Boeing 787-8 - Page 272

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.12.8 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
ENG OIL
TEMP L, R
(FLAPS 20)
VREF20 4330 80/-90 120/160 -210/730 110/-100 110/-110 340 0 430
ENG OIL
TEMP L, R
(FLAPS 30)
VREF30 4140 80/-80 110/140 -200/720 110/-90 100/-100 330 0 360
ENG SURGE L, R
(FLAPS 20)
VREF20 4330 80/-90 120/160 -210/730 110/-100 110/-110 340 0 430
ENG SURGE L, R
(FLAPS 30)
VREF30 4140 80/-80 110/140 -200/720 110/-90 100/-100 330 0 360
**ENG SVR
DAMAGE/SEP
L, R
(FLAPS 20)
VREF20 4330 80/-90 120/160 -210/730 110/-100 110/-110 340 0 430
**ENG SVR
DAMAGE/SEP
L, R
(FLAPS 30)
VREF30 4140 80/-80 110/140 -200/720 110/-90 100/-100 330 0 360
FIRE ENG L, R
(FLAPS 20)
VREF20 4330 80/-90 120/160 -210/730 110/-100 110/-110 340 0 430
FIRE ENG L, R
(FLAPS 30)
VREF30 4140 80/-80 110/140 -200/720 110/-90 100/-100 330 0 360
FLAP/SLAT
CONTROL
(FLAPS 20)
VREF20 4120 80/-80 110/150 -190/690 90/-80 100/-100 300 270 650
FLAPS DRIVE
(UP < FLAPS ≤ 1)
VREF30+40 4870 80/-90 140/180 -210/730 90/-80 120/-120 270 380 930
FLAPS DRIVE
(1 < FLAPS ≤ 5)
VREF30+40 5090 90/-90 150/190 -220/750 110/-90 130/-130 290 390 940
FLAPS DRIVE
(5 < FLAPS < 20)
VREF30+20 4570 80/-90 130/170 -200/720 100/-90 110/-120 300 330 790
FLAPS DRIVE
(FLAPS ≥ 20)
VREF20 4120 80/-80 110/150 -190/690 90/-80 100/-100 300 270 650
FLAPS PRIMARY
FAIL
(FLAPS 20)
VREF20 4430 80/-90 120/160 -200/720 100/-90 100/-110 340 290 710
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