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TIME
(HR:MIN)
FUEL
(1000 LB)
TIME
(HR:MIN)
FUEL
(1000 LB)
TIME
(HR:MIN)
400 11.7 0:57 11.2 0:57 10.8 0:56 10.5 0:57 10.5 0:58
800 24.4 1:51 23.6 1:49 22.9 1:47 22.3 1:47 22.1 1:47
1200 37.0 2:45 35.9 2:41 35.0 2:38 34.1 2:37 33.8 2:37
1600 49.7 3:39 48.3 3:34 47.0 3:29 45.9 3:27 45.5 3:27
2000 62.4 4:33 60.7 4:26 59.1 4:20 57.7 4:17 57.1 4:17
2400 74.6 5:28 72.5 5:20 70.6 5:12 69.0 5:08 68.2 5:06
2800 86.7 6:23 84.3 6:13 82.2 6:04 80.3 5:58 79.2 5:56
3200 98.7 7:19 95.9 7:08 93.5 6:57 91.3 6:50 90.0 6:47
3600 110.5 8:16 107.2 8:03 104.5 7:51 102.1 7:42 100.6 7:37
4000 122.3 9:13 118.5 8:58 115.5 8:44 112.8 8:34 111.1 8:28
4400 133.6 10:12 129.3 9:55 126.1 9:39 123.1 9:27 121.2 9:20
4800 144.9 11:10 140.1 10:52 136.6 10:34 133.4 10:21 131.3 10:11
5200 155.9 12:10 150.7 11:49 146.9 11:30 143.5 11:15 141.1 11:04
5600 166.8 13:10 161.2 12:48 157.1 12:27 153.4 12:10 150.8 11:56
6000 177.6 14:11 171.6 13:46 167.3 13:24 163.2 13:04 160.4 12:49
6400 188.0 15:13 181.7 14:47 177.1 14:22 172.8 14:01 169.8 13:44
6800 198.4 16:16 191.8 15:47 186.9 15:20 182.4 14:57 179.1 14:38
7200 208.6 17:19 201.7 16:48 196.5 16:20 191.8 15:55 188.3 15:33
7600 218.6 18:24 211.4 17:50 206.0 17:20 201.0 16:53 197.3 16:29
8000 228.6 19:29 221.1 18:53 215.4 18:20 210.2 17:51 206.3 17:25
787 Flight Crew Operations Manual
Performance Inflight
All Engine
FAA
Category A Brakes
PI.11.6 Boeing Proprietary
All EngineLong Range Cruise Enroute Fuel and Time - High Altitude
Fuel Required Adjustment (1000 LB)
Long Range Cruise Wind-Altitude Trade
Descent at .84/310/250 KIAS
REFERENCE FUEL REQUIRED
(1000 LB)
WEIGHT AT CHECK POINT (1000 LB)
300 400 500 600 700
20 -4.3 -1.8 0.0 13.8 69.2
40 -8.7 -4.3 0.0 19.4 80.2
60 -13.1 -6.7 0.0 24.5 89.9
80 -17.6 -9.1 0.0 29.1 98.4
100 -22.1 -11.5 0.0 33.1 105.6
120 -26.7 -13.8 0.0 36.6 111.6
140 -31.3 -16.1 0.0 39.5 116.4
160 -36.0 -18.3 0.0 41.9 119.9
180 -40.7 -20.5 0.0 43.7 122.1
200 -45.5 -22.6 0.0 45.0 123.2
220 -50.4 -24.7 0.0 45.7 123.0
240 -55.2 -26.7 0.0 45.9 121.5
PRESSURE
ALTITUDE
(1000 FT)
CRUISE WEIGHT (1000 LB)
660 620 580 540 500 460 420 380 340 300
43 68 25 4 0 9
41 60 24 4 0 6 22
39 50 20 4 0 5 18 37
37 38 15 2 0 4 16 32 52
35 54 27 10 1 0 5 15 30 47 66
33 17 5 0 0 6 16 29 44 62 79
31 2 0 1 8 17 29 43 59 75 91
29 0 3 10 19 30 43 57 72 87 102
27 5 12 22 32 44 57 71 84 98 110
25 16 25 35 46 58 70 83 95 107 118
The above wind factor table is for calculation of wind required to maintain present range capability at new
pressure altitude, i.e., break-even wind.
Method:
1. Read wind factors for present and new altitudes from table.
2. Determine difference (new altitude wind factor minus present altitude wind factor);
This difference may be negative or positive.
3. Break-even wind at new altitude is present altitude wind plus difference from step 2.
PRESSURE ALT (1000 FT) 25 27 29 31 33 35 37 39 41 43
DISTANCE (NM) 93 100 107 114 119 124 130 136 142 148
TIME (MINUTES) 19 20 21 22 23 23 24 25 25 26
787 Flight Crew Operations Manual
Performance Inflight
All Engine
FAA
Category A Brakes
Boeing Proprietary PI.11.7
All EngineHolding
Flaps Up
WEIGHT
(1000 LB)
PRESSURE ALTITUDE (FT)
1500 5000 10000 15000 20000 25000 30000 35000 40000 43000
660
EPR 1.023 1.031 1.046 1.059 1.075 1.123 1.197
KIAS 259 260 261 277 302 306 310
FF/ENG 9570 9500 9210 9310 9760 9970 10350
620
EPR 1.020 1.027 1.040 1.056 1.067 1.109 1.171 1.363
KIAS 251 252 253 262 287 296 300 279
FF/ENG 8980 8900 8610 8620 9000 9260 9530 10110
580
EPR 1.017 1.023 1.035 1.053 1.064 1.095 1.149 1.276
KIAS 243 244 245 248 269 285 289 279
FF/ENG 8410 8310 8230 7980 8220 8550 8780 9080
540
EPR 1.014 1.020 1.030 1.047 1.060 1.078 1.129 1.216
KIAS 234 235 236 237 252 275 278 279
FF/ENG 8000 7730 7780 7540 7640 7870 8050 8330
500
EPR 1.012 1.016 1.026 1.040 1.056 1.068 1.111 1.178 1.410
KIAS 226 226 227 228 235 259 267 271 249
FF/ENG 7440 7330 7200 6970 6960 7130 7340 7580 8380
460
EPR 1.007 1.011 1.020 1.033 1.053 1.063 1.094 1.150 1.288
KIAS 219 219 219 219 220 238 255 259 249
FF/ENG 6890 6780 6630 6560 6360 6510 6660 6840 7270
420
EPR 1.003 1.007 1.013 1.024 1.040 1.058 1.073 1.125 1.213 1.361
KIAS 213 213 213 213 213 220 243 246 249 232
FF/ENG 6520 6250 6100 6000 5940 5820 6000 6130 6550 6920
380
EPR 1.000 1.002 1.007 1.016 1.029 1.049 1.066 1.104 1.170 1.250
　
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