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TIME
(HR:MIN)
FUEL
(1000 LB)
TIME
(HR:MIN)
FUEL
(1000 LB)
TIME
(HR:MIN)
FUEL
(1000 LB)
TIME
(HR:MIN)
200 7.9 0:38 6.8 0:37 6.1 0:36 5.4 0:35
400 16.8 1:13 15.3 1:10 14.1 1:07 13.1 1:04
600 25.7 1:48 23.6 1:44 22.0 1:39 20.7 1:34
800 34.4 2:24 31.9 2:17 29.8 2:11 28.2 2:04
1000 43.0 2:59 40.1 2:51 37.6 2:43 35.6 2:34
1200 51.6 3:35 48.1 3:25 45.3 3:15 42.9 3:04
1400 60.0 4:12 56.1 3:59 52.9 3:47 50.2 3:35
1600 68.4 4:48 64.1 4:34 60.4 4:20 57.4 4:05
1800 76.6 5:25 71.9 5:08 67.8 4:53 64.5 4:36
REFERENCE FUEL REQUIRED
(1000 LB)
WEIGHT AT CHECK POINT (1000 LB)
300 400 500 600 700
5 -0.7 -0.4 0.0 0.6 1.5
10 -2.1 -1.1 0.0 1.7 3.5
15 -3.4 -1.7 0.0 2.7 5.5
20 -4.6 -2.3 0.0 3.7 7.4
25 -5.8 -2.9 0.0 4.6 9.4
30 -7.1 -3.5 0.0 5.6 11.3
35 -8.3 -4.1 0.0 6.5 13.2
40 -9.5 -4.7 0.0 7.4 15.1
45 -10.8 -5.3 0.0 8.3 16.9
50 -12.0 -5.9 0.0 9.2 18.7
55 -13.2 -6.5 0.0 10.1 20.5
60 -14.5 -7.1 0.0 10.9 22.3
65 -15.7 -7.7 0.0 11.7 24.0
70 -16.9 -8.3 0.0 12.5 25.8
75 -18.1 -9.0 0.0 13.3 27.5
80 -19.4 -9.6 0.0 14.1 29.1
APU fuel included.
787 Flight Crew Operations Manual
Performance Inflight
Engine Inoperative
FAA
Category A Brakes
PI.13.10 Boeing Proprietary
ENGINE INOP
MAX CONTINUOUS THRUST
Holding
Flaps up
WEIGHT
(1000 LB)
PRESSURE ALTITUDE (FT)
1500 5000 10000 15000 20000 25000
660
EPR 1.162 1.199 1.270 1.362
KIAS 259 260 261 277
FF/ENG 17770 17790 17960 18700
620
EPR 1.148 1.180 1.244 1.329
KIAS 251 252 253 262
FF/ENG 16570 16570 16680 17150
580
EPR 1.134 1.162 1.219 1.299 1.409
KIAS 243 244 245 248 269
FF/ENG 15390 15400 15440 15690 16690
540
EPR 1.120 1.145 1.195 1.268 1.364
KIAS 234 235 236 237 252
FF/ENG 14230 14230 14240 14380 15010
500
EPR 1.107 1.130 1.173 1.237 1.324 1.464
KIAS 226 226 227 228 235 259
FF/ENG 13100 13080 13080 13150 13510 14800
460
EPR 1.093 1.113 1.151 1.207 1.287 1.397
KIAS 219 219 219 219 220 238
FF/ENG 12030 11980 11970 11980 12120 12860
420
EPR 1.081 1.097 1.130 1.177 1.246 1.344
KIAS 213 213 213 213 213 220
FF/ENG 11010 10930 10890 10890 10950 11290
380
EPR 1.069 1.083 1.110 1.150 1.208 1.294
KIAS 207 207 207 207 207 207
FF/ENG 10270 9920 9850 9840 9850 9970
340
EPR 1.058 1.070 1.092 1.125 1.173 1.245
KIAS 200 200 200 200 200 200
FF/ENG 9270 9170 8840 8820 8810 8850
300
EPR 1.047 1.057 1.076 1.102 1.141 1.201
KIAS 192 192 192 192 192 192
FF/ENG 8290 8200 8010 7920 7900 7810
This table includes 5% additional fuel for holding in a racetrack pattern.
787 Flight Crew Operations Manual
Performance Inflight
Engine Inoperative
FAA
Category A Brakes
Boeing Proprietary PI.13.11
ENGINE INOP
ADVISORY INFORMATION
Gear Down Landing Rate of Climb Available
Flaps 20
Flaps 30
TAT (°C)
RATE OF CLIMB (FT/MIN)
PRESSURE ALTITUDE (FT)
-2000 0 2000 4000 6000 8000
52 650 550
50 700 600 460
48 750 650 510
46 810 700 560 410
44 850 750 610 450
42 890 810 660 480 350
40 930 860 700 520 380
38 970 900 740 550 410 260
36 1000 940 780 590 440 290
34 1040 980 820 630 470 320
32 1050 1020 850 660 500 350
30 1050 1050 880 690 540 380
20 1070 1070 960 820 660 500
10 1090 1100 980 830 690 550
0 1110 1120 1000 850 700 570
-20 1160 1170 1040 890 730 590
-40 1210 1220 1090 930 770 620
Rate of climb capability shown is valid for 400000 lb, gear down at VREF20 + 5.
Decrease rate of climb 40 ft/min per 10000 lb greater than 400000 lb.
Increase rate of climb 60 ft/min per 10000 lb less than 400000 lb.
TAT (°C)
RATE OF CLIMB (FT/MIN)
PRESSURE ALTITUDE (FT)
-2000 0 2000 4000 6000 8000
52 170 70
50 220 110 -30
48 260 160 20
46 310 200 60 -90
44 350 250 110 -60
42 390 300 150 -20 -160
40 420 350 190 10 -130
38 450 380 220 40 -110 -250
36 490 410 260 70 -80 -220
34 520 450 290 100 -50 -200
32 520 480 320 130 -20 -170
30 520 520 350 160 10 -150
20 530 530 410 270 110 -50
10 540 540 420 270 130 -10
0 560 550 430 280 130 0
-20 580 580 450 290 140 0
-40 610 610 470 310 150 0
Rate of climb capability shown is valid for 400000 lb, gear down at VREF30 + 5.
Decrease rate of climb 40 ft/min per 10000 lb greater than 400000 lb.
Increase rate of climb 60 ft/min per 10000 lb less than 400000 lb.
　
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