曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
Based on engine bleed for packs on, engine anti-ice on or off and wing anti-ice
off
Wind Adjustment
WIND
(KTS)
OAT & ALT ADJUSTED OBSTACLE LIMIT WEIGHT (1000 LB)
420 460 500 540 580 620 660
15 TW -64.7 -63.3 -61.9 -60.6 -59.2 -57.8 -56.5
10 TW -43.1 -42.2 -41.3 -40.4 -39.5 -38.6 -37.6
5 TW -21.6 -21.1 -20.6 -20.2 -19.7 -19.3 -18.8
0 0 0 0 0 0 0 0
10 HW 6.8 6.3 5.7 5.2 4.7 4.2 3.6
20 HW 13.6 12.5 11.5 10.4 9.4 8.3 7.3
30 HW 20.4 18.8 17.2 15.6 14.1 12.5 10.9
40 HW 27.2 25.1 23.0 20.8 18.7 16.6 14.5
With engine bleed for packs off, increase weight by 600 lb.
With engine and wing anti-ice on, decrease weight by 3100 lb.
787 Flight Crew Operations Manual
Performance Dispatch
Takeoff
FAA
Category A Brakes
PD.10.6 Boeing Proprietary
TakeoffBrake Energy Limits VMBE
Maximum Brake Energy Speed
Weight Adjusted VMBE
OAT
(°C)
REFERENCE VMBE (KIAS)
PRESSURE ALTITUDE (FT)
-2000 0 2000 4000 6000 8000
54 198 190
50 198 191 184
46 199 191 185 178
42 200 192 185 179 172
38 200 193 186 180 173 167
34 202 194 187 180 174 168
30 203 194 188 181 175 169
26 205 196 189 182 176 170
22 207 198 190 184 177 171
18 208 199 192 185 178 172
14 210 201 194 186 180 173
10 210 203 195 188 181 174
6 210 205 197 190 183 176
2 210 207 199 191 184 177
-2 210 209 201 193 186 179
-6 210 210 202 195 188 180
-10 210 210 204 197 189 182
WEIGHT
(1000 LB)
REFERENCE VMBE (KIAS)
160 165 170 175 180 185 190 195 200 205 210
380 194 200 207 210 210 210 210 210 210 210 210
400 187 193 200 206 210 210 210 210 210 210 210
420 182 188 194 200 206 210 210 210 210 210 210
440 177 183 189 194 200 206 210 210 210 210 210
460 173 178 184 189 195 201 206 210 210 210 210
480 169 174 179 185 190 196 201 207 210 210 210
500 165 170 175 181 186 191 196 202 207 210 210
520 162 167 172 177 182 187 192 197 202 207 210
540 158 163 168 173 178 183 188 193 198 203 207
560 155 160 165 169 174 179 184 189 193 198 203
580 152 157 161 166 171 175 180 185 189 194 199
600 149 154 159 163 168 172 177 181 186 190 195
620 147 151 156 160 165 169 173 178 182 187 191
640 145 149 153 158 162 166 170 175 179 183 188
660 143 147 151 155 159 163 168 172 176 180 184
Increase VMBE by 3 knots per 1% uphill runway slope. Decrease VMBE by 5 knots per 1% downhill runway
slope.
Increase VMBE by 5 knots per 10 knots headwind. Decrease VMBE by 21 knots per 10 knots tailwind.
Decrease VMBE by 10 knots for one brake deactivated and 21 knots for two brakes deactivated.
Decrease climb weight improvement by 3500 lb for each knot V1 exceeds VMBE.
Determine normal V1, VR, V2 speeds for lower brake release weight.
787 Flight Crew Operations Manual
Performance Dispatch
Takeoff
FAA
Category A Brakes
Boeing Proprietary PD.10.7
Takeoff Speeds
Flaps 15
V1, VR, V2 for Max Takeoff Thrust
V1, VR, V2 Adjustments*
Slope and Wind V1 Adjustments*
WEIGHT
(1000 LB)
FLAPS 15
V1 VR V2
660 156 162 168
640 153 159 165
620 151 156 163
600 148 153 161
580 145 151 158
560 142 148 156
540 139 144 153
520 135 141 150
500 132 138 148
480 129 135 145
460 125 132 142
440 121 128 139
420 117 125 136
400 113 121 134
380 109 118 130
360 104 114 127
340 100 110 124
Check V1(MCG) and minimum VR.
TEMP V1 VR V2
PRESS ALT (FT) PRESS ALT (FT) PRESS ALT (FT)
°C °F -2000 0 1000 2000 3000 -2000 0 1000 2000 3000 -2000 0 1000 2000 3000
50 122 4 5 6 7 8 2 2 3 3 4 -1 -1 -2 -2 -2
40 104 1 2 3 4 5 1 1 2 2 3 0 -1 -1 -1 -1
30 86 0 0 1 2 4 0 0 1 1 2 0 0 0 -1 -1
20 68 0 0 1 1 2 0 0 0 1 1 0 0 0 0 -1
-40 -40 0 0 1 1 2 0 0 0 1 1 0 0 0 0 -1
WEIGHT
(1000 LB)
SLOPE (%) WIND (KTS)
-2 -1 0 1 2 -15 -10 -5 0 10 20 30 40
660 -5 -2 0 2 4 -2 -1 -1 0 0 1 1 2
620 -4 -2 0 2 4 -2 -1 0 0 0 1 1 2
580 -4 -2 0 2 3 -2 -1 0 0 0 1 1 2
540 -3 -1 0 2 3 -2 -1 0 0 0 1 1 2
500 -3 -1 0 2 3 -2 -1 0 0 0 1 1 2
460 -3 -1 0 2 3 -2 -1 0 0 0 1 1 2
420 -3 -1 0 2 3 -2 -1 0 0 1 1 2 2
380 -3 -1 0 2 3 -2 -1 0 0 1 1 2 2
340 -3 -1 0 2 3 -2 -1 0 0 1 1 2 2
*V1 not to exceed VR
787 Flight Crew Operations Manual
Performance Dispatch
Takeoff
FAA
Category A Brakes
PD.10.8 Boeing Proprietary
Takeoff Speeds
Flaps 15
V1(MCG), Minimum VR
Max Takeoff Thrust
TEMP PRESSURE ALTITUDE (FT)
-2000 0 1000 2000 3000
°C °F V1(MCG) Min VR V1(MCG) Min VR V1(MCG) Min VR V1(MCG) Min VR V1(MCG) Min VR
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
787机组操作手册Flight Crew Operations Manual 1(42)
