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MAX AUTO 3980 +60/-40 90 -170 610 0 0 90 -100 410 0 0
AUTOBRAKE 4 4940 +80/-60 130 -240 850 0 -20 130 -130 520 0 0
AUTOBRAKE 3 5970 +100-/80 160 -290 1060 40 -70 160 -160 560 10 20
AUTOBRAKE 2 6640 +120/-110 190 -340 1220 100 -140 180 -180 530 190 190
AUTOBRAKE 1 7010 +140/-120 220 -370 1360 160 -190 200 -190 530 480 580
MAX MANUAL 4040 +70/-70 100 -200 750 100 -90 100 -100 320 220 500
MAX AUTO 4450 +70/-70 110 -210 770 80 -50 100 -100 410 220 520
AUTOBRAKE 4 4960 +80/-80 130 -240 880 20 -30 130 -130 520 20 80
AUTOBRAKE 3 5970 +100/-110 160 -290 1060 40 -70 160 -160 560 10 20
MAX MANUAL 5420 +100/-100 160 -310 1240 260 -190 140 -140 410 580 1460
MAX AUTO 5720 +100/-100 160 -310 1230 240 -160 140 -140 480 550 1410
AUTOBRAKE 4 5720 +100/-100 160 -310 1250 220 -140 150 -150 510 540 1460
AUTOBRAKE 3 6250 +110/-110 170 -340 1330 180 -140 170 -170 560 280 980
MAX MANUAL 6930 +150/-140 230 -460 1960 630 -370 190 -180 470 1230 3390
MAX AUTO 7320 +150/-140 230 -450 1940 640 -360 190 -180 490 1240 3430
AUTOBRAKE 4 7320 +150/-140 230 -460 1950 620 -380 190 -180 460 1260 3470
AUTOBRAKE 3 7340 +150/-140 230 -470 1970 590 -330 200 -190 560 1100 3330
*Reference distance is for sea level, standard day, no wind or slope, VREF30 approach speed and 2 engine
reverse thrust.
Max Manual braking data valid for auto speedbrakes. For manual speedbrakes, increase reference landing
distance by 200 ft.
Autobrake data valid for both auto and manual speedbrakes.
Actual (unfactored) distances are shown.
Includes distance from 50 ft above threshold (1000 ft of air distance).
December 10, 2007
Advisory Information
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.31.2 D632W001-TBC
ADVISORY INFORMATION
Advisory Information Normal Configuration Landing Distance
Flaps 25
Dry Runway
Good Reported Braking Action
Medium Reported Braking Action
Poor Reported Braking Action
LANDING DISTANCE AND ADJUSTMENTS (FT)
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
BRAKING
CONFIGURATION
450000 LB
LANDING
WT
PER
10000 LB
ABOVE
BELOW
450000 LB
PER
1000 FT
ABOVE
S.L.
HEAD
WIND
TAIL
WIND
DN
HILL
UP
HILL
ABV
ISA
BLW
ISA
PER
10 KTS
ABOVE
VREF25
ONE
REV
NO
REV
MAX MANUAL 3050 +80/-40 70 -120 440 40 -30 60 -60 230 60 140
MAX AUTO 4210 +60/-40 100 -180 630 0 0 100 -100 420 0 0
AUTOBRAKE 4 5260 +90/-70 140 -250 880 0 -30 140 -140 530 0 0
AUTOBRAKE 3 6370 +110/-90 180 -310 1090 50 -90 170 -170 550 40 50
AUTOBRAKE 2 7020 +130/-120 210 -350 1250 120 -160 190 -190 520 300 300
AUTOBRAKE 1 7360 +150/-140 240 -380 1390 190 -210 210 -200 530 620 780
MAX MANUAL 4200 +70/-70 110 -200 760 100 -90 100 -100 320 250 580
MAX AUTO 4660 +70/-70 120 -210 790 70 -50 110 -110 420 230 580
AUTOBRAKE 4 5270 +90/-90 140 -250 910 20 -30 140 -140 530 20 80
AUTOBRAKE 3 6370 +110/-120 180 -310 1090 50 -90 170 -170 550 40 50
MAX MANUAL 5630 +110/-110 170 -320 1250 260 -200 150 -150 410 660 1680
MAX AUTO 5960 +110/-110 170 -310 1250 240 -160 150 -150 480 630 1630
AUTOBRAKE 4 5960 +110/-110 170 -320 1270 210 -140 160 -160 530 540 1620
AUTOBRAKE 3 6650 +120/-120 190 -350 1360 180 -160 180 -180 550 300 1080
MAX MANUAL 7180 +150/-150 240 -470 1980 640 -380 200 -190 470 1370 3900
MAX AUTO 7620 +150/-140 240 -460 1970 640 -370 200 -190 490 1380 3930
AUTOBRAKE 4 7620 +150/-140 240 -460 1970 620 -370 200 -190 480 1400 3990
AUTOBRAKE 3 7690 +150/-150 240 -470 2010 590 -350 210 -200 550 1180 3770
*Reference distance is for sea level, standard day, no wind or slope, VREF25 approach speed and 2 engine
reverse thrust.
Max Manual braking data valid for auto speedbrakes. For manual speedbrakes, increase reference landing
distance by 200 ft.
Autobrake data valid for both auto and manual speedbrakes.
Actual (unfactored) distances are shown.
Includes distance from 50 ft above threshold (1000 ft of air distance).
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.31.3
ADVISORY INFORMATION
Advisory Information Normal Configuration Landing Distance
　
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