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.12.7
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
ANTI-ICE LEAK
ENG L, R
(FLAPS 20)
VREF20 4400 80/-90 120/160 -210/750 120/-100 110/-110 340 0 380
ANTI-ICE LEAK
ENG L, R
(FLAPS 30)
VREF30 4210 80/-80 110/140 -210/730 110/-100 100/-100 330 0 310
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 5370 120/-120 170/230 -290/1080 210/-170 140/-140 380 690 1800
BRAKES
(FLAPS 30)
VREF30 5280 110/-120 160/220 -290/1080 210/-170 140/-140 380 640 1630
ENG FAIL L, R
(FLAPS 20)
VREF20 4330 80/-90 120/160 -210/730 110/-100 110/-110 340 0 430
ENG FAIL L, R
(FLAPS 30)
VREF30 4140 80/-80 110/140 -200/720 110/-90 100/-100 330 0 360
ENG LIMIT
EXCEED L, R
(FLAPS 20)
VREF20 4330 80/-90 120/160 -210/730 110/-100 110/-110 340 0 430
ENG LIMIT
EXCEED L, R
(FLAPS 30)
VREF30 4140 80/-80 110/140 -200/720 110/-90 100/-100 330 0 360
ENG OIL
FILTER L, R
(FLAPS 20)
VREF20 4330 80/-90 120/160 -210/730 110/-100 110/-110 340 0 430
ENG OIL
FILTER L, R
(FLAPS 30)
VREF30 4140 80/-80 110/140 -200/720 110/-90 100/-100 330 0 360
ENG OIL
PRESS L, R
(FLAPS 20)
VREF20 4330 80/-90 120/160 -210/730 110/-100 110/-110 340 0 430
ENG OIL
PRESS L, R
(FLAPS 30)
VREF30 4140 80/-80 110/140 -200/720 110/-90 100/-100 330 0 360
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