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10°C, decrease gradient by 0.6%.
787 Flight Crew Operations Manual
Performance Dispatch
Landing
FAA
Category A Brakes
Boeing Proprietary PD.12.5
Quick Turnaround Limit Weight
Flaps 30 Limit Weight (1000 LB)
AIRPORT OAT AIRPORT PRESSURE ALTITUDE (FT)
°C °F 0 2000 4000 6000 8000
54 129 519
50 122 522 502
45 113 526 506 487
40 104 531 511 491 472
35 95 536 515 495 476 458
30 86 540 520 499 480 462
25 77 545 524 504 484 466
20 68 550 529 508 488 470
15 59 555 534 513 493 474
10 50 561 539 518 497 478
5 41 566 544 523 502 482
0 32 572 550 528 507 487
-5 23 577 555 533 512 492
-10 14 583 561 539 517 497
-15 5 589 567 544 523 502
-20 -4 595 573 550 528 507
-30 -22 608 585 562 540 518
-40 -40 622 598 575 552 530
-50 -58 636 612 588 565 543
-54 -65 642 618 594 571 548
Increase weight by 6200 lb per 1% uphill slope. Decrease weight by 7700 lb per 1% downhill slope.
Increase weight by 16500 lb per 10 knots headwind. Decrease weight by 56400 lb per 10 knots tailwind.
Decrease weight by 23800 lb when one brake is deactivated. Decrease weight by 77800 lb when two brakes
are deactivated.
After landing at weights exceeding those shown above, adjusted for slope and wind, wait at least 65 minutes
and check that wheel thermal plugs have not melted before executing a takeoff.
As an alternate procedure, no waiting period is required if the BRAKE TEMP advisory message on EICAS is
not displayed 10 to 15 minutes after parking.
787 Flight Crew Operations Manual
Performance Dispatch
Landing
FAA
Category A Brakes
PD.12.6 Boeing Proprietary
Intentionally
Blank
787 Flight Crew Operations Manual
Performance Dispatch Chapter PD
Gear Down Section 13
FAA
Category A Brakes
FAST-Doc PI/PD Template 9/1/99
Boeing Proprietary PD.13.1
PD.13 Performance Dispatch-Gear DownGEAR DOWN
Gear DownTakeoff Climb Limit Weight
Flaps 15
AIRPORT OAT TAKEOFF CLIMB LIMIT WEIGHT (1000 LB)
AIRPORT PRESSURE ALTITUDE (FT)
°C °F 0 1000 2000 3000
54 129 394.2 384.9 377.9 370.6
52 126 405.2 387.1 377.9 370.6
50 122 415.8 397.5 379.9 370.6
48 118 426.1 407.6 389.8 372.6
46 115 436.7 417.6 399.3 382.1
44 111 446.9 427.5 409.0 391.1
42 108 457.0 437.2 418.2 400.1
40 104 467.2 446.9 427.7 409.2
38 100 478.0 456.6 436.7 418.0
36 97 488.8 467.6 446.0 426.8
34 93 499.3 478.6 457.2 435.6
32 90 509.9 489.2 468.5 447.1
30 86 520.5 499.8 479.3 458.3
28 82 530.6 510.4 489.9 469.1
26 79 540.8 520.5 500.2 479.7
24 75 545.9 530.4 510.1 489.9
22 72 545.9 535.3 520.1 500.0
20 68 545.9 535.3 524.9 509.7
18 64 545.9 535.3 524.9 514.3
16 61 545.9 535.3 524.9 514.3
14 57 545.9 535.3 524.7 514.1
12 54 545.9 535.3 524.7 514.1
10 50 545.9 535.3 524.7 514.1
With engine bleeds for packs off, increase weight by 200 lb.
With engine anti-ice on, decrease weight by 8800 lb.
With engine and wing anti-ice on, decrease weight by 10800 lb.
787 Flight Crew Operations Manual
Performance Dispatch
Gear Down
FAA
Category A Brakes
PD.13.2 Boeing Proprietary
GEAR DOWN
Gear DownLanding Climb Limit Weight
Valid for approach with flaps 20 and landing with flaps 25 or 30
AIRPORT OAT LANDING CLIMB LIMIT WEIGHT (1000 LB)
AIRPORT PRESSURE ALTITUDE (FT)
°C °F 0 1000 2000 3000
54 129 465.3
52 126 476.5 458.9
50 122 487.7 470.1 452.5
48 118 498.6 481.2 463.3 444.8
46 115 509.3 491.9 473.8 454.0
44 111 520.3 502.3 484.0 463.0
42 108 531.8 512.3 493.7 471.8
40 104 542.8 522.2 503.0 480.4
38 100 551.8 531.7 512.0 488.7
36 97 560.2 539.8 520.0 496.7
34 93 568.5 547.8 527.6 504.4
32 90 576.5 555.3 534.9 511.4
30 86 582.1 562.6 541.7 518.3
28 82 584.5 568.1 548.2 524.7
26 79 584.6 570.1 553.5 530.6
24 75 584.7 570.2 555.7 535.6
22 72 584.7 570.3 555.7 537.6
20 68 584.8 570.4 555.8 537.7
18 64 584.9 570.5 555.9 537.7
16 61 585.0 570.5 556.0 537.8
14 57 585.1 570.6 556.1 537.9
12 54 585.3 570.7 556.2 538.0
10 50 585.4 570.8 556.3 538.1
-40 -40 587.9 573.1 558.5 540.3
Based on engine bleed for 2 packs on, APU on or off, engine anti-ice on or off and wing anti-ice off.
With engine bleed for packs off, increase weight by 1500 lb.
With engine and wing anti-ice on, decrease weight by 2400 lb.
When operating in icing conditions during any part of the flight with forecast landing temperature below
10°C, decrease weight by 58000 lb.
787 Flight Crew Operations Manual
　
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