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360 0.59 90.2 91.0 91.9 92.7 93.5 94.4 95.2 96.0 96.8 97.6 96.9 96.1
BLEED CONFIGURATION PRESS ALT (1000 FT)
16 14 12 10 5
ENGINE ANTI-ICE ON -0.4 -0.4 -0.4 -0.4 -0.3
ENGINE & WING ANTI-ICE ON (packs on) -0.5 -0.5 -0.5 -0.5 -0.5
ENGINE & WING ANTI-ICE ON (packs off) -0.7 -0.7 -0.7 -0.7 -0.7
December 10, 2007
777 Flight Crew Operations Manual
Performance Inflight
Engine Inoperative
777-200/GE90-76B
JAA/JAROPS
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D632W001-TBC PI.12.5
ENGINE INOP
MAX CONTINUOUS THRUST
Driftdown Speed/Level Off Altitude
100 ft/min residual rate of climb
Includes APU fuel burn
WEIGHT (1000 KG) OPTIMUM
DRIFTDOWN
SPEED
(KIAS)
LEVEL OFF PRESSURE ALTITUDE (FT)
START
DRIFT
DOWN
LEVEL
OFF
ISA + 10°C
& BELOW ISA + 15°C ISA + 20°C
260 252 263 19700 18400 16600
240 232 253 22000 21000 19700
220 213 243 24200 23500 22300
200 194 232 26600 26000 25000
180 174 220 29000 28700 27900
160 155 208 31600 31500 31000
December 10, 2007
777 Flight Crew Operations Manual
Performance Inflight
Engine Inoperative
777-200/GE90-76B
JAA/JAROPS
Category A Brakes
Copyright © The Boeing Company. See title page for details.
PI.12.6 D632W001-TBC
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
273 255 238 224 211 200 190 181 172 165 158
412 383 358 337 317 300 285 271 258 246 236
550 511 478 449 423 400 379 361 344 329 314
686 639 597 561 529 500 474 451 430 411 393
822 765 716 673 634 600 569 541 516 493 472
958 892 835 784 740 700 664 632 603 576 552
1093 1018 953 896 845 800 759 723 689 659 631
1227 1144 1071 1007 951 900 854 813 776 742 711
1362 1270 1190 1119 1056 1000 950 904 863 825 790
1496 1395 1308 1230 1161 1100 1045 995 949 908 870
1630 1521 1426 1342 1267 1200 1140 1085 1036 991 949
1765 1647 1544 1453 1372 1300 1235 1176 1123 1074 1029
1900 1773 1662 1565 1478 1400 1330 1267 1209 1157 1108
2035 1900 1781 1676 1583 1500 1425 1357 1296 1239 1188
2171 2027 1900 1788 1689 1600 1520 1448 1382 1322 1267
2308 2154 2019 1900 1795 1700 1615 1538 1468 1404 1346
2445 2282 2139 2012 1900 1800 1710 1628 1554 1486 1424
AIR
DIST
(NM)
FUEL REQUIRED (1000 KG)
TIME
WEIGHT AT START OF DRIFTDOWN (1000 KG) (HR:MIN)
160 180 200 220 240 260
100 0.9 1.0 1.0 1.1 1.2 1.3 0:15
200 2.1 2.3 2.5 2.7 2.9 3.1 0:32
300 3.4 3.7 4.1 4.4 4.8 5.2 0:49
400 4.7 5.2 5.7 6.2 6.7 7.2 1:05
500 6.0 6.6 7.3 8.0 8.6 9.3 1:21
600 7.2 8.0 8.8 9.6 10.4 11.2 1:37
700 8.4 9.3 10.3 11.3 12.2 13.1 1:53
800 9.6 10.7 11.8 12.9 13.9 15.0 2:09
900 10.8 12.0 13.3 14.5 15.7 16.9 2:24
1000 12.0 13.3 14.7 16.1 17.5 18.8 2:39
1100 13.2 14.7 16.2 17.7 19.2 20.7 2:55
1200 14.4 16.0 17.6 19.3 20.9 22.5 3:10
1300 15.5 17.3 19.1 20.9 22.6 24.4 3:25
1400 16.7 18.6 20.5 22.4 24.3 26.2 3:41
1500 17.8 19.8 21.9 24.0 26.0 28.0 3:57
1600 18.9 21.1 23.3 25.5 27.6 29.8 4:13
1700 20.0 22.3 24.7 27.0 29.3 31.6 4:29
1800 21.1 23.6 26.1 28.5 30.9 33.4 4:45
APU fuel included.
Driftdown at optimum speed and cruise at LRC speed.
December 10, 2007
777 Flight Crew Operations Manual
Performance Inflight
Engine Inoperative
777-200/GE90-76B
JAA/JAROPS
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D632W001-TBC PI.12.7
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Altitude Capability
100 ft/min residual rate of climb
Long Range Cruise Control
WEIGHT
(1000 KG)
PRESSURE ALTITUDE (FT)
ISA + 10°C
& BELOW ISA + 15°C ISA + 20°C
260 15400 13400 10700
240 18500 16300 14400
220 21300 20100 18000
200 23900 22900 21500
180 26600 25800 24600
160 29500 28900 27900
140 32400 32200 31400
With engine anti-ice on, decrease altitude capability by 700 ft.
With engine and wing anti-ice on, decrease altitude capability by 1100 ft.
WEIGHT
(1000 KG)
PRESSURE ALTITUDE (1000 FT)
10 15 17 19 21 23 25 27
260
%N1 91.5 95.9 97.6
MACH .557 .602 .624
KIAS 309 305 304
FF/ENG 7544 7611 7718
240
　
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