Boeing 787-8 - Page 280

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.12.16 D615Z003-TBC
ADVISORY INFORMATION
Advisory Information
Non-Normal Configuration Landing Distance
Poor 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 8050 200/-200 290/390 -510/1940 730/-480 240/-240 550 0 3320
ENG OIL
TEMP L, R
(FLAPS 30)
VREF30 7700 190/-190 260/350 -500/1900 710/-460 220/-230 530 0 2770
ENG SURGE L, R
(FLAPS 20)
VREF20 8050 200/-200 290/390 -510/1940 730/-480 240/-240 550 0 3320
ENG SURGE L, R
(FLAPS 30)
VREF30 7700 190/-190 260/350 -500/1900 710/-460 220/-230 530 0 2770
**ENG SVR
DAMAGE/SEP
L, R
(FLAPS 20)
VREF20 8050 200/-200 290/390 -510/1940 730/-480 240/-240 550 0 3320
**ENG SVR
DAMAGE/SEP
L, R
(FLAPS 30)
VREF30 7700 190/-190 260/350 -500/-1900 710/-460 220/-230 530 0 2770
FIRE ENG L, R
(FLAPS 20)
VREF20 8050 200/-200 290/390 -510/1940 730/-480 240/-240 550 0 3320
FIRE ENG L, R
(FLAPS 30)
VREF30 7700 190/-190 260/350 -500/1900 710/-460 220/-230 530 0 2770
FLAP/SLAT
CONTROL
(FLAPS 20)
VREF20 6840 170/-170 250/350 -430/1630 460/-320 190/-200 440 1500 4570
FLAPS DRIVE
(UP < FLAPS ≤ 1)
VREF30+40 8010 180/-180 300/410 -440/1690 450/-330 230/-230 400 1910 6090
FLAPS DRIVE
(1 < FLAPS ≤ 5)
VREF30+40 8410 200/-200 320/430 -460/1750 500/-360 240/-250 430 1950 5980
FLAPS DRIVE
(5 < FLAPS < 20)
VREF30+20 7600 180/-180 280/380 -450/1690 490/-350 210/-220 450 1740 5380
FLAPS DRIVE
(FLAPS ≥ 20)
VREF20 6840 170/-170 250/350 -430/1630 460/-320 190/-200 440 1500 4570
FLAPS PRIMARY
FAIL
(FLAPS 20)
VREF20 7190 180/-170 260/360 -440/1670 480/-340 200/-200 480 1600 4970
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