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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.)
787 Flight Crew Operations Manual
Performance Inflight Chapter PI
Engine Inoperative Section 13
FAA
Category A Brakes
FAST-Doc PI/PD Template 9/1/99
Boeing Proprietary PI.13.1
PI.13 Performance Inflight-Engine InoperativeENGINE INOP
Engine InoperativeInitial Max Continuous EPR
Based on .84M, engine bleed for packs on and anti-ice off
TAT
(°C)
PRESSURE ALTITUDE (1000 FT)
27 29 31 33 35 37 39 41 43
20 &
ABOVE 1.243 1.234 1.226 1.211 1.192 1.183 1.181 1.175 1.170
15 1.284 1.275 1.263 1.250 1.232 1.222 1.220 1.216 1.212
10 1.327 1.319 1.307 1.288 1.273 1.264 1.262 1.259 1.257
5 1.364 1.366 1.354 1.337 1.314 1.306 1.304 1.302 1.300
0 1.364 1.402 1.406 1.388 1.368 1.355 1.354 1.351 1.349
-5 1.364 1.402 1.439 1.444 1.424 1.412 1.411 1.408 1.406
-10 1.364 1.402 1.439 1.473 1.482 1.471 1.469 1.467 1.465
-15 1.364 1.402 1.439 1.473 1.506 1.523 1.523 1.521 1.518
-20 &
BELOW 1.364 1.402 1.439 1.473 1.506 1.523 1.523 1.521 1.518
787 Flight Crew Operations Manual
Performance Inflight
Engine Inoperative
FAA
Category A Brakes
PI.13.2 Boeing Proprietary
ENGINE INOP
Engine InoperativeMax Continuous EPR
Based on engine bleed for packs on or off and anti-ice off
37000 FT to 29000 FT Pressure Altitudes
EPR Adjustments for Engine Bleed
37000 FT PRESS ALT TAT (°C)
KIAS M -50 -45 -40 -35 -30 -25 -20 -15 -10 -5 0 5
200 0.63 1.531 1.531 1.531 1.531 1.531 1.489 1.436 1.385 1.341 1.302 1.263 1.233
240 0.74 1.534 1.534 1.534 1.534 1.534 1.534 1.517 1.455 1.402 1.349 1.308 1.268
280 0.86 1.506 1.506 1.506 1.506 1.506 1.506 1.506 1.506 1.469 1.413 1.356 1.304
35000 FT PRESS ALT TAT (°C)
KIAS M -50 -45 -40 -35 -30 -25 -20 -15 -10 -5 0 5
200 0.60 1.517 1.517 1.517 1.517 1.517 1.486 1.433 1.385 1.341 1.304 1.267 1.234
240 0.71 1.514 1.514 1.514 1.514 1.514 1.514 1.502 1.444 1.394 1.344 1.305 1.266
280 0.82 1.519 1.519 1.519 1.519 1.519 1.519 1.519 1.519 1.476 1.417 1.362 1.311
33000 FT PRESS ALT TAT (°C)
KIAS M -50 -45 -40 -35 -30 -25 -20 -15 -10 -5 0 5
200 0.58 1.499 1.499 1.499 1.499 1.499 1.499 1.447 1.401 1.358 1.323 1.290 1.257
240 0.68 1.491 1.491 1.491 1.491 1.491 1.491 1.491 1.452 1.402 1.355 1.314 1.278
280 0.79 1.489 1.489 1.489 1.489 1.489 1.489 1.489 1.489 1.472 1.414 1.363 1.314
320 0.89 1.427 1.427 1.427 1.427 1.427 1.427 1.427 1.427 1.427 1.427 1.389 1.338
31000 FT PRESS ALT TAT (°C)
KIAS M -45 -40 -35 -30 -25 -20 -15 -10 -5 0 5 10
200 0.55 1.480 1.480 1.480 1.480 1.480 1.461 1.414 1.372 1.332 1.303 1.274 1.245
240 0.66 1.471 1.471 1.471 1.471 1.471 1.471 1.461 1.410 1.365 1.322 1.291 1.260
280 0.76 1.459 1.459 1.459 1.459 1.459 1.459 1.459 1.459 1.415 1.366 1.321 1.281
320 0.85 1.426 1.426 1.426 1.426 1.426 1.426 1.426 1.426 1.426 1.406 1.353 1.306
29000 FT PRESS ALT TAT (°C)
KIAS M -40 -35 -30 -25 -20 -15 -10 -5 0 5 10 15
200 0.53 1.493 1.493 1.493 1.493 1.493 1.454 1.411 1.369 1.334 1.302 1.270 1.252
240 0.63 1.475 1.475 1.475 1.475 1.475 1.475 1.441 1.395 1.352 1.315 1.286 1.255
280 0.73 1.446 1.446 1.446 1.446 1.446 1.446 1.446 1.426 1.378 1.334 1.293 1.259
320 0.82 1.413 1.413 1.413 1.413 1.413 1.413 1.413 1.413 1.413 1.362 1.317 1.273
360 0.91 1.351 1.351 1.351 1.351 1.351 1.351 1.351 1.351 1.351 1.351 1.330 1.284
ANTI-ICE CONFIGURATION PRESSURE ALTITUDE (1000 FT)
37 35 33 31 29
ENGINE ONLY -0.004 -0.003 -0.003 -0.003 -0.003
ENGINE & WING* -0.015 -0.014 -0.013 -0.012 -0.012
ENGINE & WING** -0.026 -0.024 -0.022 -0.021 -0.020
* Wing anti-ice on, packs on.
**Wing anti-ice on, packs off.
787 Flight Crew Operations Manual
　
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