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Assumes maximum manual braking and maximum available reverse thrust.
December 10, 2007
777 Operations Manual
Performance Inflight
Advisory Information
777-200/GE90-76B
JAA/JAROPS
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D632W001-TBC PI.11.5
ADVISORY INFORMATION
Advisory Information Non-Normal Configuration Landing Distance
Good Reported Braking Action
LANDING DISTANCE AND ADJUSTMENT (M)
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
EICAS
MESSAGE VREF
180000
KG
LDG
WT
PER
5000 KG
ABV/BLW
180000 KG
PER
1000 FT
ABV
S.L.
HEAD/
TAIL
WIND
DOWN/
UP
HILL
ABV/
BLW
ISA
PER
10 KTS
ABV
VREF
ONE
REV
NO
REV
ANTISKID
(FLAPS 25) VREF25 1565 35/-35 50 -90/350 70/-50 20/-20 115 220 590
ANTISKID
(FLAPS 30) VREF30 1490 35/-35 45 -90/345 70/-50 20/-20 115 195 520
ENG SHUTDOWN
L, R (FLAPS 20) VREF20 1290 25/-25 35 -65/225 35/-30 20/-20 105 - 115
ENG SHUTDOWN
L, R (FLAPS 30) VREF30 1160 25/-25 30 -60/220 30/-25 15/-15 100 - 80
FLAPS DRIVE
(FLAPS ≤ 5) VREF30+40 1475 25/-25 45 -65/235 35/-25 20/-20 90 130 315
FLAPS DRIVE
(5 < FLAPS < 20) VREF30+20 1330 25/-25 35 -60/225 30/-25 20/-20 100 105 255
FLAPS DRIVE
(FLAPS ≥ 20) VREF20 1235 25/-25 35 -60/220 30/-25 15/-15 95 90 210
FLAPS PRIMARY
FAIL VREF20 1365 25/-25 35 -65/235 35/-30 20/-20 115 105 255
FLAP/SLAT
CONTROL VREF20 1225 25/-25 35 -60/215 30/-25 15/-15 95 85 205
FLIGHT
CONTROL MODE VREF20 1405 30/-30 35 -65/240 35/-30 20/-20 125 115 285
HYD PRESS SYS C VREF20 1365 25/-25 35 -65/235 35/-30 20/-20 115 105 255
HYD PRESS
SYS L+C VREF30+20 1685 30/-30 50 -80/275 55/-45 25/-25 155 - 215
HYD PRESS
SYS L+R VREF30+20 1800 30/-30 50 -90/315 85/-65 25/-25 180 - -
HYD PRESS
SYS R+C VREF30+20 1730 35/-35 50 -80/290 65/-50 25/-25 170 - 235
HYD PRESS SYS L
(FLAPS 25) VREF25 1330 25/-25 35 -65/245 45/-35 20/-20 120 - 130
HYD PRESS SYS L
(FLAPS 30) VREF30 1265 25/-25 35 -65/240 45/-35 20/-20 120 - 115
HYD PRESS SYS R
(FLAPS 25) VREF25 1330 25/-25 35 -65/245 45/-35 20/-20 120 - 130
HYD PRESS SYS R
(FLAPS 30) VREF30 1250 25/-25 35 -65/240 40/-35 20/-20 120 - 110
PITCH UP
AUTHORITY
(FLAPS 5)
VREF30+40 1470 25/-25 40 -65/230 30/-25 20/-20 90 115 275
PITCH UP
AUTHORITY
(FLAPS 20)
VREF30+20 1285 25/-25 35 -60/220 30/-25 20/-20 90 90 210
PRI FLIGHT
COMPUTERS VREF20 1405 30/-30 35 -65/240 35/-30 20/-20 125 115 285
SLATS DRIVE VREF30+30 1435 25/-25 40 -65/240 35/-30 20/-20 100 115 275
STABILIZER VREF30+20 1335 25/-25 35 -60/230 35/-25 20/-20 100 100 245
Actual (unfactored) distances are shown.
Includes distances from 50 ft above threshold (305 m air distance).
Assumes maximum manual braking and maximum available reverse thrust.
December 10, 2007
777 Operations Manual
Performance Inflight
Advisory Information
777-200/GE90-76B
JAA/JAROPS
Category A Brakes
Copyright © The Boeing Company. See title page for details.
PI.11.6 D632W001-TBC
ADVISORY INFORMATION
Advisory Information Non-Normal Configuration Landing Distance
Medium Reported Braking Action
LANDING DISTANCE AND ADJUSTMENT (M)
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
EICAS
MESSAGE VREF
180000
KG
LDG
WT
PER
5000 KG
ABV/BLW
180000 KG
PER
1000 FT
ABV
S.L.
HEAD/
TAIL
WIND
DOWN/
UP
HILL
ABV/
BLW
ISA
PER
10 KTS
ABV
VREF
ONE
REV
NO
REV
ANTISKID
(FLAPS 25) VREF25 1975 50/-45 65 -130/545 170/-100 25/-30 135 490 1630
ANTISKID
(FLAPS 30) VREF30 1885 50/-45 65 -130/535 165/-100 25/-25 130 440 1450
ENG SHUTDOWN
L, R (FLAPS 20) VREF20 1805 45/-45 55 -105/385 100/-75 25/-25 140 - 370
ENG SHUTDOWN
L, R (FLAPS 30) VREF30 1600 35/-35 45 -100/370 85/-65 25/-25 130 - 270
FLAPS DRIVE
(FLAPS ≤ 5) VREF30+40 1995 45/-45 65 -100/385 80/-65 30/-30 120 355 1030
FLAPS DRIVE
(5 < FLAPS < 20) VREF30+20 1785 40/-40 55 -95/365 75/-60 25/-25 120 295 820
　
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