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4000 394.4 355.5 353.1 350.6 350.0 347.4 344.3 341.2 339.4 319.8 297.1
4200 409.0 369.4 366.9 364.4 363.8 361.1 358.0 354.9 353.0 333.1 309.9
4600 435.9 395.0 392.4 389.9 389.2 386.4 383.2 380.0 378.1 357.4 333.4
5000 459.8 417.6 414.9 412.2 411.6 408.7 405.4 402.0 400.0 378.7 354.0
5400 478.8 435.3 432.5 429.8 429.1 426.1 422.7 419.2 417.2 395.2 369.8
5800 497.0 452.3 449.4 446.6 445.9 442.8 439.3 435.8 433.7 411.1 384.9
6200 514.3 468.4 465.5 462.6 461.9 458.8 455.2 451.5 449.4 426.2 399.4
6600 530.9 483.9 481.0 478.0 477.2 474.1 470.4 466.6 464.4 440.7 413.2
7000 546.9 498.9 495.8 492.8 492.0 488.8 485.0 481.2 479.0 454.7 426.6
7400 562.2 513.2 510.1 507.0 506.2 502.9 499.0 495.1 492.8 468.1 439.4
7800 577.0 527.1 523.9 520.7 519.9 516.6 512.6 508.7 506.3 481.1 451.8
8200 591.8 540.9 537.6 534.4 533.6 530.2 526.1 522.1 519.7 494.0 464.2
8600 606.1 554.2 550.9 547.6 546.8 543.2 539.1 535.0 532.6 506.4 476.0
9000 619.3 566.5 563.1 559.8 558.9 555.3 551.2 547.0 544.5 517.8 486.8
9400 631.8 578.0 574.5 571.2 570.3 566.6 562.4 558.1 555.6 528.4 496.9
9800 644.0 589.2 585.7 582.3 581.4 577.7 573.3 569.0 566.4 538.7 506.6
10200 655.7 600.0 596.5 593.0 592.1 588.3 583.9 579.5 576.9 548.8 516.2
10600 666.9 610.5 606.9 603.3 602.4 598.6 594.1 589.7 587.0 558.5 525.5
CLIMB
LIMIT WT
(1000 LB)
592.4 590.2 590.0 589.8 589.7 585.0 578.7 572.6 568.8 527.6 478.0
With engine bleed for packs off, increase field limit weight by 600 lb and climb limit weight by 1800 lb.
With engine and wing anti-ice on, decrease field limit weight by 1700 lb and climb limit weight by 4800 lb.
787 Flight Crew Operations Manual
Performance Dispatch
Takeoff
FAA
Category A Brakes
PD.10.4 Boeing Proprietary
Takeoff Obstacle Limit Weight
Flaps 15
Based on engine bleed for packs on, engine anti-ice on or off and wing anti-ice
off
Sea Level, 29°C & Below, Zero Wind
OAT Adjustment
Pressure Altitude Adjustment
OBSTACLE
HEIGHT
(FT)
REFERENCE OBSTACLE LIMIT WEIGHT (1000 LB)
DISTANCE FROM BRAKE RELEASE (1000 FT)
8 10 12 14 16 18 20 22 24 26 28
10 560.6 620.8 660.4 686.4
50 524.0 576.6 619.0 649.6 668.5 683.5
100 490.3 539.4 578.6 611.9 637.7 654.4 666.9 677.1 685.4 692.2
150 463.0 510.7 550.4 582.4 608.8 629.8 645.6 656.6 665.8 673.6 680.3
200 439.3 487.9 527.3 559.1 584.9 606.6 624.3 638.6 649.2 657.7 665.0
250 418.9 468.7 507.6 539.2 565.1 586.5 605.0 620.3 633.2 643.4 651.4
300 400.5 451.1 490.1 521.6 547.6 569.3 587.6 603.6 617.2 628.8 638.4
350 383.1 435.3 474.4 505.8 531.9 553.8 572.3 588.4 602.5 614.6 625.2
400 367.3 421.0 459.8 491.4 517.5 539.6 558.5 574.6 588.8 601.5 612.5
450 368.1 407.9 446.4 478.1 504.3 526.6 545.7 562.1 576.4 589.1 600.6
500 355.8 394.9 433.9 465.7 492.1 514.4 533.7 550.4 565.0 577.8 589.3
550 344.5 382.7 422.4 454.0 480.6 503.1 522.5 539.4 554.3 567.3 578.8
600 371.3 411.6 443.0 469.8 492.4 512.0 529.1 544.1 557.4 569.1
650 371.3 401.4 432.8 459.4 482.3 502.0 519.2 534.4 547.9 559.9
700 361.7 391.6 423.1 449.7 472.7 492.5 509.9 525.2 538.9 551.1
750 352.6 382.2 413.9 440.5 463.5 483.5 501.0 516.5 530.3 542.6
800 344.0 373.2 405.3 431.7 454.7 474.8 492.4 508.1 522.0 534.5
850 364.5 397.1 423.3 446.3 466.6 484.3 500.0 514.1 526.7
900 365.0 389.2 415.3 438.3 458.5 476.4 492.3 506.5 519.2
950 357.5 381.5 407.8 430.7 450.9 468.9 484.8 499.1 512.0
1000 350.3 374.1 400.8 423.3 443.5 461.5 477.6 492.0 505.0
Obstacle height must be calculated from lowest point of the runway to conservatively account for runway
slope.
OAT (°C) REFERENCE OBSTACLE LIMIT WEIGHT (1000 LB)
420 460 500 540 580 620 660
29 & Below 0 0 0 0 0 0 0
30 -2.5 -2.8 -3.0 -3.3 -3.6 -3.8 -4.1
32 -7.5 -8.3 -9.1 -9.9 -10.7 -11.5 -12.3
34 -12.5 -13.8 -15.2 -16.5 -17.9 -19.2 -20.6
36 -17.5 -19.4 -21.3 -23.1 -25.0 -26.9 -28.8
38 -22.5 -24.9 -27.3 -29.7 -32.2 -34.6 -37.0
40 -27.5 -30.4 -33.4 -36.4 -39.3 -42.3 -45.2
42 -35.2 -39.1 -43.0 -46.8 -50.7 -54.6 -58.5
44 -42.9 -47.7 -52.5 -57.3 -62.1 -67.0 -71.8
46 -50.6 -56.3 -62.1 -67.8 -73.6 -79.3 -85.1
48 -58.2 -64.9 -71.6 -78.3 -85.0 -91.7 -98.4
50 -65.9 -73.6 -81.2 -88.8 -96.4 -104.0 -111.6
ALT (FT) OAT ADJUSTED OBSTACLE LIMIT WEIGHT (1000 LB)
420 460 500 540 580 620 660
S.L. & Below 0 0 0 0 0 0 0
1000 -14.3 -15.6 -17.0 -18.3 -19.6 -20.9 -22.2
2000 -30.3 -33.1 -36.0 -38.9 -41.8 -44.6 -47.5
3000 -46.0 -50.7 -55.5 -60.2 -64.9 -69.6 -74.3
787 Flight Crew Operations Manual
Performance Dispatch
Takeoff
FAA
Category A Brakes
Boeing Proprietary PD.10.5
Takeoff Obstacle Limit Weight
Flaps 15
　
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