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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.
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.A10.8 D615Z003 Boeing Proprietary
ADVISORY INFORMATION
Advisory Information Non-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
HYD PRESS
SYS C VREF20 4540 +80/-80 120 -210 770 110 -100 380
HYD PRESS SYS
L+C VREF30+ 20 5510 +90/-90 160 -260 910 180 -150 510
HYD PRESS SYS
L+R VREF30+ 20 5740 +90/-90 170 -290 990 250 -200 580
HYD PRESS SYS
R+C VREF30+ 20 5650 +100/-100 160 -260 920 190 -160 550
PITCH UP
AUTHORITY
(FLAPS 5)
VREF30+ 40 4860 +80/-80 130 -210 760 100 -90 290
PITCH UP
AUTHORITY
(FLAPS 20)
VREF30+ 20 4260 +70/-70 110 -200 720 100 -80 290
PRI FLIGHT
COMPUTERS VREF20 4670 +90/-90 120 -220 780 120 -100 410
SLATS DRIVE VREF30+ 30 4780 +80/-80 130 -220 780 110 -100 330
STABILIZER VREF30+ 20 4440 +80/-80 120 -200 750 110 -90 320
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.
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.A10.9
ADVISORY INFORMATION
Advisory Information Non-Normal Configuration Landing Distance
Medium 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 6000 +130/-130 180 -340 1260 320 -240 460
ENGINE
SHUTDOWN
　
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