Boeing 787-8 - Page 276

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.
PI.12.12 D615Z003-TBC
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
ENG OIL
TEMP L, R
(FLAPS 20)
VREF20 6050 140/-140 190/260 -340/1220 300/-240 170/-170 450 0 1340
ENG OIL
TEMP L, R
(FLAPS 30)
VREF30 5780 130/-130 170/230 -330/1200 290/-230 160/-160 440 0 1120
ENG SURGE L, R
(FLAPS 20)
VREF20 6050 140/-140 190/260 -340/1220 300/-240 170/-170 450 0 1340
ENG SURGE L, R
(FLAPS 30)
VREF30 5780 130/-130 170/230 -330/1200 290/-230 160/-160 440 0 1120
**ENG SVR
DAMAGE/SEP
L, R
(FLAPS 20)
VREF20 6050 140/-140 190/260 -340/1220 300/-240 170/-170 450 0 1340
**ENG SVR
DAMAGE/SEP
L, R
(FLAPS 30)
VREF30 5780 130/-130 170/230 -330/1200 290/-230 160/-160 440 0 1120
FIRE ENG L, R
(FLAPS 20)
VREF20 6050 140/-140 190/260 -340/1220 300/-240 170/-170 450 0 1340
FIRE ENG L, R
(FLAPS 30)
VREF30 5780 130/-130 170/230 -330/1200 290/-230 160/-160 440 0 1120
FLAP/SLAT
CONTROL
(FLAPS 20)
VREF20 5460 120/-120 180/240 -300/1090 220/-180 140/-150 380 730 1950
FLAPS DRIVE
(UP < FLAPS ≤ 1)
VREF30+40 6440 130/-130 210/280 -310/1140 220/-180 170/-180 340 980 2690
FLAPS DRIVE
(1 < FLAPS ≤ 5)
VREF30+40 6750 140/-140 220/300 -330/1180 240/-200 180/-190 370 1000 2680
FLAPS DRIVE
(5 < FLAPS < 20)
VREF30+20 6070 130/-130 200/260 -310/1140 230/-190 160/-170 390 870 2330
FLAPS DRIVE
(FLAPS ≥ 20)
VREF20 5460 120/-120 180/240 -300/1090 220/-180 140/-150 380 730 1950
FLAPS PRIMARY
FAIL
(FLAPS 20)
VREF20 5790 130/-130 180/250 -310/1130 230/-180 150/-150 420 790 2120
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