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THRUST
ADJ
BRAKING
CONFIGURATION
180000 KG
LANDING
WT
PER
5000 KG
ABOVE /
BELOW
180000 KG
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 905 +30/-15 20 -35 125 10 -10 20 -20 70 15 35
MAX AUTO 1225 +25/-25 30 -55 180 0 0 30 -30 125 0 0
AUTOBRAKE 4 1520 +30/-35 40 -75 250 0 -5 40 -40 165 0 0
AUTOBRAKE 3 1815 +40/-40 50 -90 315 10 -20 50 -50 185 5 5
AUTOBRAKE 2 2000 +50/-50 60 -105 360 30 -45 55 -55 170 45 45
AUTOBRAKE 1 2110 +55/-55 70 -115 400 55 -65 60 -60 165 170 175
MAX MANUAL 1245 +25/-25 30 -60 215 30 -25 30 -30 100 65 160
MAX AUTO 1305 +25/-25 35 -65 225 20 -15 30 -30 120 75 175
AUTOBRAKE 4 1525 +35/-35 40 -75 260 5 -10 40 -40 165 5 25
AUTOBRAKE 3 1815 +40/-40 50 -90 315 10 -20 50 -50 185 5 5
MAX MANUAL 1665 +40/-40 50 -95 355 70 -60 40 -40 125 195 510
MAX AUTO 1665 +40/-40 50 -95 350 65 -45 40 -40 140 185 505
AUTOBRAKE 4 1685 +40/-40 50 -95 355 60 -40 45 -45 155 190 530
AUTOBRAKE 3 1895 +45/-45 55 -105 385 40 -35 50 -50 185 80 350
MAX MANUAL 2120 +55/-50 70 -140 550 165 -110 55 -55 145 415 1245
MAX AUTO 2120 +55/-50 70 -140 545 165 -110 55 -55 140 420 1260
AUTOBRAKE 4 2120 +55/-55 70 -140 545 160 -110 55 -55 145 425 1275
AUTOBRAKE 3 2150 +55/-50 70 -140 555 150 -90 55 -55 180 390 1245
*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 65 meters.
Autobrake data valid for both auto and manual speedbrakes.
Actual (unfactored) distances are shown.
Includes distance from 50 ft above threshold (305 meters of air distance).
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.21.4 D632W001-TBC
ADVISORY INFORMATION
Advisory Information Non-Normal Configuration Landing Distance
Dry Runway
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 913 +27/-17 21 -37 131 12 -12 73
ENGINE
SHUTDOWN
(FLAPS 30)
VREF30 834 +24/-13 18 -37 125 12 -9 70
FLAPS DRIVE
(FLAPS
BETWEEN
5 AND 20)
VREF30+ 20 959 +27/-13 21 -37 137 12 -12 67
FLAPS DRIVE
(FLAPS GREATER
THAN OR EQUAL
TO 20)
VREF20 904 +27/-13 21 -37 131 12 -9 67
FLAPS DRIVE
(FLAPS LESS
THAN OR EQUAL
TO 5)
VREF30+ 40 1051 +37/-13 27 -43 146 15 -12 76
FLAPS PRIMARY
FAIL VREF20 1013 +24/-17 21 -40 140 12 -12 85
FLAP/SLAT
CONTROL VREF20 898 +27/13 18 -37 131 12 -9 67
FLIGHT
CONTROL MODE VREF20 1038 +24/-17 24 -43 143 12 -12 91
HYD PRESS
SYS C VREF20 1013 +24/-17 21 -40 140 12 -12 85
HYD PRESS SYS
L+C VREF30+ 20 1165 +24/-20 27 -46 158 18 -15 110
HYD PRESS SYS
L+R VREF30+ 20 1126 +27/-17 27 -46 162 21 -18 113
HYD PRESS SYS
R+C VREF30+ 20 1198 +24/-20 27 -49 165 21 -18 122
PITCH UP
AUTHORITY
(FLAPS 5)
VREF30+ 40 1057 +34/-13 24 -43 146 12 -12 64
PITCH UP
AUTHORITY
(FLAPS 20)
VREF30+ 20 935 +27/-13 21 -37 134 12 -12 64
PRI FLIGHT
COMPUTERS VREF20 1038 +24/-17 24 -43 143 12 -12 91
SLATS DRIVE VREF30+ 30 1050 +27/-17 24 -40 140 12 -12 73
STABILIZER VREF30+ 20 974 +27/-17 21 -37 134 12 -12 70
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.
D632W001-TBC PI.21.5
　
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