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-5 23 440 610 785
-10 14 430 600 770
For more extensive than normal crew usage, add 1.2 psi/person/minute.
787 Flight Crew Operations Manual
Performance Dispatch
Enroute
FAA
Category A Brakes
PD.11.8 Boeing Proprietary
ENGINE INOP
MAX CONTINUOUS THRUST
Net Level Off Weight
Anti-Ice Adjustment
PRESSURE
ALTITUDE
(1000 FT)
LEVEL OFF WEIGHT (1000 LB)
ISA +10°C
& BELOW ISA +15°C ISA+ 20°C
29 334.7
28 351.7 334.3
27 369.3 351.6 333.6
26 387.6 369.5 351
25 406.6 388.2 369.1
24 424.1 405.1 385
23 442.3 422.5 401.5
22 461.1 440.7 418.5
21 480.5 459.4 436.1
20 500.6 478.9 454.4
19 520.3 498 472.9
18 540.5 517.7 492
17 561.3 538 511.8
16 582.6 558.9 532.1
15 600.6 576.5 548.5
14 619.1 594.2 565.3
13 637.6 612.2 582.4
12 656.4 630 599.9
11 673.8 645.7 614.3
10 661.3 627.6
9 639.8
8 652.1
7 664.2
ANTI-ICE
CONFIGURATION
LEVEL OFF WEIGHT ADJUSTMENT (1000 LB)
PRESSURE ALTITUDE (1000 FT)
10 12 14 16 18 20 22 24 26
ENGINE ONLY -9.5 -8.4 -7.1 -5.9 -4.2 -2.4 -3.1 -2.5 -2.0
ENGINE AND WING -12.6 -11.4 -10.4 -9.2 -7.5 -5.6 -7.0 -6.4 -6.0
787 Flight Crew Operations Manual
Performance Dispatch
Enroute
FAA
Category A Brakes
Boeing Proprietary PD.11.9
ALL ENGINES
Long Range Cruise Critical Fuel Reserves
Ground to Air Miles Conversion
Critical Fuel (1000 LB)
AIR DISTANCE (NM) GROUND
DISTANCE
(NM)
AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS) TAILWIND COMPONENT (KTS)
100 80 60 40 20 20 40 60 80 100
286 264 244 227 213 200 189 178 169 161 154
568 524 487 454 425 400 378 358 340 323 309
851 785 729 680 638 600 567 537 510 486 463
1133 1046 971 907 850 800 756 716 680 648 618
1415 1307 1214 1133 1062 1000 945 895 850 810 773
1697 1567 1456 1359 1275 1200 1134 1074 1021 972 928
1980 1828 1698 1586 1487 1400 1323 1253 1191 1134 1083
2262 2089 1941 1812 1699 1600 1512 1432 1361 1297 1238
2544 2350 2183 2038 1912 1800 1701 1611 1531 1459 1393
AIR
DISTANCE
(NM)
WEIGHT AT CRITICAL POINT (1000 LB)
340 380 420 460 500 540 580 620 660
200 8.8 9.2 9.6 9.9 10.3 10.6 10.9 11.3 11.8
300 13.0 13.6 14.1 14.5 15.1 15.5 16.0 16.6 17.2
400 17.1 17.9 18.6 19.2 20.0 20.5 21.1 21.8 22.6
500 21.3 22.3 23.1 23.9 24.9 25.4 26.2 27.1 28.0
600 25.4 26.6 27.6 28.5 29.7 30.3 31.2 32.2 33.3
700 29.5 30.9 32.0 33.1 34.4 35.2 36.2 37.4 38.7
800 33.6 35.1 36.5 37.7 39.2 40.1 41.2 42.5 44.0
900 37.6 39.4 40.9 42.3 43.9 45.0 46.2 47.7 49.3
1000 41.7 43.7 45.4 46.8 48.7 49.9 51.2 52.7 54.5
1100 45.7 47.9 49.8 51.4 53.3 54.7 56.1 57.8 59.8
1200 49.8 52.0 54.1 55.9 58.0 59.6 61.0 62.9 65.0
1300 53.9 56.2 58.5 60.4 62.7 64.4 65.9 67.9 70.2
1400 57.9 60.3 62.8 64.9 67.3 69.2 70.8 73.0 75.3
1500 62.0 64.5 67.2 69.3 71.9 74.0 75.7 78.0 80.5
1600 66.0 68.6 71.4 73.8 76.5 78.8 80.6 83.0 85.6
1700 70.1 72.6 75.7 78.3 81.1 83.5 85.5 88.0 90.7
1800 74.2 76.7 80.0 82.7 85.7 88.3 90.4 92.9 95.8
Based on: Emergency descent to 10000 ft, level cruise at 10000 ft, 250 KIAS descent to 1500 ft. 15 minute hold
at 1500 ft. One missed approach; approach and land. Includes 5% allowance for wind errors.
Increase fuel required 0.8% for each 10°C above ISA.
If icing conditions exist, increase fuel required by 8% to account for engine and wing anti-ice on (4%) and ice
accumulation on unheated surfaces (4%).
Allowance for performance deterioration not included.
Compare the fuel required for all engine and engine inoperative critical fuel reserves and use the higher of
the two.
787 Flight Crew Operations Manual
Performance Dispatch
Enroute
FAA
Category A Brakes
PD.11.10 Boeing Proprietary
ENGINE INOP
Long Range Cruise Critical Fuel Reserves
Ground to Air Miles Conversion
Critical Fuel (1000 LB)
AIR DISTANCE (NM) GROUND
DISTANCE
(NM)
AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS) TAILWIND COMPONENT (KTS)
100 80 60 40 20 20 40 60 80 100
286 263 244 227 213 200 189 179 170 161 154
572 527 488 455 426 400 377 357 339 322 307
859 791 732 682 638 600 566 535 508 483 461
1146 1054 977 910 851 800 754 714 677 644 615
1432 1318 1221 1137 1064 1000 943 892 847 806 768
1719 1582 1465 1365 1277 1200 1132 1071 1016 967 922
2006 1846 1710 1592 1490 1400 1320 1249 1185 1128 1075
2292 2110 1954 1820 1703 1600 1509 1428 1355 1289 1229
2579 2373 2198 2047 1916 1800 1697 1606 1524 1450 1382
AIR
DISTANCE
(NM)
WEIGHT AT CRITICAL POINT (1000 LB)
　
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