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STABILIZER VREF30+20 3440 +90/-50 80 -140 480 50 -40 260
Actual (unfactored) distances are shown.
Includes distance from 50 ft above threshold to stop (1000 ft air distance).
Assumes maximum manual braking and maximum available reverse thrust.
December 10, 2007
777 Flight Crew Operations Manual
Performance Inflight
Advisory Information
777-300/PW4090
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D632W001-TBC PI.31.5
ADVISORY INFORMATION
Advisory Information Non-Normal Configuration Landing Distance
Good Reported Braking Action
LANDING DISTANCE AND ADJUSTMENTS (FT)
REFERENCE
DISTANCE
FOR
450000 LB
LANDING
WEIGHT
WT
ADJUST
PER
10000 LB
ABOVE/
BELOW
450000 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 5420 +100/-100 170 -310 1190 260 -190 410
ENGINE
SHUTDOWN
(FLAPS 20)
VREF20 4740 +80/-80 130 -220 810 140 -110 380
ENGINE
SHUTDOWN
(FLAPS 30)
VREF30 4210 +70/-70 110 -200 760 120 -100 350
FLAPS DRIVE
(FLAPS
BETWEEN
5 AND 20)
VREF30+20 4750 +80/-80 140 -210 780 120 -100 340
FLAPS DRIVE
(FLAPS GREATER
THAN OR EQUAL
TO 20)
VREF20 4510 +80/-80 130 -210 760 120 -100 340
FLAPS DRIVE
(FLAPS LESS
THAN OR EQUAL
TO 5)
VREF30+40 5290 +80/-80 160 -220 820 120 -100 330
FLAPS PRIMARY
FAIL VREF20 4970 +80/-90 140 -220 820 130 -110 410
FLAP/SLAT
CONTROL VREF20 4460 +80/-80 120 -210 760 110 -90 330
FLIGHT
CONTROL MODE VREF20 5120 +90/-90 150 -230 840 140 -120 440
HYD PRESS SYS
C VREF20 4970 +80/-90 140 -220 820 130 -110 410
HYD PRESS SYS
L+C VREF30+20 5980 +100/-90 180 -270 960 210 -160 540
HYD PRESS SYS
L+R VREF30+20 6320 +100/-100 190 -300 1040 270 -210 610
HYD PRESS SYS
R+C VREF30+20 6140 +100/-100 180 -270 980 220 -180 590
PITCH UP
AUTHORITY
(FLAPS 5)
VREF30+40 5220 +80/-80 150 -220 810 120 -110 310
PITCH UP
AUTHORITY
(FLAPS 20)
VREF30+20 4590 +70/-70 130 -210 770 110 -90 310
PRI FLIGHT
COMPUTERS VREF20 5120 +90/-90 150 -230 840 140 -120 440
SLATS DRIVE VREF30+30 5150 +80/-80 150 -220 820 130 -110 350
STABILIZER VREF30+20 4790 +80/-80 140 -220 790 120 -100 350
Actual (unfactored) distances are shown.
Includes distance from 50 ft above threshold to stop (1000 ft air distance).
Assumes maximum manual braking and maximum available reverse thrust.
December 10, 2007
777 Flight Crew Operations Manual
Performance Inflight
Advisory Information
777-300/PW4090
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
PI.31.6 D632W001-TBC
ADVISORY INFORMATION
Advisory Information Non-Normal Configuration Landing Distance
Medium Reported Braking Action
LANDING DISTANCE AND ADJUSTMENTS (FT)
REFERENCE
DISTANCE
FOR
450000 LB
LANDING
WEIGHT
WT
ADJUST
PER
10000 LB
ABOVE/
BELOW
450000 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 5420 +100/ -100 170 -310 1190 260 -190 410
ENGINE
SHUTDOWN
(FLAPS 20)
VREF20 6720 +130/-130 210 -360 1380 380 -280 500
ENGINE
SHUTDOWN
(FLAPS 30)
VREF30 5870 +110/-110 180 -340 1290 330 -240 460
FLAPS DRIVE
(FLAPS
BETWEEN
5 AND 20)
VREF30+20 6400 +120/-120 210 -340 1280 290 -220 440
FLAPS DRIVE
(FLAPS GREATER
THAN OR EQUAL
TO 20)
VREF20 6090 +120/-120 200 -330 1260 290 -210 430
FLAPS DRIVE
(FLAPS LESS
THAN OR EQUAL
TO 5)
VREF30+40 7240 +130/-130 250 -350 1340 310 -240 440
FLAPS PRIMARY
FAIL VREF20 6610 +130/-130 220 -350 1320 320 -240 500
FLAP/SLAT
CONTROL VREF20 6000 +120/-110 190 -320 1240 280 -210 420
FLIGHT
CONTROL MODE VREF20 6840 +140/-130 230 -360 1350 350 -260 550
HYD PRESS SYS
C VREF20 6610 +130/-130 220 -350 1320 320 -240 500
HYD PRESS SYS
L+C VREF30+20 8480 +150/-150 290 -440 1620 570 -400 700
　
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