Boeing 787-8 - Page 281

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.12.17
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
FLIGHT
CONTROL
MODE
(FLAPS 20)
VREF20 7310 180/-180 270/380 -450/1690 500/-350 250/-210 500 1680 5330
FLIGHT
CONTROLS
(FLAPS 20)
VREF30+20 7960 190/-190 300/410 -460/1740 530/-380 230/-230 490 1950 6190
**FUEL LEAK
(FLAPS 20)
VREF20 8050 200/-200 290/390 -510/1940 730/-480 240/-240 550 0 3320
**FUEL LEAK
(FLAPS 30)
VREF30 7700 190/-190 260/350 -500/1900 710/-460 220/-230 530 0 2770
FUEL QTY LOW
(FLAPS 20)
VREF20 6840 170/-170 250/350 -430/1630 460/-320 190/-200 440 1500 4570
HYD PRESS
SYS C
(FLAPS 20)
VREF20 7190 180/-170 260/360 -440/1670 480/-340 200/-200 480 1600 4970
HYD PRESS
SYS L
(FLAPS 25)
VREF25 8310 200/-200 290/380 -540/2060 830/-520 230/-230 560 0 2970
HYD PRESS
SYS L
(FLAPS 30)
VREF30 8090 190/-190 270/370 -540/2040 820/-520 230/-230 550 0 2630
HYD PRESS
SYS L+C
(FLAPS 20)
VREF30+20 10090 230/-230 360/480 -600/2250 980/-620 290/-290 640 0 4200
HYD PRESS
SYS L+R
(FLAPS 20)
VREF30+20 13810 260/-270 400/530 -860/3170 2480/-1290 380/-350 860 0 0
HYD PRESS
SYS R
(FLAPS 25)
VREF25 8450 200/-200 290/390 -550/2090 860/-540 240/-240 580 0 3130
HYD PRESS
SYS R
(FLAPS 30)
VREF30 8210 190/-200 280/370 -540/2060 840/-530 230/-230 570 0 2750
HYD PRESS
SYS R+C
(FLAPS 20)
VREF30+20 10380 240/-240 370/500 -620/2290 1030/-660 290/-300 680 0 4600
NAV AIR
DATA SYS
(FLAPS 20)
VREF20 7020 170/-170 250/350 -430/1650 460/-320 190/-200 460 1490 4540
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