Boeing 787-8 - Page 274

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.12.10 D615Z003-TBC
ADVISORY INFORMATION
Advisory Information
Non-Normal Configuration Landing Distance
Good 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 4330 80/-80 110/160 -200/710 90/-80 100/-100 320 270 640
OVERHEAT
ENG L, R
(FLAPS 20)
VREF20 4330 80/-90 120/160 -210/730 110/-100 110/-110 340 0 430
OVERHEAT
ENG L, R
(FLAPS 30)
VREF30 4140 80/-80 110/140 -200/720 110/-90 100/-100 330 0 360
PITCH UP
AUTHORITY
(FLAPS ≥ 20)
VREF30+20 4650 80/-90 130/170 -210/730 100/-90 110/-120 320 350 830
PITCH UP
AUTHORITY
(FLAPS ≤ 15)
VREF30+40 5060 90/-90 140/190 -210/750 100/-90 130/-130 290 380 920
PRI FLIGHT
COMPUTERS
(FLAPS 20)
VREF20 4500 90/-90 120/170 -210/730 100/-90 110/-110 350 310 760
ROLL LEFT
AUTHORITY
(FLAPS 20)
VREF30+20 4600 80/-90 130/170 -210/720 100/-90 110/-120 310 330 790
ROLL RIGHT
AUTHORITY
(FLAPS 20)
VREF30+20 4600 80/-90 130/170 -210/720 100/-90 110/-120 310 330 790
SLATS DRIVE
(FLAPS 20)
VREF30+30 5000 90/-90 140/190 -220/760 110/-100 130/-130 320 390 950
SPOILER PAIRS
(FLAPS 25)
VREF25+5 4310 80/-80 120/160 -200/710 100/-90 100/-110 320 300 700
SPOILER PAIRS
(FLAPS 30)
VREF30+5 4210 80/-80 110/150 -200/700 100/-90 100/-100 320 270 620
STABILIZER
(FLAPS 20)
VREF30+20 4650 80/-90 130/170 -210/730 100/-90 110/-120 320 350 830
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