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1400 35.4 39.2 43.0 46.9 50.8 54.8 58.9 62.7 66.9 3:26
1500 37.9 41.9 46.0 50.2 54.4 58.7 63.0 67.1 71.6 3:41
1600 40.3 44.6 49.0 53.4 57.9 62.5 67.1 71.5 76.3 3:56
1700 42.7 47.3 51.9 56.7 61.4 66.3 71.2 75.9 80.9 4:11
1800 45.1 49.9 54.9 59.9 64.9 70.0 75.2 80.2 85.5 4:27
APU fuel included.
Driftdown at optimum driftdown speed and cruise at LRC speed.
December 15, 2006
787 Flight Crew Operations Manual
Performance Inflight A
One Engine Inoperative
777-200ER/TRENT892
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary PI.A11.7
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Altitude Capability
100 ft/min residual rate of climb
WEIGHT
(1000 LB)
PRESSURE ALTITUDE (FT)
ISA+10°C
& BELOW ISA+15°C ISA+20°C
660 15000 12700 10400
640 15600 13500 11100
620 16300 14300 11900
600 16900 15100 12700
580 17700 16100 14100
560 18700 17100 15400
540 19800 18200 16400
520 20700 19300 17500
500 21700 20300 18600
480 22700 21400 19700
460 23700 22400 20900
440 24800 23500 22100
420 25900 24700 23300
400 27100 25800 24600
380 28300 27000 25800
360 29500 28200 26900
340 30800 29500 28100
320 32400 30800 29400
300 34100 32500 30700
December 15, 2006
787 Flight Crew Operations Manual
Performance Inflight A
One Engine Inoperative
777-200ER/TRENT892
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
PI.A11.8 D615Z003 Boeing Proprietary
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Control
WEIGHT
(1000 LB)
PRESSURE ALTITUDE (1000 FT)
10 15 17 19 21 23 25 27
660
EPR 1.258 1.365
MACH .585 .641
KIAS 325 325
FF/ENG 19637 20013
620
EPR 1.237 1.335 1.385
MACH .585 .641 .665
KIAS 325 325 325
FF/ENG 18893 19190 19415
580
EPR 1.217 1.302 1.349 1.408
MACH .580 .630 .655 .684
KIAS 322 320 320 322
FF/ENG 18013 18059 18238 18696
540
EPR 1.194 1.268 1.308 1.356 1.420
MACH .563 .611 .633 .659 .689
KIAS 313 310 309 310 312
FF/ENG 16696 16656 16733 16922 17428
500
EPR 1.172 1.237 1.271 1.312 1.362 1.428
MACH .545 .592 .612 .635 .661 .692
KIAS 302 300 298 298 299 301
FF/ENG 15394 15334 15331 15411 15601 16141
460
EPR 1.151 1.209 1.238 1.272 1.314 1.365 1.433
MACH .526 .572 .592 .612 .635 .661 .693
KIAS 291 289 288 287 286 287 289
FF/ENG 14112 14046 14023 14021 14093 14273 14753
420
EPR 1.131 1.181 1.207 1.236 1.270 1.312 1.363 1.433
MACH .505 .551 .570 .590 .610 .633 .660 .692
KIAS 279 278 277 276 275 274 275 277
FF/ENG 12840 12771 12750 12729 12724 12782 12940 13370
380
EPR 1.111 1.155 1.177 1.203 1.232 1.265 1.307 1.358
MACH .482 .527 .546 .566 .586 .606 .629 .656
KIAS 267 266 265 264 263 262 261 262
FF/ENG 11570 11516 11489 11470 11450 11441 11479 11605
340
EPR 1.092 1.131 1.150 1.171 1.196 1.224 1.257 1.297
MACH .459 .502 .520 .539 .559 .579 .600 .623
KIAS 254 253 252 251 251 250 249 248
FF/ENG 10328 10268 10248 10224 10206 10188 10171 10187
300
EPR 1.075 1.106 1.123 1.142 1.162 1.185 1.213 1.244
MACH .434 .474 .492 .510 .530 .550 .570 .591
KIAS 240 238 238 238 237 236 235 234
FF/ENG 9133 9031 9011 8995 8976 8955 8938 8918
December 15, 2006
787 Flight Crew Operations Manual
Performance Inflight A
One Engine Inoperative
777-200ER/TRENT892
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary PI.A11.9
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Diversion Fuel and Time
Ground to Air Miles Conversion
Reference Fuel and Time Required at Check Point
Fuel Required Adjustment (1000 LB)
AIR DISTANCE (NM) GROUND
DISTANCE
(NM)
AIR DISTANCE (NM)
HEADWIND COMPONENT (KTS) TAILWIND COMPONENT (KTS)
100 80 60 40 20 20 40 60 80 100
282 261 242 226 213 200 191 182 174 167 160
564 522 484 452 425 400 381 364 348 334 321
846 783 727 680 638 600 572 546 522 501 481
1130 1045 970 906 850 800 763 728 696 667 641
1415 1309 1214 1133 1063 1000 953 909 870 833 801
1700 1572 1459 1361 1276 1200 1144 1091 1044 1000 961
1987 1837 1703 1589 1489 1400 1334 1273 1217 1166 1120
2275 2102 1948 1817 1703 1600 1525 1455 1391 1332 1279
2564 2368 2194 2045 1916 1800 1715 1636 1564 1498 1438
AIR
DIST
(NM)
PRESSURE ALTITUDE (1000 FT)
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