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MACH .516 .562 .581 .601 .623 .648 .677
KIAS 286 284 283 282 281 281 282
FF/ENG 6126 6094 6085 6077 6089 6140 6273
180
EPR 1.119 1.166 1.189 1.217 1.247 1.284 1.330 1.386
MACH .492 .537 .556 .576 .596 .617 .642 .671
KIAS 272 271 270 269 268 267 267 268
FF/ENG 5490 5462 5451 5443 5434 5438 5475 5573
160
EPR 1.098 1.139 1.158 1.181 1.207 1.237 1.272 1.316
MACH .466 .510 .529 .548 .568 .588 .609 .633
KIAS 258 257 256 256 255 254 253 252
FF/ENG 4862 4838 4827 4817 4809 4800 4796 4817
December 10, 2007
777 Flight Crew Operations Manual
Performance Inflight
Engine Inoperative
777-200ER/TRENT892
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D632W001-TBC PI.22.9
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 KG)
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
287 264 244 227 213 200 191 182 174 167 160
576 530 489 455 426 400 381 364 348 334 321
865 796 735 684 640 600 572 546 522 501 482
1156 1064 982 913 853 800 763 729 698 669 643
1448 1332 1229 1142 1067 1000 953 910 871 835 803
1742 1602 1477 1372 1281 1200 1144 1092 1045 1002 963
2036 1871 1725 1602 1495 1400 1335 1274 1219 1168 1122
2332 2141 1973 1831 1709 1600 1525 1456 1392 1334 1282
2629 2414 2223 2062 1924 1800 1715 1637 1565 1500 1441
AIR
DIST
(NM)
PRESSURE ALTITUDE (1000 FT)
10 14 18 22 26
FUEL
(1000 KG)
TIME
(HR:MIN)
FUEL
(1000 KG)
TIME
(HR:MIN)
FUEL
(1000 KG)
TIME
(HR:MIN)
FUEL
(1000 KG)
TIME
(HR:MIN)
FUEL
(1000 KG)
TIME
(HR:MIN)
200 3.4 0:40 3.0 0:38 2.6 0:37 2.4 0:36 2.1 0:34
400 7.1 1:17 6.5 1:13 6.0 1:10 5.5 1:07 5.2 1:03
600 10.9 1:54 10.0 1:48 9.3 1:43 8.7 1:38 8.2 1:33
800 14.5 2:31 13.5 2:24 12.6 2:17 11.8 2:10 11.2 2:02
1000 18.2 3:09 16.9 2:59 15.8 2:51 14.9 2:42 14.2 2:32
1200 21.8 3:47 20.3 3:35 19.1 3:25 17.9 3:14 17.1 3:02
1400 25.3 4:26 23.7 4:12 22.2 3:59 20.9 3:47 20.0 3:33
1600 28.8 5:05 27.0 4:48 25.4 4:33 23.9 4:19 22.9 4:03
1800 32.3 5:44 30.3 5:25 28.5 5:08 26.9 4:52 25.7 4:34
REFERENCE FUEL REQUIRED
(1000 KG)
WEIGHT AT CHECK POINT (1000 KG)
160 180 200 220 240 260 280 300
2 -0.1 -0.1 0.0 0.1 0.3 0.4 0.6 0.7
4 -0.4 -0.2 0.0 0.4 0.7 1.1 1.5 1.9
6 -0.6 -0.3 0.0 0.6 1.2 1.8 2.4 3.1
8 -0.9 -0.4 0.0 0.8 1.6 2.5 3.4 4.3
10 -1.1 -0.5 0.0 1.0 2.1 3.2 4.3 5.4
12 -1.3 -0.7 0.0 1.2 2.5 3.8 5.2 6.6
14 -1.6 -0.8 0.0 1.4 2.9 4.5 6.1 7.7
16 -1.8 -0.9 0.0 1.6 3.3 5.1 6.9 8.8
18 -2.0 -1.0 0.0 1.8 3.7 5.7 7.8 10.0
20 -2.3 -1.1 0.0 2.0 4.1 6.3 8.6 11.1
22 -2.5 -1.2 0.0 2.2 4.5 6.9 9.5 12.1
24 -2.8 -1.4 0.0 2.4 4.9 7.5 10.3 13.2
26 -3.0 -1.5 0.0 2.5 5.2 8.1 11.1 14.3
28 -3.2 -1.6 0.0 2.7 5.6 8.7 11.9 15.4
30 -3.5 -1.7 0.0 2.9 5.9 9.2 12.7 16.4
32 -3.7 -1.8 0.0 3.0 6.2 9.7 13.5 17.4
34 -3.9 -2.0 0.0 3.1 6.6 10.3 14.2 18.5
December 10, 2007
777 Flight Crew Operations Manual
Performance Inflight
Engine Inoperative
777-200ER/TRENT892
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
PI.22.10 D632W001-TBC
ENGINE INOP
MAX CONTINUOUS THRUST
Holding
Flaps up
WEIGHT
(1000 KG)
PRESSURE ALTITUDE (FT)
1500 5000 10000 15000 20000 25000
300
EPR 1.163 1.2 1.271 1.363
KIAS 260 260 262 277
FF/ENG 8080 8090 8160 8510
280
EPR 1.147 1.179 1.242 1.327 1.46
KIAS 251 251 253 261 286
FF/ENG 7480 7480 7530 7730 8420
260
EPR 1.131 1.159 1.215 1.294 1.401
KIAS 242 242 243 246 266
FF/ENG 6890 6900 6910 7010 7430
240
EPR 1.116 1.141 1.189 1.259 1.352
KIAS 232 233 234 235 247
FF/ENG 6310 6310 6320 6370 6620
220
EPR 1.101 1.124 1.165 1.225 1.31 1.437
KIAS 223 223 224 224 230 251
FF/ENG 5760 5740 5740 5760 5880 6350
200
EPR 1.087 1.105 1.141 1.192 1.268 1.37
KIAS 216 216 216 216 216 229
FF/ENG 5240 5200 5190 5190 5240 5480
180
EPR 1.074 1.089 1.119 1.161 1.224 1.316
KIAS 209 209 209 209 209 209
FF/ENG 4850 4690 4660 4660 4680 4750
160
EPR 1.062 1.075 1.097 1.133 1.184 1.26
KIAS 202 202 202 202 202 202
FF/ENG 4350 4300 4150 4150 4140 4170
140
EPR 1.049 1.06 1.079 1.107 1.148 1.21
　
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