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FLAPS DRIVE
(FLAPS ≥ 20) VREF20 1650 40/-40 50 -90/360 75/-60 25/-25 120 245 680
FLAPS PRIMARY
FAIL VREF20 1795 45/-45 55 -100/380 80/-65 25/-25 145 285 815
FLAP/SLAT
CONTROL VREF20 1630 35/-35 50 -90/355 70/-55 20/-25 120 240 650
FLIGHT
CONTROL MODE VREF20 1855 45/-45 60/ -100/385 90/-65 25/-25 155 315 920
HYD PRESS SYS C VREF20 1795 45/-45 55 -100/380 80/-65 25/-25 145 285 815
HYD PRESS
SYS L+C VREF30+20 2390 50/-50 80 -130/495 160/-115 35/-35 200 - 715
HYD PRESS
SYS L+R VREF30+20 2945 50/-45 90 -170/635 335/-200 50/-50 255 - -
HYD PRESS
SYS R+C VREF30+20 2440 55/-50 80 -135/500 175/-120 35/-40 215 - 760
HYD PRESS SYS L
(FLAPS 25) VREF25 1895 45/-40 60 -115/435 125/-90 25/-30 160 - 450
HYD PRESS SYS L
(FLAPS 30) VREF30 1805 40/-40 55 -110/430 120/-85 25/-25 160 - 400
HYD PRESS SYS R
(FLAPS 25) VREF25 1885 45/-40 60 -115/435 125/-85 25/-30 155 - 440
HYD PRESS SYS R
(FLAPS 30) VREF30 1765 40/-35 55 -110/425 115/-80 25/-25 150 - 370
PITCH UP
AUTHORITY
(FLAPS 5)
VREF30+40 1970 40/-40 60 -100/380 75/-60 25/-30 115 310 845
PITCH UP
AUTHORITY
(FLAPS 20)
VREF30+20 1710 35/-35 50 -95/360 70/-55 25/-25 115 245 665
PRI FLIGHT
COMPUTERS VREF20 1855 45/-45 60 -100/385 90/-65 25/-25 155 315 920
SLATS DRIVE VREF30+30 1905 40/-40 60 -100/380 80/-65 25/-25 125 300 825
STABILIZER VREF30+20 1770 40/-40 55 -100/370 75/-60 25/-25 120 270 750
Actual (unfactored) distances are shown.
Includes distances from 50 ft above threshold (305 m air distance).
Assumes maximum manual braking and maximum available reverse thrust.
December 10, 2007
777 Operations Manual
Performance Inflight
Advisory Information
777-200/GE90-76B
JAA/JAROPS
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D632W001-TBC PI.11.7
ADVISORY INFORMATION
Advisory Information Non-Normal Configuration Landing Distance
Poor Reported Braking Action
LANDING DISTANCE AND ADJUSTMENT (M)
REF
DIST
WT
ADJ
ALT
ADJ
WIND
ADJ PER
10 KTS
SLOPE
ADJ
PER 1%
TEMP
ADJ
PER 10°C
VREF
ADJ
REVERSE
THRUST
ADJ
EICAS
MESSAGE VREF
180000
KG
LDG
WT
PER
5000 KG
ABV/BLW
180000 KG
PER
1000 FT
ABV
S.L.
HEAD/
TAIL
WIND
DOWN/
UP
HILL
ABV/
BLW
ISA
PER
10 KTS
ABV
VREF
ONE
REV
NO
REV
ANTISKID
(FLAPS 25) VREF25 2640 75/-70 100 -220/1055 870/-230 35/-45 145 2135 5000
ANTISKID
(FLAPS 30) VREF30 2525 75/-65 95 -215/1040 845/-225 35/-45 145 2000 5000
ENG SHUTDOWN
L, R (FLAPS 20) VREF20 2415 65/-65 80 -160/620 255/-150 35/-40 170 965
ENG SHUTDOWN
L, R (FLAPS 30) VREF30 2125 55/-55 65 -145/605 225/-135 35/-35 155 705
FLAPS DRIVE
(FLAPS ≤ 5) VREF30+40 2535 60/-60 90 -145/595 185/-120 35/-40 145 770 2875
FLAPS DRIVE
(5 < FLAPS < 20) VREF30+20 2275 55/-55 75 -140/570 175/-110 35/-35 145 645 2290
FLAPS DRIVE
(FLAPS ≥ 20) VREF20 2090 55/-55 70 -135/560 170/-105 30/-35 140 550 1895
FLAPS PRIMARY
FAIL VREF20 2245 60/-60 75 -145/580 185/-120 35/-35 160 620 2245
FLAP/SLAT
CONTROL VREF20 2055 55/-55 70 -135/555 170/-105 30/-30 135 525 1800
FLIGHT
CONTROL MODE VREF20 2320 65/-65 80 -145/595 200/-125 35/-35 175 690 2565
HYD PRESS SYS C VREF20 2245 60/-60 75 -145/580 185/-120 35/-35 160 620 2245
HYD PRESS
SYS L+C VREF30+20 3285 75/-75 120 -215/865 490/-250 50/-55 230 - 2120
HYD PRESS
SYS L+R VREF30+20 5020 75/-35 175 -370/15852685/660 90/-95 325 - -
HYD PRESS
SYS R+C VREF30+20 3330 75/-75 125 -215/870 545/-260 50/-55 245 - 2215
HYD PRESS SYS L
(FLAPS 25) VREF25 2630 65/-60 95 -185/785 425/-200 40/-45 185 - 1380
HYD PRESS SYS L
(FLAPS 30) VREF30 2510 60/-55 90 -185/770 420/-195 40/-45 190 - 1250
HYD PRESS SYS R
(FLAPS 25) VREF25 2595 65/-55 90 -185/775 415/-190 40/-45 180 - 1330
HYD PRESS SYS R
(FLAPS 30) VREF30 2420 55/-55 80 -175/755 395/-185 35/-40 175 - 1130
PITCH UP
AUTHORITY
(FLAPS 5)
VREF30+40 2485 55/-55 85 -145/580 175/-115 35/-40 130 660 2260
PITCH UP
AUTHORITY
(FLAPS 20)
VREF30+20 2155 55/-55 75 -135/560 170/-105 30/-35 130 540 1810
PRI FLIGHT
COMPUTERS VREF20 2320 65/-65 80 -145/595 200/-125 35/-35 175 690 2565
SLATS DRIVE VREF30+30 2375 55/-55 80 -145/585 185/-120 35/-35 140 625 2135
STABILIZER VREF30+20 2225 55/-55 75 -140/575 175/-115 35/-35 140 585 2005
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波音777快速检查单 Quick Reference Handbook QRH(79)
