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 45 50 55 60 65 70 75 80 85 90
30 & BELOW 0 0 0 0 0 0 0 0 0 0 0
32 -0.6 -0.7 -0.8 -0.8 -0.9 -1.0 -1.1 -1.2 -1.3 -1.3 -1.4
34 -1.2 -1.3 -1.5 -1.7 -1.8 -2.0 -2.2 -2.3 -2.5 -2.7 -2.8
36 -1.8 -2.0 -2.3 -2.5 -2.8 -3.0 -3.3 -3.5 -3.8 -4.0 -4.3
38 -2.3 -2.7 -3.0 -3.3 -3.7 -4.0 -4.3 -4.7 -5.0 -5.3 -5.7
40 -2.9 -3.3 -3.8 -4.2 -4.6 -5.0 -5.4 -5.8 -6.3 -6.7 -7.1
42 -3.5 -4.0 -4.5 -5.0 -5.5 -6.0 -6.5 -7.0 -7.5 -7.9 -8.4
44 -4.0 -4.6 -5.2 -5.8 -6.3 -6.9 -7.5 -8.1 -8.6 -9.2 -9.8
46 -4.6 -5.2 -5.9 -6.6 -7.2 -7.9 -8.5 -9.2 -9.8 -10.5 -11.1
48 -5.1 -5.9 -6.6 -7.3 -8.1 -8.8 -9.6 -10.3 -11.0 -11.8 -12.5
50 -5.7 -6.5 -7.3 -8.1 -9.0 -9.8 -10.6 -11.4 -12.2 -13.0 -13.9
Pressure Altitude Adjustments
ALT (FT) OAT ADJUSTED OBSTACLE LIMIT WEIGHT (1000 KG)
40 45 50 55 60 65 70 75 80 85 90
S.L.& BELOW 0 0 0 0 0 0 0 0 0 0 0
1000 -1.5 -1.6 -1.8 -2.0 -2.1 -2.3 -2.5 -2.7 -2.8 -3.0 -3.2
2000 -2.9 -3.3 -3.6 -3.9 -4.3 -4.6 -5.0 -5.3 -5.6 -6.0 -6.3
3000 -4.3 -4.8 -5.3 -5.8 -6.3 -6.8 -7.3 -7.8 -8.3 -8.9 -9.4
4000 -5.6 -6.3 -7.0 -7.6 -8.3 -9.0 -9.7 -10.4 -11.0 -11.7 -12.4
5000 -6.9 -7.7 -8.6 -9.4 -10.2 -11.1 -11.9 -12.8 -13.6 -14.5 -15.3
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本文链接地址:737NG机组操作手册Flight Crew Operations Manual FCOM 2(25)