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D632W001-TBC PI.20.3
General Flight With Unreliable Airspeed / Turbulent Air Penetration
Altitude and/or vertical speed indications may also be unreliable.
Final Approach (1500 FT)
Gear Down, Set Thrust for 3° Glideslope
FLAP POSITION
(VREF + INCREMENT)
WEIGHT (1000 KG)
160 200 240 280
FLAPS 20
(VREF20 + 10)
PITCH ATT 1.0 1.5 1.5 1.5
EPR 1.010 1.010 1.020 1.020
(Alt Mode %N1) (34.7) (40.2) (45.0) (49.3)
KIAS 142 157 172 185
FLAPS 25
(VREF25 + 10)
PITCH ATT 0.0 0.5 0.5 0.5
EPR 1.030 1.040 1.050 1.070
(Alt Mode %N1) (44.1) (50.7) (56.2) (60.6)
KIAS 138 153 166 179
FLAPS 30
(VREF30 + 10)
PITCH ATT -0.5 0.0 0.0 0.0
EPR 1.050 1.070 1.090 1.110
(Alt Mode %N1) (50.5) (56.9) (62.4) (66.8)
KIAS 131 146 159 171
December 10, 2007
777 Flight Crew Operations Manual
Performance Inflight
General
777-200ER/TRENT892
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
PI.20.4 D632W001-TBC
Max Climb EPR
Based on engine bleed for packs on and anti-ice off
EPR Adjustments for Engine Bleed
TAT
(°C)
PRESSURE ALTITUDE (1000 FT)/SPEED (IAS OR MACH)
0 5 10 15 20 25 30 35 40 43
310 310 310 310 310 310 310 0.84 0.84 0.84
60 1.132 1.122 1.127 1.146 1.166 1.159 1.152 1.174 1.178 1.170
50 1.168 1.161 1.147 1.146 1.166 1.159 1.152 1.174 1.178 1.170
40 1.209 1.205 1.191 1.184 1.173 1.159 1.152 1.174 1.178 1.170
30 1.217 1.253 1.243 1.237 1.228 1.196 1.157 1.174 1.178 1.170
20 1.217 1.253 1.284 1.298 1.292 1.259 1.228 1.191 1.178 1.170
10 1.217 1.253 1.284 1.329 1.364 1.337 1.307 1.273 1.260 1.257
0 1.217 1.253 1.284 1.329 1.374 1.399 1.402 1.367 1.351 1.348
-10 1.217 1.253 1.284 1.329 1.374 1.399 1.434 1.482 1.468 1.465
-15 &
BELOW 1.217 1.253 1.284 1.329 1.374 1.399 1.434 1.506 1.521 1.518
BLEED CONFIGURATION PRESSURE ALTITUDE (1000 FT)
0 5 10 15 20 25 30 35 40 43
ENGINE ONLY -0.008 -0.010 -0.015 -0.015 -0.006 -0.005 -0.003 -0.003 -0.004 -0.005
ENGINE & WING* -0.010 -0.012 -0.018 -0.020 -0.012 -0.012 -0.011 -0.014 -0.017 -0.019
ENGINE & WING** -0.012 -0.014 -0.021 -0.025 -0.018 -0.019 -0.020 -0.024 -0.029 -0.033
*Wing anti-ice on, packs on.
**Wing anti-ice on, single bleed source and both packs off.
December 10, 2007
777 Flight Crew Operations Manual
Performance Inflight
General
777-200ER/TRENT892
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D632W001-TBC PI.20.5
VREF
WEIGHT
(1000 KG)
FLAPS
30 25 20
300 166 174 180
290 164 171 177
280 161 168 174
270 157 165 171
260 154 162 168
250 151 159 164
240 148 156 161
230 145 152 158
220 142 149 154
210 139 145 150
200 135 142 147
190 132 138 143
180 128 134 139
170 124 131 135
160 121 127 131
150 117 123 127
140 113 118 123
December 10, 2007
777 Flight Crew Operations Manual
Performance Inflight
General
777-200ER/TRENT892
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
PI.20.6 D632W001-TBC
Intentionally
Blank
December 10, 2007
777 Flight Crew Operations Manual
Performance Inflight Chapter PI
Advisory Information Section 21
777-200ER/TRENT892
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D632W001-TBC PI.21.1
PI.21 Performance Inflight-AdAviDsoVry IISnfOorRmaYti oInNFORMATION
Advisory Information Normal Configuration Landing Distance
Flaps 30
Dry Runway
Good Reported Braking Action
Medium Reported Braking Action
Poor Reported Braking Action
LANDING DISTANCE AND ADJUSTMENTS (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
BRAKING
CONFIGURATION
180000 KG
LANDING
WT
PER
5000 KG
ABOVE/
BELOW
180000 KG
PER
1000 FT
ABOVE
S.L.
HEAD
WIND
TAIL
WIND
DN
HILL
UP
HILL
ABV
ISA
BLW
ISA
PER
10 KTS
ABOVE
VREF30
ONE
REV
NO
REV
MAX MANUAL 830 +25/-15 15 -35 125 10 -10 15 -15 65 10 25
MAX AUTO 1100 +20/-15 25 -50 175 0 0 25 -25 115 0 0
AUTOBRAKE 4 1350 +30/-20 35 -65 245 0 -5 35 -35 145 0 0
AUTOBRAKE 3 1620 +35/-30 45 -85 305 10 -10 45 -45 175 0 5
　
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