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FLAPS DRIVE
(FLAPS LESS
THAN OR EQUAL
TO 5)
VREF30+ 40 8320 +180/-180 300 -480 1960 610 -390 480
FLAPS PRIMARY
FAIL VREF20 7530 +180/-180 250 -470 1910 610 -390 530
FLAP/SLAT
CONTROL VREF20 6900 +160/160 230 -440 1820 550 -350 450
FLIGHT
CONTROL MODE VREF20 7790 +190/-190 270 -480 1950 650 -410 570
HYD PRESS
SYS C VREF20 7530 +180/-180 250 -470 1910 610 -390 530
HYD PRESS SYS
L+C VREF30+ 20 10430 +220/-220 360 -650 2560 1300 -730 760
HYD PRESS SYS
L+R VREF30+ 20 13990 +240/-240 400 -920 3550 3300 -1450 1000
HYD PRESS SYS
R+C VREF30+ 20 10570 +230/-230 370 -660 2580 1340 -750 780
PITCH UP
AUTHORITY
(FLAPS 5)
VREF30+ 40 8180 +170/-170 280 -470 1950 570 -370 430
PITCH UP
AUTHORITY
(FLAPS 20)
VREF30+ 20 7220 +160/-160 240 -450 1880 550 -350 430
PRI FLIGHT
COMPUTERS VREF20 7790 +190/-190 270 -480 1950 650 -410 570
SLATS DRIVE VREF30+ 30 7960 +170/-170 270 -480 1920 600 -390 460
STABILIZER VREF30+ 20 7450 +160/-160 250 -460 1880 580 -370 460
Actual (unfactored) distances are shown.
Includes distance from 50 ft above threshold to stop (1000 ft of air distance).
Assumes maximum manual braking and maximum available reverse thrust.
787 Flight Crew Operations Manual
Performance Inflight
Advisory Information
FAA
Category A Brakes
PI.12.8 Boeing Proprietary
ADVISORY INFORMATION
Advisory InformationLanding 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) -2000 0 2000 4000 6000 8000
54 129 570.0 537.3
52 126 583.3 550.2
50 122 597.2 562.9 520.9
48 118 611.1 575.4 533.6
46 115 625.2 587.8 545.7 502.4
44 111 638.9 601.5 557.7 512.0
42 108 651.9 615.9 569.4 521.5 484.3
40 104 663.8 629.6 580.7 531.0 492.5
38 100 673.3 641.1 592.5 540.0 500.1 462.2
36 97 682.2 658.2 604.0 549.1 507.7 469.4
34 93 691.0 669.1 613.7 558.0 515.2 476.4
32 90 691.2 678.9 623.1 566.4 523.0 483.5
30 86 691.3 686.2 632.1 574.8 531.1 490.5
28 82 691.5 688.7 640.7 583.1 539.0 497.9
26 79 691.6 688.8 650.1 590.8 546.8 505.5
24 75 691.7 688.9 655.3 598.0 554.4 511.9
22 72 691.9 689.0 655.5 603.9 559.0 516.1
20 68 692.0 689.1 655.6 606.3 561.3 519.4
18 64 692.0 689.2 655.9 606.4 563.6 523.0
16 61 692.0 689.3 656.1 606.4 564.8 526.9
14 57 692.1 689.4 656.3 606.6 564.9 529.7
12 54 692.2 689.6 656.5 606.7 564.9 530.6
10 50 692.3 689.7 656.7 606.8 565.0 530.7
-40 -40 694.9 692.7 659.6 609.5 567.5 532.9
Based on engine bleed for 2 packs on, engine anti-ice on or off and wing anti-ice off.
With engine bleed for packs off, increase weight by 2000 lb.
With engine and wing anti-ice on, decrease weight by 3400 lb.
When operating in icing conditions during any part of the flight with forecast landing temperature below
10°C, decrease weight by 45400 lb.
787 Flight Crew Operations Manual
Performance Inflight
Advisory Information
FAA
Category A Brakes
Boeing Proprietary PI.12.9
ADVISORY INFORMATION
Advisory InformationRecommended Brake Cooling Schedule
Reference Brake Energy (Millions of Foot Pounds)
BRAKES ON SPEED (KIAS)
80 100 120 140 160 180
WEIGHT
(1000 LB)
OAT
(°C)
PRESSURE ALTITUDE (1000 FT)
0 4 8 0 4 8 0 4 8 0 4 8 0 4 8 0 4 8
660
0 17.3 19.0 21.1 26.1 29.0 32.5 36.3 40.7 45.9 47.8 53.8 60.8 60.3 68.0 77.0 73.1 82.3 92.8
10 17.8 19.6 21.8 26.9 30.0 33.6 37.5 42.1 47.4 49.4 55.6 62.9 62.3 70.2 79.4 75.4 84.9 95.6
15 18.1 20.0 22.2 27.4 30.5 34.2 38.2 42.8 48.2 50.2 56.6 63.9 63.4 71.4 80.7 76.7 86.2 97.0
20 18.4 20.3 22.5 27.8 31.0 34.7 38.8 43.5 49.0 51.1 57.5 65.0 64.4 72.5 81.9 77.9 87.5 98.4
30 18.8 20.7 23.0 28.5 31.8 35.6 39.8 44.7 50.4 52.5 59.1 66.8 66.2 74.6 84.2 80.0 89.8 100.9
40 19.0 21.0 23.3 29.0 32.3 36.3 40.6 45.6 51.4 53.6 60.4 68.3 67.7 76.3 86.1 81.9 91.9 103.2
620
0 16.5 18.1 20.0 24.8 27.5 30.8 34.4 38.6 43.4 45.3 50.9 57.6 57.1 64.4 72.9 69.3 78.1 88.2
10 17.0 18.6 20.7 25.6 28.4 31.8 35.6 39.8 44.9 46.8 52.6 59.5 59.0 66.5 75.2 71.6 80.6 90.9
15 17.2 18.9 21.0 26.0 28.9 32.4 36.2 40.5 45.6 47.6 53.5 60.5 60.0 67.6 76.4 72.7 81.8 92.3
20 17.5 19.2 21.3 26.4 29.4 32.9 36.8 41.2 46.4 48.4 54.4 61.5 61.0 68.7 77.6 73.9 83.1 93.6
30 17.9 19.7 21.8 27.1 30.1 33.7 37.7 42.3 47.7 49.7 55.9 63.2 62.7 70.6 79.8 75.9 85.4 96.1
40 18.1 19.9 22.1 27.5 30.6 34.3 38.4 43.1 48.6 50.7 57.1 64.6 64.1 72.2 81.6 77.7 87.3 98.3
580
0 15.6 17.1 19.0 23.5 26.0 29.1 32.5 36.4 40.9 42.7 48.0 54.2 53.8 60.7 68.6 65.4 73.7 83.4
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787机组操作手册Flight Crew Operations Manual 1(76)
