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2 Engine Reverse Thrust
Cooling Time (Minutes)
REFERENCE BRAKE ENERGY PER BRAKE (MILLIONS OF FOOT POUNDS)
EVENT 10 20 30 40 50 60 70 80 90
RTO MAX MAN 10 20 30 40 50 60 70 80 90
LANDING
MAX MAN 6.3 15.6 24.9 34.0 43.2 52.3 61.6 70.9 80.4
MAX AUTO 6.1 14.4 22.8 31.3 40.0 49.0 58.2 67.7 77.6
AUTOBRAKE 4 5.9 13.6 21.2 29.1 37.1 45.5 54.2 63.3 73.0
AUTOBRAKE 3 5.6 12.7 19.7 26.9 34.2 41.9 49.8 58.3 67.3
AUTOBRAKE 2 5.3 11.8 18.2 24.8 31.5 38.4 45.6 53.3 61.5
AUTOBRAKE 1 5.2 11.0 16.8 22.8 28.9 35.2 41.9 48.9 56.4
REFERENCE BRAKE ENERGY PER BRAKE (MILLIONS OF FOOT POUNDS)
EVENT 10 20 30 40 50 60 70 80 90
RTO MAX MAN 10 20 30 40 50 60 70 80 90
LANDING
MAX MAN 5.8 14.7 23.4 32.0 40.4 48.8 57.2 65.6 74.2
MAX AUTO 4.3 11.6 18.9 26.4 34.1 42.0 50.2 58.9 68.0
AUTOBRAKE 4 3.6 9.2 15.0 21.1 27.5 34.4 41.7 49.6 58.2
AUTOBRAKE 3 2.5 6.6 11.1 15.9 21.0 26.7 32.8 39.5 46.8
AUTOBRAKE 2 1.4 4.4 7.6 11.3 15.3 19.7 24.5 29.8 35.6
AUTOBRAKE 1 1.0 3.0 5.3 7.8 10.6 13.9 17.5 21.7 26.4
EVENT ADJUSTED BRAKE ENERGY (MILLIONS OF FOOT POUNDS)
16 & BELOW 17 18 20 24 28 32 35 36 TO 44 45 & ABOVE
GEAR DOWN
INFLIGHT
NO SPECIAL
PROCEDURE
REQUIRED
1 2 3 4 6 7 7 CAUTION FUSE PLUG
GROUND 11 18 26 42 55 66 73 MELT ZONE
BTMS UP TO 2.4 2.4 2.6 2.9 3.4 4.0 4.5 4.9 5.0 TO 6.3 6.3 & ABOVE
Observe maximum quick turnaround limit.
Table shows energy per brake added by a single stop with all brakes operating. Energy is assumed to be
equally distributed among the operating brakes. Total energy is the sum of residual energy plus energy
added.
Add 1.0 million foot pounds for each taxi mile.
For one brake deactivated, increase brake energy by 10 percent.
For two brakes deactivated, increase brake energy by 20 percent.
When in caution zone, wheel fuse plugs may melt. Delay takeoff and inspect after one hour. If overheat occurs
after takeoff, extend gear soon for at least 8 minutes.
When in fuse plug melt zone, clear runway immediately. Unless required, do not set parking brake. Do not
attempt to taxi for one hour. Tire, wheel and brake replacement may be required. If overheat occurs after
takeoff, extend gear soon for at least 12 minutes.
Brake temperature monitor system (BTMS) indication on EICAS may be used 10 to 15 minutes after airplane
has come to a complete stop, or inflight with gear retracted, to determine recommended cooling schedule.
(When inflight with gear extended, the BTMS indications may vary between individual brakes, due to airstream
effects.)
December 15, 2006
787 Flight Crew Operations Manual
Performance Inflight A
Advisory Information
777-200ER/TRENT892
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary PI.A10.13
ADVISORY INFORMATION
Advisory Information Landing 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.
December 15, 2006
787 Flight Crew Operations Manual
Performance Inflight A
Advisory Information
777-200ER/TRENT892
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
PI.A10.14 D615Z003 Boeing Proprietary
　
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