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)
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737NG机组操作手册Flight Crew Operations Manual FCOM 1(129)