Boeing 787-8 - Page 268

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.12.4 D615Z003-TBC
ADVISORY INFORMATION
Advisory Information
Non-Normal Configuration Landing Distance
Dry Runway
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 3050 80/-50 70/90 -120/420 40/-30 60/-70 230 0 100
ENG OIL
TEMP L, R
(FLAPS 30)
VREF30 2930 80/-50 60/80 -120/410 40/-30 60/-60 220 0 90
ENG SURGE L, R
(FLAPS 20)
VREF20 3050 80/-50 70/90 -120/420 40/-30 60/-70 230 0 100
ENG SURGE L, R
(FLAPS 30)
VREF30 2930 80/-50 60/80 -120/410 40/-30 60/-60 220 0 90
**ENG SVR
DAMAGE/SEP
L, R
(FLAPS 20)
VREF20 3050 80/-50 70/90 -120/420 40/-30 60/-70 230 0 100
**ENG SVR
DAMAGE/SEP
L, R
(FLAPS 30)
VREF30 2930 80/-50 60/80 -120/410 40/-30 60/-60 220 0 90
FIRE ENG L, R
(FLAPS 20)
VREF20 3050 80/-50 70/90 -120/420 40/-30 60/-70 230 0 100
FIRE ENG L, R
(FLAPS 30)
VREF30 2930 80/-50 60/80 -120/410 40/-30 60/-60 220 0 90
FLAP/SLAT
CONTROL
(FLAPS 20)
VREF20 3010 80/-50 70/90 -120/410 30/-30 60/-60 220 70 140
FLAPS DRIVE
(UP < FLAPS ≤ 1)
VREF30+40 3690 130/-60 90/150 -140/480 40/-40 80/-80 240 120 270
FLAPS DRIVE
(1 < FLAPS ≤ 5)
VREF30+40 3680 130/-60 90/150 -130/470 40/-40 80/-90 240 110 230
FLAPS DRIVE
(5 < FLAPS < 20)
VREF30+20 3310 100/-50 70/100 -130/430 40/-30 70/-70 210 80 180
FLAPS DRIVE
(FLAPS ≥ 20)
VREF20 3010 80/-50 70/90 -120/410 30/-30 60/-60 220 70 140
FLAPS PRIMARY
FAIL
(FLAPS 20)
VREF20 3300 80/-50 70/100 -130/440 40/-30 70/-70 250 70 160
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