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Performance Dispatch
Gear Down
FAA
Category A Brakes
Boeing Proprietary PD.13.3
GEAR DOWN
Gear DownTakeoff Obstacle Limit Weight
Based on engine bleed for packs on, engine anti-ice off and wing anti-ice off
Flaps 15
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
10 545.1 581.3
50 511.4 546.8 570.5 587.9
100 478.0 517.6 542.6 560.7 574.6 585.4 594.1
150 451.9 491.7 520.6 540.1 554.9 566.7 576.2 584.0 590.6
200 430.3 470.5 499.9 522.3 538.2 550.8 561.2 569.7 576.9
250 411.8 451.8 482.0 505.1 523.3 536.8 547.8 557.0 564.8
300 393.9 435.4 466.1 489.8 508.7 524.0 535.7 545.4 553.8
350 377.1 420.6 451.5 475.9 495.3 511.2 524.3 534.7 543.4
400 374.1 407.2 438.2 463.0 483.0 499.4 513.0 524.6 533.8
450 361.1 394.1 426.0 451.0 471.5 488.4 502.5 514.4 524.6
500 349.1 381.7 414.7 439.9 460.7 478.0 492.5 504.8 515.5
550 370.0 404.2 429.6 450.6 468.2 483.1 495.8 506.7
600 368.4 393.9 419.8 441.0 458.9 474.1 487.1 498.4
650 358.6 384.1 410.6 432.0 450.1 465.5 478.8 490.4
700 349.3 374.6 402.0 423.4 441.7 457.3 470.9 482.7
750 340.4 365.6 393.5 415.3 433.7 449.5 463.3 475.4
800 364.6 385.4 407.5 426.0 442.0 456.0 468.3
850 356.7 377.5 400.2 418.7 434.9 449.0 461.4
900 349.1 369.8 393.1 411.7 428.0 442.2 454.8
950 341.8 362.4 386.1 405.1 421.3 435.7 448.4
1000 361.7 379.2 398.8 414.9 429.4 442.2
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)
380 420 460 500 540 580 620
29 & Below 0 0 0 0 0 0 0
30 -3.2 -3.5 -3.8 -4.0 -4.3 -4.6 -4.9
32 -9.7 -10.5 -11.3 -12.1 -12.9 -13.7 -14.6
34 -16.1 -17.5 -18.8 -20.2 -21.5 -22.9 -24.3
36 -22.6 -24.5 -26.4 -28.3 -30.2 -32.1 -34.0
38 -29.0 -31.4 -33.9 -36.3 -38.8 -41.2 -43.7
40 -35.5 -38.4 -41.4 -44.4 -47.4 -50.4 -53.4
42 -40.5 -44.5 -48.5 -52.5 -56.5 -60.5 -64.4
44 -45.6 -50.6 -55.6 -60.6 -65.6 -70.6 -75.5
46 -50.7 -56.7 -62.7 -68.7 -74.7 -80.6 -86.6
48 -55.8 -62.8 -69.7 -76.7 -83.7 -90.7 -97.7
50 -60.8 -68.8 -76.8 -84.8 -92.8 -100.8 -108.8
ALT (FT) OAT ADJUSTED OBSTACLE LIMIT WEIGHT (1000 LB)
380 420 460 500 540 580 620
S.L. & Below 0 0 0 0 0 0 0
1000 -12.7 -14.1 -15.6 -17.0 -18.4 -19.8 -21.3
2000 -27.8 -30.9 -33.9 -37.0 -40.0 -43.1 -46.1
3000 -42.9 -47.6 -52.3 -57.0 -61.6 -66.3 -71.0
787 Flight Crew Operations Manual
Performance Dispatch
Gear Down
FAA
Category A Brakes
PD.13.4 Boeing Proprietary
GEAR DOWN
Gear DownTakeoff Obstacle Limit Weight
Based on engine bleed for packs on, engine anti-ice off and wing anti-ice off
Wind Adjustment
Long Range Cruise Altitude Capability
Max Climb Thrust, 300 ft/min residual rate of climb
WIND
(KTS)
OAT & ALT ADJUSTED OBSTACLE LIMIT WEIGHT (1000 LB)
380 420 460 500 540 580 620
15 TW -56.1 -53.5 -51.0 -48.4 -45.8 -43.2 -40.6
10 TW -37.4 -35.7 -34.0 -32.2 -30.5 -28.8 -27.0
5 TW -18.7 -17.8 -17.0 -16.1 -15.3 -14.4 -13.5
0 0 0 0 0 0 0 0
10 HW 6.1 5.4 4.7 4.0 3.3 2.6 1.9
20 HW 12.1 10.7 9.3 7.9 6.5 5.2 3.8
30 HW 18.2 16.1 14.0 11.9 9.8 7.7 5.6
40 HW 24.3 21.5 18.7 15.9 13.1 10.3 7.5
With engine bleed for packs off, increase weight by 700 lb.
With engine anti-ice on, decrease weight by 2200 lb.
With engine and wing anti-ice on, decrease weight by 3700 lb.
WEIGHT
(1000 LB)
PRESSURE ALTITUDE (FT)
ISA+10°C
& BELOW ISA+15°C ISA+20°C
660 13100 10400 7300
640 14500 12000 9000
620 16000 13500 10800
600 17500 15100 12400
580 19000 16600 14000
560 20500 18200 15600
540 21800 19700 17300
520 23200 21100 19000
500 24500 22500 20600
480 25600 24000 22000
460 26400 25300 23500
440 27300 26200 25000
420 28300 27100 25900
400 29300 28000 26900
380 30300 29000 27900
360 31500 30100 28900
340 33100 31300 30000
320 34700 33000 31300
300 36300 34700 33100
787 Flight Crew Operations Manual
Performance Dispatch
Gear Down
FAA
Category A Brakes
Boeing Proprietary PD.13.5
GEAR DOWN
Gear DownLong Range Cruise Trip Fuel and Time
Ground to Air Miles Conversion
Reference Fuel and Time Required
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
　
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