Boeing 787-8 - Page 267

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.12.3
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
ANTI-ICE LEAK
ENG L, R
(FLAPS 20)
VREF20 3080 90/-50 70/90 -120/420 40/-40 60/-70 230 0 80
ANTI-ICE LEAK
ENG L, R
(FLAPS 30)
VREF30 2960 80/-50 60/80 -120/410 40/-30 60/-60 220 0 60
ANTISKID
(FLAPS 25)
VREF25 5370 120/-120 170/230 -290/1080 210/-170 140/-140 380 690 1800
ANTISKID
(FLAPS 30)
VREF30 5280 110/-120 160/220 -290/1080 210/-170 140/-140 380 640 1630
BRAKES
(FLAPS 25)
VREF25 4050 160/-80 110/170 -190/680 90/-80 100/-100 290 250 590
BRAKES
(FLAPS 30)
VREF30 3980 140/-80 100/140 -190/680 90/-80 90/-100 300 230 540
ENG FAIL L, R
(FLAPS 20)
VREF20 3050 80/-50 70/90 -120/420 40/-30 60/-70 230 0 100
ENG FAIL L, R
(FLAPS 30)
VREF30 2930 80/-50 60/80 -120/410 40/-30 60/-60 220 0 90
ENG LIMIT
EXCEED L, R
(FLAPS 20)
VREF20 3050 80/-50 70/90 -120/420 40/-30 60/-70 230 0 100
ENG LIMIT
EXCEED L, R
(FLAPS 30)
VREF30 2930 80/-50 60/80 -120/410 40/-30 60/-60 220 0 90
ENG OIL
FILTER L, R
(FLAPS 20)
VREF20 3050 80/-50 70/90 -120/420 40/-30 60/-70 230 0 100
ENG OIL
FILTER L, R
(FLAPS 30)
VREF30 2930 80/-50 60/80 -120/410 40/-30 60/-60 220 0 90
ENG OIL
PRESS L, R
(FLAPS 20)
VREF20 3050 80/-50 70/90 -120/420 40/-30 60/-70 230 0 100
ENG OIL
PRESS L, R
(FLAPS 30)
VREF30 2930 80/-50 60/80 -120/410 40/-30 60/-60 220 0 90
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).
February 15, 2010