Boeing 787-8 - Page 277

787 Flight Crew Operations Manual
DO NOT USE FOR FLIGHT
Performance Inflight
Advisory Information
787-8/
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D615Z003-TBC PI.12.13
ADVISORY INFORMATION
Advisory Information
Non-Normal Configuration Landing Distance
Medium Reported Braking Action
LANDING DISTANCE AND ADJUSTMENT (FT)
REF
DIST
WT
ADJ
ALT
ADJ
WIND
ADJ PER
10 KTS
SLOPE
ADJ
PER 1%
TEMP
ADJ
PER
10°C
APP
SPEED
ADJ
REVERSE
THRUST
ADJ
EICAS
MESSAGE
REF SPEED
370000
LB
LDG
WT
PER
10000 LB
ABV/BLW
370000 LB
PER
1000 FT
ABV
S.L.
STD/
HIGH*
HEAD/
TAIL
WIND
DOWN/UP
HILL
ABV/
BLW
ISA
PER
10 KTS
ABV
VREF
ONE
REV
NO
REV
FLIGHT
CONTROL
MODE
(FLAPS 20)
VREF20 5890 130/-130 190/260 -320/1140 240/-190 150/-160 440 830 2280
FLIGHT
CONTROLS
(FLAPS 20)
VREF30+20 6420 140/-140 210/290 -330/1190 260/-210 170/-180 440 1020 2800
**FUEL LEAK
(FLAPS 20)
VREF20 6050 140/-140 190/260 -340/1220 300/-240 170/-170 450 0 1340
**FUEL LEAK
(FLAPS 30)
VREF30 5780 130/-130 170/230 -330/1200 290/-230 160/-160 440 0 1120
FUEL QTY LOW
(FLAPS 20)
VREF20 5460 120/-120 180/240 -300/1090 220/-180 140/-150 380 730 1950
HYD PRESS
SYS C
(FLAPS 20)
VREF20 5790 130/-130 180/250 -310/1130 230/-180 150/-150 420 790 2120
HYD PRESS
SYS L
(FLAPS 25)
VREF25 6160 130/-140 190/250 -350/1270 320/-250 160/-170 460 0 1180
HYD PRESS
SYS L
(FLAPS 30)
VREF30 6000 130/-130 180/240 -340/1250 320/-240 160/-160 460 0 1040
HYD PRESS
SYS L+C
(FLAPS 20)
VREF30+20 7630 160/-160 240/320 -400/1410 400/-310 210/-210 550 0 1750
HYD PRESS
SYS L+R
(FLAPS 20)
VREF30+20 9050 170/-180 260/340 -490/1720 690/-500 250/-250 680 0 0
HYD PRESS
SYS R
(FLAPS 25)
VREF25 6260 140/-140 190/260 -350/1280 330/-260 170/-170 480 0 1240
HYD PRESS
SYS R
(FLAPS 30)
VREF30 6080 130/-130 180/240 -350/1270 330/-250 160/-160 470 0 1080
HYD PRESS
SYS R+C
(FLAPS 20)
VREF30+20 7830 160/-170 250/330 -410/1440 420/-330 210/-220 580 0 1910
NAV AIR
DATA SYS
(FLAPS 20)
VREF20 5650 120/-120 180/240 -300/1110 210/-170 140/-150 400 730 1930
Actual (unfactored) distances are shown.
Includes distances from 50 ft above threshold (1000 ft air distance).
Assumes max manual braking and maximum available reverse thrust.
*Altitude adjustment - Use STD up to 8000 ft pressure altitude, above 8000 ft,
Adjustment = STD*8+HIGH*((Press Alt/1000)-8).
**Unannunciated Non-Normal Checklist condition.
February 15, 2010