Boeing 787-8 - Page 273

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.12.9
ADVISORY INFORMATION
Advisory Information
Non-Normal Configuration Landing Distance
Good 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 4500 90/-90 120/170 -210/730 100/-90 110/-110 350 310 760
FLIGHT
CONTROLS
(FLAPS 20)
VREF30+20 4890 90/-90 140/190 -220/760 120/-100 120/-130 360 410 1000
**FUEL LEAK
(FLAPS 20)
VREF20 4330 80/-90 120/160 -210/730 110/-100 110/-110 340 0 430
**FUEL LEAK
(FLAPS 30)
VREF30 4140 80/-80 110/140 -200/720 110/-90 100/-100 330 0 360
FUEL QTY LOW
(FLAPS 20)
VREF20 4120 80/-80 110/150 -190/690 90/-80 100/-100 300 270 650
HYD PRESS
SYS C
(FLAPS 20)
VREF20 4430 80/-90 120/160 -200/720 100/-90 100/-110 340 290 710
HYD PRESS
SYS L
(FLAPS 25)
VREF25 4370 80/-90 110/150 -210/750 120/-100 110/-110 340 0 360
HYD PRESS
SYS L
(FLAPS 30)
VREF30 4260 80/-80 110/140 -210/740 120/-100 100/-110 340 0 320
HYD PRESS
SYS L+C
(FLAPS 20)
VREF30+20 5500 100/-100 150/200 -250/860 150/-130 140/-140 420 0 580
HYD PRESS
SYS L+R
(FLAPS 20)
VREF30+20 5810 100/-110 150/200 -270/940 210/-180 150/-160 480 0 0
HYD PRESS
SYS R
(FLAPS 25)
VREF25 4430 80/-90 120/150 -210/760 120/-100 110/-110 360 0 380
HYD PRESS
SYS R
(FLAPS 30)
VREF30 4310 80/-80 110/150 -210/740 120/-100 100/-110 350 0 330
HYD PRESS
SYS R+C
(FLAPS 20)
VREF30+20 5630 100/-110 150/200 -250/870 160/-140 140/-150 450 0 630
NAV AIR
DATA SYS
(FLAPS 20)
VREF20 4330 80/-80 110/160 -200/710 90/-80 100/-100 320 270 640
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