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KIAS 207 207 207 207 207 207 221 233 237 232
FF/ENG 6000 5880 5590 5470 5400 5220 5360 5560 5780 6010
340
EPR .996 .998 1.002 1.008 1.019 1.035 1.059 1.079 1.137 1.187
KIAS 200 200 200 200 200 200 200 219 223 225
FF/ENG 5500 5370 5090 4960 4880 4820 4680 4910 5160 5370
300
EPR .994 .995 .997 1.001 1.009 1.023 1.040 1.068 1.109 1.146
KIAS 192 192 192 192 192 192 192 196 208 210
FF/ENG 5030 4890 4730 4480 4390 4310 4270 4190 4480 4630
This table includes 5% additional fuel for holding in a racetrack pattern.
787 Flight Crew Operations Manual
Performance Inflight
All Engine
FAA
Category A Brakes
PI.11.8 Boeing Proprietary
All EngineHolding
Flaps 1
WEIGHT
(1000 LB)
PRESSURE ALTITUDE (FT)
1500 5000 10000 15000 20000
660
EPR 1.057 1.069 1.096 1.134 1.191
KIAS 228 228 228 228 228
FF/ENG 10290 9970 9940 9980 10040
620
EPR 1.050 1.062 1.084 1.119 1.169
KIAS 222 222 222 222 222
FF/ENG 9640 9560 9270 9300 9340
580
EPR 1.044 1.054 1.073 1.104 1.148
KIAS 217 217 217 217 217
FF/ENG 9000 8900 8610 8610 8650
540
EPR 1.038 1.047 1.063 1.089 1.128
KIAS 211 211 211 211 211
FF/ENG 8370 8270 7970 8090 8110
500
EPR 1.031 1.040 1.054 1.076 1.110
KIAS 205 205 205 205 205
FF/ENG 7910 7810 7690 7440 7450
460
EPR 1.026 1.033 1.046 1.063 1.092
KIAS 199 199 199 199 199
FF/ENG 7290 7200 7070 6820 6800
420
EPR 1.020 1.026 1.037 1.052 1.075
KIAS 193 193 193 193 193
FF/ENG 6700 6610 6480 6380 6180
380
EPR 1.015 1.020 1.029 1.042 1.060
KIAS 187 187 187 187 187
FF/ENG 6270 6010 5900 5790 5720
340
EPR 1.011 1.015 1.022 1.032 1.046
KIAS 180 180 180 180 180
FF/ENG 5710 5590 5330 5220 5130
300
EPR 1.007 1.010 1.015 1.024 1.035
KIAS 172 172 172 172 172
FF/ENG 5170 5030 4890 4670 4560
This table includes 5% additional fuel for holding in a racetrack pattern.
787 Flight Crew Operations Manual
Performance Inflight Chapter PI
Advisory Information Section 12
FAA
Category A Brakes
FAST-Doc PI/PD Template 9/1/99
Boeing Proprietary PI.12.1
PI.12 Performance Inflight-AdAviDsoVry IISnfOorRmaYti oInNFORMATION
Advisory InformationNormal Configuration Landing Distance
Flaps 30
Dry Runway
Good Reported Braking Action
Medium Reported Braking Action
Poor Reported Braking Action
LANDING DISTANCE AND ADJUSTMENTS (FT)
REF
DIST*
WT
ADJ
ALT
ADJ
WIND ADJ
PER 10 KTS
SLOPE ADJ
PER 1%
TEMP ADJ
PER 10°C
VREF
ADJ
REVERSE
THRUST
ADJ
BRAKING
CONFIGURATION
400000 LB
LANDING
WT
PER
10000 LB
ABOVE
BELOW
40000 LB
PER
1000 FT
ABOVE
S.L.
HEAD
WIND
TAIL
WIND
DN
HILL
UP
HILL
ABV
ISA
BLW
ISA
PER
10 KTS
ABOVE
VREF30
ONE
REV
NO
REV
MAX MANUAL 2740 +70/-40 50 -110 420 30 -30 50 -50 220 30 80
MAX AUTO 3620 +60/-40 80 -160 580 0 0 80 -80 380 0 0
AUTOBRAKE 4 4440 +80/-60 110 -220 800 0 -20 110 -110 480 0 0
AUTOBRAKE 3 5340 +100/-80 140 -270 1000 40 -40 140 -140 580 10 20
AUTOBRAKE 2 5970 +120/-100 170 -320 1160 50 -110 160 -160 530 50 50
AUTOBRAKE 1 6380 +140/-120 190 -350 1300 130 -170 170 -170 510 350 360
MAX MANUAL 3730 +70/-60 90 -190 720 90 -80 80 -90 310 160 380
MAX AUTO 4090 +70/-70 100 -190 740 70 -60 90 -90 360 180 410
AUTOBRAKE 4 4460 +80/-80 110 -220 830 20 -30 110 -110 480 20 80
AUTOBRAKE 3 5340 +100/-100 140 -270 1000 40 -40 140 -140 580 10 20
MAX MANUAL 4970 +100/-100 140 -290 1190 230 -170 120 -120 390 480 1220
MAX AUTO 5250 +100/-100 140 -290 1170 220 -140 120 -120 450 460 1210
AUTOBRAKE 4 5250 +110/-100 140 -290 1190 220 -140 130 -130 440 510 1300
AUTOBRAKE 3 5600 +110/-110 150 -320 1260 160 -100 150 -150 580 240 890
MAX MANUAL 6320 +150/-130 200 -430 1880 570 -330 160 -160 450 1060 2970
MAX AUTO 6700 +150/-130 200 -430 1860 570 -340 160 -160 440 1070 3000
AUTOBRAKE 4 6700 +150/-140 200 -430 1870 550 -340 160 -160 440 1090 3050
AUTOBRAKE 3 6700 +150/-130 200 -430 1880 560 -280 170 -170 560 1050 3020
*Reference distance is for sea level, standard day, no wind or slope, VREF30 approach speed and 2 engine
reverse thrust.
Max Manual braking data valid for auto speedbrakes. For manual speedbrakes, increase reference landing
distance by 200 ft.
Autobrake data valid for both auto and manual speedbrakes.
Actual (unfactored) distances are shown.
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787机组操作手册Flight Crew Operations Manual 1(72)
