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380
EPR 1.259 1.290 1.325 1.367 1.417 1.480
MACH .342 .354 .368 .382 .397 .412
KIAS 207 207 207 207 207 207
FF/ENG 17607 17627 17675 17802 18002 18353
340
EPR 1.228 1.255 1.285 1.320 1.362 1.412 1.474
MACH .330 .343 .356 .369 .383 .399 .414
KIAS 200 200 200 200 200 200 200
FF/ENG 16031 16040 16056 16096 16206 16379 16693
300
EPR 1.199 1.221 1.248 1.278 1.312 1.353 1.402
MACH .318 .330 .343 .356 .370 .384 .399
KIAS 192 192 192 192 192 192 192
FF/ENG 14508 14488 14489 14503 14533 14620 14769
787 Flight Crew Operations Manual
Performance Inflight
Gear Down, Engine INOP
FAA
Category A Brakes
Boeing Proprietary PI.17.3
GEAR DOWN
ENGINE INOP
MAX CONTINUOUS THRUST
Gear Down, Engine InoperativeLong 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
161 144 129 118 108 100 94 88 84 80 76
330 293 262 237 217 200 187 175 165 156 149
501 444 396 358 327 300 280 262 246 233 221
672 595 530 478 436 400 373 349 328 309 294
844 746 663 598 546 500 466 436 409 386 366
1016 898 798 719 655 600 559 523 490 462 438
1190 1051 933 840 765 700 652 610 572 538 510
1364 1204 1067 961 875 800 746 696 653 615 582
1539 1357 1202 1082 984 900 838 782 733 690 654
1715 1512 1338 1203 1094 1000 931 869 814 767 726
AIR
DIST
(NM)
PRESSURE ALTITUDE (1000 FT)
6 8 10 12
FUEL
(1000 LB)
TIME
(HR:MIN)
FUEL
(1000 LB)
TIME
(HR:MIN)
FUEL
(1000 LB)
TIME
(HR:MIN)
FUEL
(1000 LB)
TIME
(HR:MIN)
100 8.2 0:26 7.8 0:25 7.5 0:25 7.2 0:24
200 17.5 0:51 16.9 0:49 16.5 0:48 16.2 0:46
300 26.6 1:15 25.9 1:13 25.3 1:11 25.1 1:09
400 35.6 1:40 34.7 1:37 34.0 1:35 33.8 1:32
500 44.5 2:05 43.4 2:02 42.6 1:58 42.3 1:55
600 53.3 2:31 52.1 2:26 51.1 2:22 50.8 2:18
700 62.0 2:56 60.6 2:51 59.5 2:46 59.1 2:41
800 70.6 3:22 69.0 3:16 67.8 3:10 67.2 3:04
900 79.1 3:47 77.3 3:41 75.9 3:34 75.3 3:28
1000 87.5 4:13 85.5 4:06 84.0 3:58 83.2 3:51
REFERENCE FUEL REQUIRED
(1000 LB)
WEIGHT AT CHECK POINT (1000 LB)
300 400 500 600 700
10 -2.2 -1.1 0.0 2.0 3.6
20 -4.6 -2.4 0.0 4.4 8.1
30 -7.0 -3.6 0.0 6.7 12.5
40 -9.5 -4.8 0.0 9.0 16.9
50 -11.9 -6.0 0.0 11.1 21.2
60 -14.3 -7.3 0.0 13.2 25.5
70 -16.7 -8.5 0.0 15.2 29.7
80 -19.1 -9.7 0.0 17.1 34.0
90 -21.5 -10.9 0.0 18.9 38.1
APU fuel included.
787 Flight Crew Operations Manual
Performance Inflight
Gear Down, Engine INOP
FAA
Category A Brakes
PI.17.4 Boeing Proprietary
GEAR DOWN
ENGINE INOP
MAX CONTINUOUS THRUST
Gear Down, Engine InoperativeHolding
Flaps Up
WEIGHT
(1000 LB)
PRESSURE ALTITUDE (FT)
1500 5000 10000 15000
540
EPR 1.331 1.405
KIAS 231 231
FF/ENG 25310 25680
500
EPR 1.299 1.365
KIAS 225 225
FF/ENG 23530 23730
460
EPR 1.270 1.327 1.444
KIAS 219 219 219
FF/ENG 21810 21890 22450
420
EPR 1.241 1.292 1.392
KIAS 213 213 213
FF/ENG 20130 20160 20460
380
EPR 1.215 1.259 1.345 1.480
KIAS 207 207 207 207
FF/ENG 18490 18490 18620 19270
340
EPR 1.190 1.228 1.302 1.412
KIAS 200 200 200 200
FF/ENG 16870 16830 16870 17200
300
EPR 1.166 1.199 1.262 1.353
KIAS 192 192 192 192
FF/ENG 15280 15230 15220 15350
This table includes 5% additional fuel for holding in a racetrack pattern.
787 Flight Crew Operations Manual
Performance Inflight Chapter PI
Text Section 18
FAA
Category A Brakes
FAST-Doc PI/PD Template 9/1/99
Boeing Proprietary PI.18.1
PI.18 Performance Inflight-Text
Text
Introduction
This chapter contains information to supplement performance data from
the Flight Management Computer. In addition, sufficient inflight data is
provided to complete a flight with the FMC inoperative. In the event of
conflict between data presented in this chapter and that contained in the
Approved Flight Manual, the Flight Manual shall always take precedence.
FMC Takeoff Speeds
FMC computed takeoff speeds can be used for all performance conditions
except where adjustments must be made to V1 for clearway, stopway,
brake deactivation, improved climb, contaminated runway situations,
unbalanced for brake energy or obstacle clearance with unbalanced V1.
　
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