7  46.6  47.3 
280  41.7  42.9  43.9  44.8  45.7  46.5 
300  42.0  43.0  44.0  44.9  45.7 

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  44  48  52  56  60  64 
10 & BELOW 12 14  0 -0.7 -1.4  0 -0.8 -1.6  0 -0.9 -1.7  0 -1.0 -1.9  0 -1.0 -2.1  0 -1.1 -2.3  0 -1.2 -2.5 
16 18 20  -2.1 -2.8 -3.5  -2.3 -3.1 -3.9  -2.6 -3.5 -4.4  -2.9 -3.8 -4.8  -3.1 -4.2 -5.2  -3.4 -4.5 -5.7  -3.7 -4.9 -6.1 
22 24 26  -4.0 -4.5 -5.1  -4.5 -5.2 -5.8  -5.1 -5.8 -6.5  -5.6 -6.4 -7.2  -6.2 -7.1 -8.0  -6.7 -7.7 -8.7  -7.2 -8.3 -9.4 
28 30 32  -5.6 -6.1 -6.4  -6.4 -7.0 -7.5  -7.2 -8.0 -8.5  -8.1 -8.9 -9.6  -8.9 -9.8 -10.7  -9.7 -10.7 -11.7  -10.5 -11.7 -12.8 
34 36 38 40  -6.7 -7.0 -7.4 -7.7  -7.9 -8.4 -8.8 -9.3  -9.1 -9.7 -10.3 -10.9  -10.3 -11.0 -11.8 -12.5  -11.5 -12.4 -13.2 -14.1  -12.7 -13.7 -14.7 -15.7  -13.9 -15.0 -16.2 -17.3 

Pressure Altitude Adjustments
ALT (FT)  OAT ADJUSTED OBSTACLE LIMIT WEIGHT (1000 KG) 
40  44  48  52  56  60  64 
10000 11000 12000  0.0 -1.8 -3.4  0.0 -1.9 -3.8  0.0 -2.1 -4.1  0.0 -2.3 -4.5  0.0 -2.5 -4.9  0.0 -2.7 -5.2  0.0 -2.8 -5.6 
13000 13500  -5.0 -5.7  -5.5 -6.3  -6.0 -6.9  -6.5 -7.5  -7.0 -8.1  -7.5 -8.7  -8.0 -9.2 

Copyright . The Boeing Company. See title page for details.
September 27, 2004  PD.20.13
Performance Dispatch

737-700/CFM56-7B22 Takeoff
FAA 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 Wind Adjustments
WIND (KTS)  OAT & ALT ADJUSTED OBSTACLE LIMIT WEIGHT (1000 KG) 
40  44  48  52  56  60  64 
15 TW 10 TW 5 TW  -6.0 -4.0 -2.0  -5.7 -3.8 -1.9  -5.4 -3.6 -1.8  -5.1 -3.4 -1.7  -4.8 -3.2 -1.6  -4.6 -3.0 -1.5  -4.3 -2.9 -1.4 
0 10 HW 20 HW  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  0 0.4 0.7  0 0.3 0.6 
30 HW 40 HW  2.2 2.9  1.9 2.6  1.7 2.3  1.5 2.0  1.3 1.7  1.1 1.4  0.8 1.1 

With engine bleed for packs off, increase weight by 700 kg.
With engine anti-ice on, decrease weight by 2100 kg.
With engine and wing anti-ice on, decrease weight by 2800 kg (optional system).

Copyright . The Boeing Company. See title page for details.
737-700/CFM56-7B22 FAA Category A Brakes 737 Flight Crew Operations Manual
　
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