Boeing 787-8 - Page 282

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.12.18 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
NAV AIRSPEED
DATA
(FLAPS 20)
VREF20 7020 170/-170 250/350 -430/1650 460/-320 190/-200 460 1490 4540
OVERHEAT
ENG L, R
(FLAPS 20)
VREF20 8050 200/-200 290/390 -510/1940 730/-480 240/-240 550 0 3320
OVERHEAT
ENG L, R
(FLAPS 30)
VREF30 7700 190/-190 260/350 -500/1900 710/-460 220/-230 530 0 2770
PITCH UP
AUTHORITY
(FLAPS ≥ 20)
VREF30+20 7540 180/-180 280/380 -440/1690 480/-340 210/-220 440 1670 5080
PITCH UP
AUTHORITY
(FLAPS ≤ 15)
VREF30+40 8320 190/-190 310/420 -460/1730 490/-350 240/-250 420 1890 5750
PRI FLIGHT
COMPUTERS
(FLAPS 20)
VREF20 7310 180/-180 270/380 -450/1690 500/-350 200/-210 500 1680 5330
ROLL LEFT
AUTHORITY
(FLAPS 20)
VREF30+20 7530 180/-180 280/380 -440/1680 480/-340 210/-220 440 1670 5060
ROLL RIGHT
AUTHORITY
(FLAPS 20)
VREF30+20 7530 180/-180 280/380 -440/1680 480/-340 210/-220 440 1670 5060
SLATS DRIVE
(FLAPS 20)
VREF30+30 8060 190/-190 300/410 -460/1730 500/-360 230/-240 440 1830 5570
SPOILER PAIRS
(FLAPS 25)
VREF25+5 7140 180/-170 260/360 -440/1660 480/-340 200/-210 460 1580 4810
SPOILER PAIRS
(FLAPS 30)
VREF30+5 7020 170/-170 250/340 -440/1660 490/-340 200/-200 460 1460 4290
STABILIZER
(FLAPS 20)
VREF30+20 7540 180/-180 280/380 -440/1690 480/-340 210/-220 440 1670 5080
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