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时间:2011-03-14 17:06来源:蓝天飞行翻译 作者:admin
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6000  -8.1  -9.1  -10.1  -11.1  -12.2  -13.2  -14.2  -15.2  -16.2  -17.2  -18.2 
7000  -9.3  -10.4  -11.6  -12.8  -14.0  -15.2  -16.4  -17.5  -18.7  -19.9  -21.1 
8000  -10.4  -11.7  -13.1  -14.5  -15.8  -17.2  -18.5  -19.9  -21.3  -22.6  -24.0 
9000  -11.5  -13.0  -14.5  -16.0  -17.5  -19.1  -20.6  -22.1  -23.6  -25.1  -26.6 
10000  -12.7  -14.3  -16.0  -17.6  -19.3  -20.9  -22.6  -24.2  -25.9  -27.5  -29.2 

Copyright . The Boeing Company. See title page for details.
March 28, 2005  PD.60.9
Performance Dispatch

737-900/CFM56-7B26 Takeoff
FAA Category G 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  45  50  55  60  65  70  75  80  85  90 
15 TW 10 TW 5 TW  -8.6 -5.7 -2.9  -8.5 -5.7 -2.8  -8.4 -5.6 -2.8  -8.3 -5.5 -2.8  -8.2 -5.5 -2.7  -8.1 -5.4 -2.7  -8.0 -5.3 -2.7  -7.9 -5.3 -2.6  -7.8 -5.2 -2.6  -7.7 -5.1 -2.6  -7.6 -5.1 -2.5 
0 10 HW 20 HW  0 1.0 2.0  0 1.0 1.9  0 0.9 1.9  0 0.9 1.8  0 0.8 1.7  0 0.8 1.6  0 0.8 1.5  0 0.7 1.4  0 0.7 1.3  0 0.6 1.2  0 0.6 1.2 
30 HW 40 HW  3.2 4.3  3.0 4.1  2.9 3.9  2.8 3.7  2.6 3.5  2.5 3.4  2.3 3.2  2.2 3.0  2.1 2.8  1.9 2.6  1.8 2.4 

With engine bleed for packs off, increase weight by 600 kg.
With engine anti-ice on, decrease weight by 300 kg.
With engine and wing anti-ice on, decrease weight by 1500 kg (optional system).

Tire Speed Limit Weight Flaps 5 Limit Weight (1000 KG)
OAT (°C)  AIRPORT PRESSURE ALTITUDE (FT) 
0  2000  4000  6000  8000  10000 
54 52 50  86.1 86.1 86.1  85.2 85.7 86.1  78.6 79.2 79.7  72.5 73.0 73.5  66.8 67.2 67.7  62.4 
48 46 44  86.1 86.1 86.1  86.1 86.1 86.1  80.3 80.8 81.4  74.0 74.5 75.0  68.2 68.6 69.1  62.8 63.2 63.6 
42 40 38  86.1 86.1 86.1  86.1 86.1 86.1  82.0 82.5 83.1  75.6 76.1 76.6  69.6 70.1 70.6  64.1 64.5 65.0 
36 34 32  86.1 86.1 86.1  86.1 86.1 86.1  83.7 84.4 85.0  77.2 77.8 78.3  71.1 71.6 72.1  65.4 65.9 66.4 
30 28 26  86.1 86.1 86.1  86.1 86.1 86.1  85.6 86.1 86.1  78.9 79.5 80.1  72.6 73.2 73.7  66.9 67.3 67.8 
24 22 20  86.1 86.1 86.1  86.1 86.1 86.1  86.1 86.1 86.1  80.6 81.2 81.8  74.3 74.8 75.4  68.3 68.8 69.3 
18 16 14  86.1 86.1 86.1  86.1 86.1 86.1  86.1 86.1 86.1  82.5 83.1 83.7  75.9 76.5 77.1  69.9 70.4 70.9 
12 10 -40  86.1 86.1 86.1  86.1 86.1 86.1  86.1 86.1 86.1  84.3 85.0 86.1  77.6 78.2 86.1  71.4 72.0 86.1 

Increase tire speed limit weight by 550 kg per knot headwind. Decrease tire speed limit weight by 1150 kg per knot tailwind.
Copyright . The Boeing Company. See title page for details.
PD.60.10  March 28, 2005
737-900/CFM56-7B26

Performance Dispatch
FAA
Takeoff
Category G Brakes
737 Flight Crew Operations Manual
Brake Energy Limits VMBE
Maximum Brake Energy Speed

OAT (°C)  REFERENCE VMBE (KIAS) 
PRESSURE ALTITUDE (FT) 
-2000  0  2000  4000  6000  8000  10000 
54 50 46  181 182 183  174 175 176  169 170  164 
42 38 34  184 184 185  177 178 178  171 171 172  164 165 166  159 159 160  153 154  146 
30 26 22  187 188 189  179 180 182  173 174 175  167 168 169  161 162 163  155 156 157  148 149 150 
18 14 10  191 193 194  183 185 186  177 178 179  170 172 173  164 165 167  158 159 161  152 153 154 
6 2 -2  196 197 199  188 189 191  181 182 184  174 176 177  168 169 171  162 163 164  156 157 158 
-6 -10  201 203  193 194  186 187  179 180  172 174  166 167  160 161 

Weight Adjusted VMBE
WEIGHT  REFERENCE VMBE (KIAS) 
(1000 KG)  160  165  170  175  180  185  190  195  200  205  210 
 
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