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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.12.5
ADVISORY INFORMATION
Advisory Information
Non-Normal Configuration Landing Distance
Dry Runway
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 3350 70/-60 70/100 -130/440 40/-40 70/-70 260 80 170
FLIGHT
CONTROLS
(FLAPS 20)
VREF30+20 3550 80/-60 80/110 -130/460 50/-40 80/-80 260 110 250
**FUEL LEAK
(FLAPS 20)
VREF20 3050 80/-50 70/90 -120/420 40/-30 60/-70 230 0 100
**FUEL LEAK
(FLAPS 30)
VREF30 2930 80/-50 60/80 -120/410 40/-30 60/-60 220 0 90
FUEL QTY LOW
(FLAPS 20)
VREF20 3010 80/-50 70/90 -120/410 30/-30 60/-60 220 70 140
HYD PRESS
SYS C
(FLAPS 20)
VREF20 3300 80/-50 70/100 -130/440 40/-30 70/-70 250 70 160
HYD PRESS
SYS L
(FLAPS 25)
VREF25 3060 80/-50 70/90 -120/420 40/-40 60/-70 230 0 70
HYD PRESS
SYS L
(FLAPS 30)
VREF30 2990 70/-50 60/80 -120/420 40/-30 60/-60 230 0 70
HYD PRESS
SYS L+C
(FLAPS 20)
VREF30+20 3890 90/-60 90/120 -150/500 50/-50 90/-90 300 0 130
HYD PRESS
SYS L+R
(FLAPS 20)
VREF30+20 3770 110/-60 90/110 -150/500 60/-60 90/-90 300 0 0
HYD PRESS
SYS R
(FLAPS 25)
VREF25 3100 80/-50 70/90 -120/430 40/-40 70/-70 240 0 80
HYD PRESS
SYS R
(FLAPS 30)
VREF30 3020 70/-50 60/80 -120/420 40/-40 60/-60 240 0 70
HYD PRESS
SYS R+C
(FLAPS 20)
VREF30+20 3960 90/-60 90/120 -150/510 60/-50 90/-90 310 0 140
NAV AIR
DATA SYS
(FLAPS 20)
VREF20 3230 80/-50 70/90 -120/430 30/-30 70/-70 230 60 140
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

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