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(FLAPS 30)
VREF30 5320 +110/-110 150 -320 1220 280 -210 430
FLAPS DRIVE
(FLAPS
BETWEEN
5 AND 20)
VREF30+ 20 5890 +120/-120 180 -310 1200 240 -190 400
FLAPS DRIVE
(FLAPS GREATER
THAN OR EQUAL
TO 20)
VREF20 5500 +120/-120 170 -300 1180 240 -190 400
FLAPS DRIVE
(FLAPS LESS
THAN OR EQUAL
TO 5)
VREF30+ 40 6530 +130/-130 220 -330 1260 260 -210 400
FLAPS PRIMARY
FAIL VREF20 5990 +130/-130 180 -320 1240 270 -210 470
FLAP/SLAT
CONTROL VREF20 5430 +110/110 160 -300 1160 230 -180 390
FLIGHT
CONTROL MODE VREF20 6180 +130/-130 190 -330 1260 290 -220 510
HYD PRESS
SYS C VREF20 5990 +130/-130 180 -320 1240 270 -210 470
HYD PRESS SYS
L+C VREF30+ 20 7740 +150/-150 260 -420 1540 480 -350 660
HYD PRESS SYS
L+R VREF30+ 20 9010 +160/-160 260 -510 1850 840 -550 800
HYD PRESS SYS
R+C VREF30+ 20 7900 +150/-150 250 -420 1560 500 -370 690
PITCH UP
AUTHORITY
(FLAPS 5)
VREF30+ 40 6490 +120/-120 200 -320 1240 250 -200 370
PITCH UP
AUTHORITY
(FLAPS 20)
VREF30+ 20 5690 +110/-110 170 -310 1180 230 -180 370
PRI FLIGHT
COMPUTERS VREF20 6180 +130/-130 190 -330 1260 290 -220 510
SLATS DRIVE VREF30+ 30 6340 +120/-120 200 -330 1240 260 -210 410
STABILIZER VREF30+ 20 5910 +120/-120 180 -320 1210 250 -200 400
Actual (unfactored) distances are shown.
Includes distance from 50 ft above threshold to stop (1000 ft of air distance).
Assumes maximum manual braking and maximum available reverse thrust.
December 15, 2006
787 Flight Crew Operations Manual
Performance Inflight A
Advisory Information
777-200ER/TRENT892
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
PI.A10.10 D615Z003 Boeing Proprietary
ADVISORY INFORMATION
Advisory Information Non-Normal Configuration Landing Distance
Poor Reported Braking Action
LANDING DISTANCE AND ADJUSTMENTS (FT)
REFERENCE
DISTANCE
FOR
400000 LB
LANDING
WT
WT
ADJUST
PER
10000 LB
ABOVE/
BELOW
400000 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 6320 +140/-130 210 -430 1800 570 -340 440
ENGINE
SHUTDOWN
(FLAPS 20)
VREF20 8040 +190/-190 270 -520 2040 830 -500 560
ENGINE
SHUTDOWN
(FLAPS 30)
VREF30 7080 +160/-160 220 -480 1980 730 -440 510
FLAPS DRIVE
(FLAPS
BETWEEN
5 AND 20)
VREF30+ 20 7480 +160/-160 250 -460 1910 600 -360 470
FLAPS DRIVE
(FLAPS GREATER
THAN OR EQUAL
TO 20)
VREF20 7000 +160/-160 230 -450 1840 560 -350 460
FLAPS DRIVE
(FLAPS LESS
THAN OR EQUAL
TO 5)
VREF30+ 40 8320 +180/-180 300 -480 1960 610 -390 480
FLAPS PRIMARY
FAIL VREF20 7530 +180/-180 250 -470 1910 610 -390 530
FLAP/SLAT
CONTROL VREF20 6900 +160/160 230 -440 1820 550 -350 450
FLIGHT
CONTROL MODE VREF20 7790 +190/-190 270 -480 1950 650 -410 570
HYD PRESS
SYS C VREF20 7530 +180/-180 250 -470 1910 610 -390 530
HYD PRESS SYS
L+C VREF30+ 20 10430 +220/-220 360 -650 2560 1300 -730 760
HYD PRESS SYS
L+R VREF30+ 20 13990 +240/-240 400 -920 3550 3300 -1450 1000
HYD PRESS SYS
R+C VREF30+ 20 10570 +230/-230 370 -660 2580 1340 -750 780
PITCH UP
AUTHORITY
(FLAPS 5)
VREF30+ 40 8180 +170/-170 280 -470 1950 570 -370 430
PITCH UP
AUTHORITY
(FLAPS 20)
VREF30+ 20 7220 +160/-160 240 -450 1880 550 -350 430
PRI FLIGHT
COMPUTERS VREF20 7790 +190/-190 270 -480 1950 650 -410 570
SLATS DRIVE VREF30+ 30 7960 +170/-170 270 -480 1920 600 -390 460
STABILIZER VREF30+ 20 7450 +160/-160 250 -460 1880 580 -370 460
Actual (unfactored) distances are shown.
Includes distance from 50 ft above threshold to stop (1000 ft of air distance).
Assumes maximum manual braking and maximum available reverse thrust.
December 15, 2006
787 Flight Crew Operations Manual
Performance Inflight A
Advisory Information
777-200ER/TRENT892
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D615Z003 Boeing Proprietary PI.A10.11
ADVISORY INFORMATION
Advisory Information Recommended Brake Cooling Schedule
Reference Brake Energy (Millions of Foot Pounds)
BRAKES ON SPEED (KIAS)
80 100 120 140 160 180
　
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