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ADVISORY INFORMATION
Advisory Information Non-Normal Configuration Landing Distance
Good Reported Braking Action
LANDING DISTANCE AND ADJUSTMENTS (M)
REFERENCE
DISTANCE
FOR
180000 KG
LANDING
WT
WT
ADJUST
PER
5000 KG
ABOVE/
BELOW
180000 KG
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 1505 +34/-34 46 -88 347 70 -52 119
ENGINE
SHUTDOWN
(FLAPS 20)
VREF20 1297 +27/-27 34 -64 226 37 -30 107
ENGINE
SHUTDOWN
(FLAPS 30)
VREF30 1164 +24/-24 30 -61 219 30 -27 101
FLAPS DRIVE
(FLAPS
BETWEEN
5 AND 20)
VREF30+ 20 1334 +24/-24 37 -61 226 30 -27 98
FLAPS DRIVE
(FLAPS GREATER
THAN OR EQUAL
TO 20)
VREF20 1245 +27/-27 34 -61 219 30 -24 94
FLAPS DRIVE
(FLAPS LESS
THAN OR EQUA
L TO 5)
VREF30+ 40 1467 +27/-27 43 -64 235 34 -27 91
FLAPS PRIMARY
FAIL VREF20 1376 +27/-27 37 64 235 34 -30 116
FLAP/SLAT
CONTROL VREF20 1234 +24/-24 34 -61 216 30 -24 94
FLIGHT
CONTROL MODE VREF20 1415 +30/-30 37 -67 238 37 -30 125
HYD PRESS
SYS C VREF20 1376 +27/-27 37 64 235 34 -30 116
HYD PRESS SYS
L+C VREF30+ 20 1671 +30/-30 49 -79 277 55 -46 155
HYD PRESS SYS
L+R VREF30+ 20 1741 +30/-30 52 -88 302 76 -61 177
HYD PRESS SYS
R+C VREF30+ 20 1712 +34/-34 49 -79 280 58 -49 168
PITCH UP
AUTHORITY
(FLAPS 5)
VREF30+ 40 1474 +27/-27 40 -64 232 30 -27 88
PITCH UP
AUTHORITY
(FLAPS 20)
VREF30+ 20 1292 +24/-24 34 -61 219 30 -24 88
PRI FLIGHT
COMPUTERS VREF20 1415 +30/-30 37 -67 238 37 -30 125
SLATS DRIVE VREF30+ 30 1449 +27/-27 40 -67 238 34 -30 101
STABILIZER VREF30+ 20 1346 +27/-27 37 -61 229 34 -27 98
Actual (unfactored) distances are shown.
Includes distance from 50 ft above threshold to stop (305 m of air distance).
Assumes maximum manual braking and maximum available reverse thrust.
December 10, 2007
777 Flight Crew Operations Manual
Performance Inflight
Advisory Information
777-200ER/TRENT892
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
PI.21.6 D632W001-TBC
ADVISORY INFORMATION
Advisory Information Non-Normal Configuration Landing Distance
Medium Reported Braking Action
LANDING DISTANCE AND ADJUSTMENTS (M)
REFERENCE
DISTANCE
FOR
180000 KG
LANDING
WT
WT
ADJUST
PER
5000 KG
ABOVE/
BELOW
180000 KG
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 1505 +34/-34 46 -88 347 70 -52 119
ENGINE
SHUTDOWN
(FLAPS 20)
VREF20 1816 +44/-44 55 -104 384 98 -73 140
ENGINE
SHUTDOWN
(FLAPS 30)
VREF30 1611 +37/-37 46 -98 372 85 -64 131
FLAPS DRIVE
(FLAPS
BETWEEN
5 AND 20)
VREF30+ 20 1784 +40/-40 55 -94 336 73 -58 122
FLAPS DRIVE
(FLAPS GREATER
THAN OR EQUAL
TO 20)
VREF20 1665 +40/-40 52 -91 360 73 -58 122
FLAPS DRIVE
(FLAPS LESS
THAN OR EQUAL
TO 5)
VREF30+ 40 1978 -44/-44 67 -101 384 79 -64 122
FLAPS PRIMARY
FAIL VREF20 1813 +44/-44 55 -98 378 82 -64 143
FLAP/SLAT
CONTROL VREF20 1644 +37/-37 49 -91 354 70 -55 119
FLIGHT
CONTROL MODE VREF20 1871 +44/-44 58 -101 384 88 -67 155
HYD PRESS
SYS C VREF20 1813 +44/-44 55 -98 378 82 -64 143
HYD PRESS SYS
L+C VREF30+ 20 2345 +50/-50 79 -128 469 146 -107 201
HYD PRESS SYS
L+R VREF30+ 20 2731 +54/-54 79 -155 564 256 -168 244
HYD PRESS SYS
R+C VREF30+ 20 2393 +50/-50 76 -128 475 152 -113 210
PITCH UP
AUTHORITY
(FLAPS 5)
VREF30+ 40 1967 +40/-40 61 -98 378 76 -61 113
PITCH UP
AUTHORITY
(FLAPS 20)
VREF30+ 20 1724 +37/-37 52 -94 360 70 -55 113
PRI FLIGHT
COMPUTERS VREF20 1871 +44/-44 58 -101 384 88 -67 155
SLATS DRIVE VREF30+ 30 1921 +40/-40 61 -101 378 79 -64 125
STABILIZER VREF30+ 20 1790 +40/-40 55 -98 369 76 -61 122
Actual (unfactored) distances are shown.
Includes distance from 50 ft above threshold to stop (305 m of air distance).
　
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