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330 0.59 1.383 1.383 1.383 1.383 1.383 1.383 1.383 1.383 1.382 1.327 1.285 1.246
5000 FT PRESS ALT TAT (°C)
KIAS M -10 -5 0 5 10 15 20 25 30 35 40 45
150 0.25 1.385 1.385 1.385 1.385 1.385 1.385 1.377 1.348 1.323 1.302 1.281 1.260
200 0.33 1.367 1.367 1.367 1.367 1.367 1.367 1.367 1.353 1.336 1.316 1.291 1.265
250 0.41 1.341 1.341 1.341 1.341 1.341 1.341 1.341 1.341 1.326 1.311 1.287 1.253
300 0.49 1.333 1.333 1.333 1.333 1.333 1.333 1.333 1.333 1.327 1.289 1.254 1.221
330 0.54 1.311 1.311 1.311 1.311 1.311 1.311 1.311 1.311 1.311 1.289 1.252 1.218
ANTI-ICE CONFIGURATION PRESSURE ALTITUDE (1000 FT)
5 10 12 14
ENGINE ONLY -0.015 -0.015 -0.013 -0.010
ENGINE & WING* -0.023 -0.025 -0.023 -0.020
ENGINE & WING** -0.031 -0.035 -0.033 -0.030
*Wing anti-ice on, packs on.
**Wing anti-ice on, packs off.
December 10, 2007
777 Flight Crew Operations Manual
Performance Inflight
Engine Inoperative
777-300/PW4090
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
PI.32.6 D632W001-TBC
ENGINE INOP
MAX CONTINUOUS THRUST
Driftdown Speed/Level Off Altitude
100 ft/min residual rate of climb
Includes APU fuel burn
WEIGHT (1000 LB) OPTIMUM
DRIFTDOWN
SPEED
(KIAS)
LEVEL OFF PRESSURE ALTITUDE (FT)
START
DRIFT
DOWN
LEVEL
OFF
ISA + 10°C
& BELOW ISA + 15°C ISA + 20°C
660 638 281 16200 14700 13100
620 600 273 17700 16300 14700
580 562 264 19000 18000 16400
540 522 255 20400 19600 18300
500 483 246 22300 21700 20500
460 444 236 24300 24100 22900
420 406 226 26400 26200 25300
380 367 215 28700 28300 27500
340 329 204 31200 30600 29900
December 10, 2007
777 Flight Crew Operations Manual
Performance Inflight
Engine Inoperative
777-300/PW4090
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D632W001-TBC PI.32.7
ENGINE INOP
MAX CONTINUOUS THRUST
Driftdown/LRC Cruise Range Capability
Ground to Air Miles Conversion
Driftdown/Cruise Fuel and Time
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
134 125 118 111 105 100 95 91 87 83 80
274 255 239 224 211 200 190 181 172 165 158
413 384 359 337 317 300 284 270 258 246 236
551 512 479 449 423 400 379 360 343 328 314
688 640 598 561 529 500 474 451 429 410 393
825 768 717 674 635 600 569 541 516 492 471
961 895 836 785 740 700 664 631 602 575 550
1097 1021 955 897 846 800 759 722 688 658 629
1233 1148 1074 1009 951 900 854 812 775 740 709
1368 1274 1192 1121 1057 1000 949 903 861 823 788
1503 1401 1311 1232 1162 1100 1044 993 947 906 867
1639 1527 1430 1344 1268 1200 1139 1084 1034 988 947
1774 1654 1548 1456 1373 1300 1234 1174 1120 1071 1026
1910 1781 1667 1567 1479 1400 1329 1265 1207 1153 1105
2047 1908 1786 1679 1585 1500 1424 1355 1293 1236 1184
2184 2035 1906 1792 1690 1600 1519 1445 1379 1318 1263
2321 2163 2025 1904 1796 1700 1614 1536 1465 1400 1341
2460 2292 2145 2016 1902 1800 1708 1626 1550 1482 1419
AIR DIST
(NM)
FUEL REQUIRED (1000 LB)
TIME
WEIGHT AT START OF DRIFTDOWN (1000 LB) (HR:MIN)
340 380 420 460 500 540 580 620 660
100 2.1 2.3 2.5 2.8 3.0 3.2 3.2 3.4 3.6 0:15
200 4.9 5.4 5.8 6.3 6.8 7.2 7.5 8.0 8.6 0:32
300 8.0 8.8 9.5 10.3 11.1 11.9 12.5 13.4 14.2 0:49
400 11.2 12.3 13.4 14.5 15.6 16.7 17.7 18.9 20.1 1:06
500 14.2 15.7 17.1 18.5 20.0 21.4 22.6 24.2 25.8 1:22
600 17.2 19.0 20.7 22.4 24.1 25.9 27.4 29.3 31.2 1:38
700 20.2 22.2 24.2 26.2 28.3 30.4 32.2 34.4 36.5 1:54
800 23.1 25.4 27.7 30.0 32.4 34.8 36.9 39.4 41.8 2:10
900 26.0 28.6 31.2 33.8 36.4 39.1 41.6 44.4 47.1 2:26
1000 28.8 31.7 34.6 37.5 40.5 43.4 46.2 49.4 52.3 2:41
1100 31.6 34.8 38.0 41.2 44.4 47.7 50.8 54.2 57.5 2:57
1200 34.4 37.9 41.4 44.8 48.4 51.9 55.3 59.1 62.6 3:13
1300 37.1 40.9 44.7 48.4 52.2 56.1 59.8 63.8 67.7 3:29
1400 39.8 43.9 47.9 52.0 56.1 60.2 64.2 68.6 72.7 3:44
1500 42.5 46.9 51.2 55.5 59.9 64.3 68.6 73.3 77.6 4:00
1600 45.1 49.8 54.4 59.0 63.7 68.4 73.0 77.9 82.5 4:17
1700 47.8 52.7 57.6 62.5 67.4 72.4 77.3 82.5 87.4 4:33
1800 50.3 55.5 60.7 65.9 71.1 76.4 81.5 87.0 92.2 4:50
Includes APU fuel burn.
Driftdown at optimum driftdown speed and cruise at LRC speed.
December 10, 2007
777 Flight Crew Operations Manual
Performance Inflight
Engine Inoperative
777-300/PW4090
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
　
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