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1700 75.0 5:16 70.7 5:03 67.3 4:52 67.0 4:33
1800 79.2 5:35 74.8 5:22 71.2 5:09 70.8 4:50
December 10, 2007
777 Flight Crew Operations Manual
Performance Inflight
Engine Inoperative
777-300/PW4090
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
D632W001-TBC PI.32.11
ENGINE INOP
MAX CONTINUOUS THRUST
Long Range Cruise Diversion Fuel and Time
Fuel Required Adjustment (1000 LB)
REFERENCE FUEL REQUIRED
(1000 LB)
WEIGHT AT CHECK POINT (1000 LB)
300 350 400 450 500 550 600 650
5 -0.7 -0.6 -0.4 -0.2 0.0 0.5 0.8 1.2
10 -1.7 -1.4 -1.0 -0.5 0.0 1.3 2.3 3.1
15 -2.8 -2.2 -1.5 -0.8 0.0 2.1 3.7 5.1
20 -3.8 -3.0 -2.1 -1.1 0.0 2.8 5.2 7.0
25 -4.9 -3.8 -2.6 -1.3 0.0 3.6 6.6 9.0
30 -5.9 -4.6 -3.1 -1.6 0.0 4.3 8.0 10.9
35 -6.9 -5.3 -3.6 -1.9 0.0 5.1 9.3 12.9
40 -7.9 -6.1 -4.2 -2.1 0.0 5.8 10.7 14.8
45 -9.0 -6.9 -4.7 -2.4 0.0 6.5 12.0 16.7
50 -10.0 -7.6 -5.2 -2.7 0.0 7.1 13.4 18.7
55 -11.0 -8.4 -5.7 -2.9 0.0 7.8 14.7 20.6
60 -12.0 -9.1 -6.2 -3.2 0.0 8.5 16.0 22.5
65 -13.0 -9.9 -6.6 -3.4 0.0 9.1 17.2 24.4
70 -14.0 -10.6 -7.1 -3.7 0.0 9.7 18.5 26.4
75 -15.0 -11.3 -7.6 -3.9 0.0 10.3 19.7 28.3
80 -16.0 -12.0 -8.0 -4.2 0.0 10.9 20.9 30.2
APU fuel included
December 10, 2007
777 Flight Crew Operations Manual
Performance Inflight
Engine Inoperative
777-300/PW4090
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
PI.32.12 D632W001-TBC
ENGINE INOP
MAX CONTINUOUS THRUST
Holding
Flaps Up
WEIGHT
(1000 LB)
PRESSURE ALTITUDE (FT)
1500 5000 10000 15000 20000 25000
660
EPR 1.150 1.186 1.256 1.382
KIAS 259 260 261 277
FF/ENG 17910 17770 18030 19530
620
EPR 1.136 1.168 1.231 1.333
KIAS 251 252 253 262
FF/ENG 16750 16610 16750 17560
580
EPR 1.122 1.152 1.208 1.294
KIAS 243 244 245 248
FF/ENG 15690 15450 15560 15900
540
EPR 1.109 1.136 1.186 1.261 1.400
KIAS 234 235 236 237 252
FF/ENG 14630 14330 14410 14510 16030
500
EPR 1.097 1.120 1.165 1.229 1.334
KIAS 226 226 227 228 235
FF/ENG 13600 13270 13270 13280 14050
460
EPR 1.085 1.105 1.144 1.199 1.283 1.470
KIAS 220 220 220 220 220 238
FF/ENG 12610 12350 12200 12140 12400 14260
420
EPR 1.073 1.090 1.124 1.171 1.241 1.371
KIAS 213 213 213 213 213 220
FF/ENG 11610 11430 11230 11090 11140 12000
380
EPR 1.061 1.076 1.105 1.145 1.201 1.303
KIAS 206 206 206 206 206 206
FF/ENG 10630 10450 10290 10050 10030 10340
340
EPR 1.051 1.063 1.087 1.121 1.164 1.252
KIAS 199 199 199 199 199 199
FF/ENG 9660 9480 9370 9050 9000 9150
December 10, 2007
777 Flight Crew Operations Manual
Performance Inflight Chapter PI
Text Section 33
Copyright © The Boeing Company. See title page for details.
D632W001-TBC PI.33.1
TPext I.33 Performance Inflight-Text
Introduction
This chapter contains information to supplement performance data from the Flight
Management Computer. In addition, sufficient inflight data is provided to
complete a flight with the FMC inoperative. In the event of conflict between data
presented in this chapter and that contained in the Approved Flight Manual, the
Flight Manual shall always take precedence.
Flight with Unreliable Airspeed / Turbulent Air Penetration
Body attitude and average EPR information is provided for use in all phases of
flight in the event of unreliable airspeed/Mach indications resulting from blocking
or freezing of the pitot system. Loss of radome may also cause unreliable
airspeed/Mach indications. Climb, cruise and descent information is based on the
recommended turbulent air penetration speed schedule: 270 knots below 25,000
feet, 280 knots or 0.82 Mach whichever is lower at 25,000 feet and above;
maintain a minimum speed of 15 knots above the minimum maneuvering speed
when below 0.82 Mach. This schedule provides ample protection from stall and
high speed buffet, while also providing protection from exceeding structural
limits.
Pitch attitude is shown in bold type for emphasis since altitude and/or vertical
speed may also be unreliable.
Max Climb EPR
This table shows Max Climb EPR for a 310/.84 climb speed schedule, normal
engine bleed for packs on and anti-ice off. Enter the table with airport pressure
altitude and TAT and read EPR. EPR adjustments are shown for anti-ice
operation.
VREF Speeds
This table contains flaps 30, 25 and 20 reference speeds for a given weight.
Advisory Information
　
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