Boeing 787-8 - Page 275

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.12.11
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
ANTI-ICE LEAK
ENG L, R
(FLAPS 20)
VREF20 6190 140/-140 190/260 -350/1270 320/-250 160/-170 460 0 1220
ANTI-ICE LEAK
ENG L, R
(FLAPS 30)
VREF30 5920 130/-130 180/230 -340/1240 310/-240 160/-160 440 0 1000
ANTISKID
(FLAPS 25)
VREF25 6740 170/-160 240/330 -420/1620 460/-320 190/-190 440 1420 4250
ANTISKID
(FLAPS 30)
VREF30 6660 160/-160 240/320 -420/1620 460/-320 180/-190 440 1330 3860
BRAKES
(FLAPS 25)
VREF25 6740 170/-160 240/330 -420/1620 460/-320 190/-190 440 1420 4250
BRAKES
(FLAPS 30)
VREF30 6660 160/-160 240/320 -420/1620 460/-320 180/-190 440 1330 3860
ENG FAIL L, R
(FLAPS 20)
VREF20 6050 140/-140 190/260 -340/1220 300/-240 170/-170 450 0 1340
ENG FAIL L, R
(FLAPS 30)
VREF30 5780 130/-130 170/230 -330/1200 290/-230 160/-160 440 0 1120
ENG LIMIT
EXCEED L, R
(FLAPS 20)
VREF20 6050 140/-140 190/260 -340/1220 300/-240 170/-170 450 0 1340
ENG LIMIT
EXCEED L, R
(FLAPS 30)
VREF30 5780 130/-130 170/230 -330/1200 290/-230 160/-160 440 0 1120
ENG OIL
FILTER L, R
(FLAPS 20)
VREF20 6050 140/-140 190/260 -340/1220 300/-240 170/-170 450 0 1340
ENG OIL
FILTER L, R
(FLAPS 30)
VREF30 5780 130/-130 170/230 -330/-1200 290/-230 160/-160 440 0 1120
ENG OIL
PRESS L, R
(FLAPS 20)
VREF20 6050 140/-140 190/260 -340/1220 300/-240 170/-170 450 0 1340
ENG OIL
PRESS L, R
(FLAPS 30)
VREF30 5780 130/-130 170/230 -330/1200 290/-230 160/-160 440 0 1120
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