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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.
Includes distance from 50 ft above threshold (1000 ft of air distance).
December 15, 2006
787 Flight Crew Operations Manual
Performance Inflight A
Advisory Information
777-200ER/TRENT892
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
PI.A10.6 D615Z003 Boeing Proprietary
ADVISORY INFORMATION
Advisory Information Normal Configuration Landing Distance
Flaps 20
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
400000 LB
PER
1000 FT
ABOVE
S.L.
HEAD
WIND
TAIL
WIND
DN
HILL
UP
HILL
ABV
ISA
BLW
ISA
PER
10 KTS
ABOVE
VREF20
ONE
REV
NO
REV
MAX MANUAL 2980 +80/-50 60 -120 420 40 -30 60 -60 230 50 110
MAX AUTO 4040 +70/-70 90 -170 590 0 0 100 -100 410 0 0
AUTOBRAKE 4 5030 +100/-100 130 -240 820 0 -20 130 -130 540 0 0
AUTOBRAKE 3 6000 +120/-120 170 -300 1030 30 -60 170 -170 610 10 20
AUTOBRAKE 2 6610 +140/-150 200 -340 1180 90 -150 180 -190 570 150 150
AUTOBRAKE 1 6980 +160/-160 230 -380 1310 170 -210 200 -200 540 560 570
MAX MANUAL 4110 +80/-70 110 -200 710 100 -90 100 -100 320 220 530
MAX AUTO 4310 +80/-80 110 -210 730 70 -60 100 -100 390 240 570
AUTOBRAKE 4 5040 +100/-100 130 -240 850 20 -30 130 -130 540 20 90
AUTOBRAKE 3 6000 +120/-120 170 -300 1030 30 -60 170 -170 610 10 20
MAX MANUAL 5500 +120/-110 160 -310 1160 240 -190 140 -140 410 640 1680
MAX AUTO 5500 +120/-110 160 -310 1150 220 -160 140 -140 460 610 1660
AUTOBRAKE 4 5560 +120/-110 160 -310 1160 200 -130 140 -140 510 620 1730
AUTOBRAKE 3 6260 +130/-130 170 -340 1260 130 -120 170 -170 610 260 1160
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).
December 15, 2006
787 Flight Crew Operations Manual
Performance Inflight A
Advisory Information
777-200ER/TRENT892
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary PI.A10.7
ADVISORY INFORMATION
Advisory Information Non-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
　
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