Boeing 787-8 - Page 279

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.12.15
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
ANTI-ICE LEAK
ENG L, R
(FLAPS 20)
VREF20 8340 200/-200 290/400 -540/2060 820/-520 230/-230 560 0 3070
ANTI-ICE LEAK
ENG L, R
(FLAPS 30)
VREF30 7990 190/-190 270/360 -530/2030 800/-510 220/-220 540 0 2530
ANTISKID
(FLAPS 25)
VREF25 8790 250/-240 380/520 -660/2770 1670/-670 260/-270 490 3390 15310
ANTISKID
(FLAPS 30)
VREF30 8700 250/-230 370/510 -660/2760 1670/-680 260/-270 500 3220 14080
BRAKES
(FLAPS 25)
VREF25 8010 220/-210 320/440 -560/2270 950/-510 230/-240 480 2450 8720
BRAKES
(FLAPS 30)
VREF30 7920 210/-200 310/430 -560/2270 960/-520 230/-240 480 2310 7960
ENG FAIL L, R
(FLAPS 20)
VREF20 8050 200/-200 290/390 -510/1940 730/-480 240/-240 550 0 3320
ENG FAIL L, R
(FLAPS 30)
VREF30 7700 190/-190 260/350 -500/1900 710/-460 220/-230 530 0 2770
ENG LIMIT
EXCEED L, R
(FLAPS 20)
VREF20 8050 200/-200 290/390 -510/1940 730/-480 240/-240 550 0 3320
ENG LIMIT
EXCEED L, R
(FLAPS 30)
VREF30 7700 190/-190 260/350 -500/1900 710/-460 220/-230 530 0 2770
ENG OIL
FILTER L, R
(FLAPS 20)
VREF20 8050 200/-200 290/390 -510/1940 730/-480 240/-240 550 0 3320
ENG OIL
FILTER L, R
(FLAPS 30)
VREF30 7700 190/-190 260/350 -500/1900 710/-460 220/-230 530 0 2770
ENG OIL
PRESS L, R
(FLAPS 20)
VREF20 8050 200/-200 290/390 -510/1940 730/-480 240/-240 550 0 3320
ENG OIL
PRESS L, R
(FLAPS 30)
VREF30 7700 190/-190 260/350 -500/1900 710/-460 220/-230 530 0 2770
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