Boeing 787-8 - Page 221

787 Flight Crew Operations Manual
DO NOT USE FOR FLIGHT
Performance Dispatch
Landing
787-8/
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D615Z003-TBC PD.12.5
Quick Turnaround Limit Weight
Flaps 30 Limit Weight (1000 LB)
AIRPORT
OAT
AIRPORT PRESSURE ALTITUDE (FT)
°C °F -2000 0 2000 4000 6000 8000 10000
54 129 405.7 391.3
50 122 408.2 393.8 379.3
45 113 411.5 396.9 382.3 367.9
40 104 414.8 400.0 385.4 370.8 356.8
35 95 418.3 403.3 388.6 373.9 359.7 345.6
30 86 421.9 406.7 391.9 377.0 362.6 348.6 334.6
25 77 425.7 410.1 395.2 380.2 365.6 351.5 337.5
20 68 429.5 413.7 398.6 383.5 368.7 354.6 340.4
15 59 433.5 417.3 402.0 386.9 372.0 357.7 343.5
10 50 437.6 421.2 405.6 390.4 375.4 360.9 346.6
5 41 441.8 425.2 409.3 394.0 378.8 364.3 350.0
0 32 446.1 429.2 413.0 397.5 382.4 367.7 353.4
-5 23 450.5 433.5 416.9 401.2 385.9 371.2 357.0
-10 14 455.0 437.9 421.0 405.0 389.6 374.7 360.2
-15 5 459.7 442.4 425.3 408.9 393.4 378.3 363.6
-20 -4 464.5 447.0 429.7 413.0 397.3 382.0 367.1
-30 -22 475.7 456.7 439.0 421.6 405.3 389.8 374.5
-40 -40 491.5 467.1 449.0 431.0 413.9 398.1 382.3
-50 -58 503.2 482.3 459.5 441.2 423.4 406.7 390.0
-54 -65 508.0 488.8 463.9 445.4 427.4 410.1 393.1
Increase weight by 3700 lb per 1% uphill slope. Decrease weight by 9200 lb per 1% downhill slope.
Increase weight by 10400 lb per 10 knots headwind. Decrease weight by 61200 lb per 10 knots tailwind.
Decrease weight by TBS lb when one brake is deactivated. Decrease weight by TBS 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.
February 15, 2010