Boeing 787-8 - Page 278

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.12.14 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
NAV AIRSPEED
DATA
(FLAPS 20)
VREF20 5650 120/-120 180/240 -300/1110 210/-170 140/-150 400 730 1930
OVERHEAT
ENG L, R
(FLAPS 20)
VREF20 6050 140/-140 190/260 -340/1220 300/-240 170/-170 450 0 1340
OVERHEAT
ENG L, R
(FLAPS 30)
VREF30 5780 130/-130 170/230 -330/1200 290/-230 160/-160 440 0 1120
PITCH UP
AUTHORITY
(FLAPS ≥ 20)
VREF30+20 6090 130/-130 200/270 -320/1140 230/-190 160/-170 390 860 2310
PITCH UP
AUTHORITY
(FLAPS ≤ 15)
VREF30+40 6690 140/-140 220/300 -330/1180 240/-200 180/-190 360 970 2590
PRI FLIGHT
COMPUTERS
(FLAPS 20)
VREF20 5890 130/-130 190/260 -320/1140 240/-190 150/-160 440 830 2280
ROLL LEFT
AUTHORITY
(FLAPS 20)
VREF30+20 6060 130/-130 200/260 -310/1140 230/-190 160/-170 380 850 2260
ROLL RIGHT
AUTHORITY
(FLAPS 20)
VREF30+20 6060 130/-130 200/260 -310/1140 230/-190 160/-170 380 850 2260
SLATS DRIVE
(FLAPS 20)
VREF30+30 6540 140/-140 220/290 -330/1180 250/-200 180/-180 390 960 2580
SPOILER PAIRS
(FLAPS 25)
VREF25+5 5710 130/-130 180/250 -310/1120 230/-190 150/-160 400 780 2080
SPOILER PAIRS
(FLAPS 30)
VREF30+5 5590 120/-120 180/240 -300/1110 230/-190 150/-150 400 720 1850
STABILIZER
(FLAPS 20)
VREF30+20 6090 130/-130 200/270 -320/1140 230/-190 160/-170 390 860 2310
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