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MAX MANUAL 7000 +170/-160 230 -460 1800 540 -360 180 -180 470 1370 4080
MAX AUTO 7000 +170/-160 230 -450 1790 550 -360 180 -180 460 1380 4130
AUTOBRAKE 4 7000 +170/-160 230 -450 1790 520 -360 180 -180 470 1400 4180
AUTOBRAKE 3 7100 +170/-160 230 -460 1820 500 -300 190 -190 590 1280 4080
*Reference distance is for sea level, standard day, no wind or slope, VREF20 approach speed and 2 engine
reverse thrust.
Max Manual braking data valid for auto speedbrakes. For manual speedbrakes, increase reference landing
distance by 210 ft.
Autobrake data valid for both auto and manual speedbrakes.
Actual (unfactored) distances are shown.
Includes distance from 50 ft above threshold (1000 ft of air distance).
787 Flight Crew Operations Manual
Performance Inflight
Advisory Information
FAA
Category A Brakes
PI.12.4 Boeing Proprietary
ADVISORY INFORMATION
Advisory InformationNon-Normal Configuration Landing Distance
Dry Runway
LANDING DISTANCE AND ADJUSTMENTS (FT)
REFERENCE
DISTANCE
FOR
400000 LB
LANDING
WT
WT
ADJUST
PER
10000 LB
ABOVE/
BELOW
400000 LB
ALT
ADJUST
PER
1000 FT
ABOVE
S.L.
WIND ADJ
PER 10 KTS
SLOPE ADJ
PER 1%
APPROACH
SPEED
EICAS
MESSAGE VREF HEAD
WIND
TAIL
WIND
DOWN
HILL
UP
HILL
PER
10 KTS
ABOVE
VREF
ANTISKID VREF30 4970 +100/-100 150 -290 1140 230 -170 390
ENGINE
SHUTDOWN
(FLAPS 20)
VREF20 3010 +80/-50 70 -120 430 40 -40 240
ENGINE
SHUTDOWN
(FLAPS 30)
VREF30 2750 +70/-40 60 -120 410 40 -30 230
FLAPS DRIVE
(FLAPS
BETWEEN
5 AND 20)
VREF30+ 20 3160 +80/-40 70 -120 450 40 -40 220
FLAPS DRIVE
(FLAPS GREATER
THAN OR EQUAL
TO 20)
VREF20 2980 +80/-40 70 -120 430 40 -30 220
FLAPS DRIVE
(FLAPS LESS
THAN OR EQUAL
TO 5)
VREF30+ 40 3460 +110/-40 90 -140 480 50 -40 250
FLAPS PRIMARY
FAIL VREF20 3340 +70/-50 70 -130 460 40 -40 280
FLAP/SLAT
CONTROL VREF20 2960 +80/-40 60 -120 430 40 -30 220
FLIGHT
CONTROL MODE VREF20 3420 +70/-50 80 -140 470 40 -40 300
HYD PRESS
SYS C VREF20 3340 +70/-50 70 -130 460 40 -40 280
HYD PRESS SYS
L+C VREF30+ 20 3840 +70/-60 90 -150 520 60 -50 360
HYD PRESS SYS
L+R VREF30+ 20 3710 +80/-50 90 -150 530 70 -60 370
HYD PRESS SYS
R+C VREF30+ 20 3950 +70/-60 90 -160 540 70 -60 400
PITCH UP
AUTHORITY
(FLAPS 5)
VREF30+ 40 3480 +100/-40 80 -140 480 40 -40 210
PITCH UP
AUTHORITY
(FLAPS 20)
VREF30+ 20 3080 +80/-40 70 -120 440 40 -40 210
PRI FLIGHT
COMPUTERS VREF20 3420 +70/-50 80 -140 470 40 -40 300
SLATS DRIVE VREF30+ 30 3460 +80/-50 80 -130 460 40 -40 240
STABILIZER VREF30+ 20 3210 +80/-50 70 -120 440 40 -40 230
Actual (unfactored) distances are shown.
Includes distance from 50 ft above threshold to stop (1000 ft of air distance).
Assumes maximum manual braking and maximum available reverse thrust.
787 Flight Crew Operations Manual
Performance Inflight
Advisory Information
FAA
Category A Brakes
Boeing Proprietary PI.12.5
ADVISORY INFORMATION
Advisory InformationNon-Normal Configuration Landing Distance
Good Reported Braking Action
LANDING DISTANCE AND ADJUSTMENTS (FT)
REFERENCE
DISTANCE
FOR
400000 LB
LANDING
WT
WT
ADJUST
PER
10000 LB
ABOVE/
BELOW
400000 LB
ALT
ADJUST
PER
1000 FT
ABOVE
S.L.
WIND ADJ
PER 10 KTS
SLOPE ADJ
PER 1%
APPROACH
SPEED
EICAS
MESSAGE VREF HEAD
WIND
TAIL
WIND
DOWN
HILL
UP
HILL
PER
10 KTS
ABOVE
VREF
ANTISKID VREF30 4970 +100/-100 150 -290 1140 230 -170 390
ENGINE
SHUTDOWN
(FLAPS 20)
VREF20 4280 +80/-80 110 -210 740 120 -100 350
ENGINE
SHUTDOWN
(FLAPS 30)
VREF30 3840 +70/-70 100 -200 720 100 -90 330
FLAPS DRIVE
(FLAPS
BETWEEN
5 AND 20)
VREF30+ 20 4400 +70/-70 120 -200 740 100 -90 320
FLAPS DRIVE
(FLAPS GREATER
THAN OR EQUAL
TO 20)
VREF20 4110 +80/-80 110 -200 720 100 -80 310
FLAPS DRIVE
(FLAPS LESS
THAN OR EQUAL
TO 5)
VREF30+ 40 4840 +80/-80 140 -210 770 110 -90 300
FLAPS PRIMARY
FAIL VREF20 4540 +80/-80 120 210 770 110 -100 380
FLAP/SLAT
CONTROL VREF20 4070 +70/70 110 -200 710 100 -80 310
FLIGHT
CONTROL MODE VREF20 4670 +90/-90 120 -220 780 120 -100 410
　
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