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250 FUEALL T(1 0(F0T0 )LB) 31240.020 31250.090 21870.070 21690.050 22410.040 0:54
300 FUEALL T(1 0(F0T0 )LB) 31260.060 31280.060 22800.070 22620.090 22450.020 1:03
350 FUEALL T(1 0(F0T0 )LB) 31290.010 32210.030 22830.080 22660.040 22490.000 1:12
400 FUEALL T(1 0(F0T0 )LB) 32210.050 32240.000 22860.090 22690.090 23420.080 1:21
450 FUEALL T(1 0(F0T0 )LB) 32240.000 32060.090 23800.010 23630.040 23460.070 1:30
500 FUEALL T(1 0(F0T0 )LB) 32260.050 32090.070 23830.020 23660.090 24210.000 1:40
787 Flight Crew Operations Manual
Performance Dispatch
Gear Down
FAA
Category A Brakes
PD.13.8 Boeing Proprietary
GEAR DOWN
Gear DownHolding Planning
Flaps Up
Flaps 1
WEIGHT
(1000 LB)
TOTAL FUEL FLOW (LB/HR)
PRESSURE ALTITUDE (FT)
1500 5000 10000 15000 20000 25000 30000
660 31450 31450 31540 31940
620 29480 29490 29490 29740
580 27600 27570 27530 27680 28290
540 25820 25740 25690 25720 26070
500 24110 23980 23920 23870 24020 24770
460 22460 22280 22180 22100 22150 22570
420 21370 20650 20500 20430 20390 20580
380 19770 19540 18860 18790 18720 18770 19210
340 18180 17960 17270 17160 17370 17060 17300
300 16610 16410 15730 15840 15770 15420 15500
WEIGHT
(1000 LB)
TOTAL FUEL FLOW (LB/HR)
PRESSURE ALTITUDE (FT)
1500 5000 10000 15000 20000
660 30050 30040 30040 30300
620 28190 28170 28130 28280 28920
580 26390 26310 26270 26360 26770
540 24660 24530 24500 24490 24710
500 22950 22790 22720 22680 22790
460 21790 21080 20940 20900 20960
420 20120 19430 19240 19200 19170
380 18450 18250 17580 17490 17730
340 16810 16630 15970 16110 16060
300 15480 15320 15070 14490 14410
These tables include 5% additional fuel for holding in a racetrack pattern.
787 Flight Crew Operations Manual
Performance Dispatch
Gear Down
FAA
Category A Brakes
Boeing Proprietary PD.13.9
GEAR DOWN
ENGINE INOP
MAX CONTINUOUS THRUST
Net Level Off Weight
Anti-ice Adjustments
PRESSURE
ALTITUDE
(1000 FT)
LEVEL OFF WEIGHT (1000 LB)
ISA + 10°C
& BELOW ISA + 15°C ISA + 20°C
18 332.1
17 345.3 328.7
16 359.0 341.9 323.4
15 371.2 353.8 334.9
14 383.8 366.2 346.8
13 396.7 378.8 359.0
12 409.9 391.6 371.6
11 422.7 403.6 383.1
10 435.6 415.9 394.8
9 447.5 427.1 405.4
8 459.2 438.4 416.2
7 471.1 449.9 427.1
6 483.1 461.3 438.1
5 495.2 472.9 449.2
4 505.0 482.3 458.4
3 514.5 491.4 467.4
2 523.7 500.6 476.4
ANTI-ICE
CONFIGURATION
LEVEL OFF WEIGHT ADJUSTMENT (1000 LB)
PRESSURE ALTITUDE (1000 FT)
8 10 12 14 16 18
ENGINE ONLY 15.9 16.5 16.5 15.7 11.9 6.8
ENGINE AND WING 20.1 20.7 21.6 21.4 17.4 11.7
787 Flight Crew Operations Manual
Performance Dispatch
Gear Down
FAA
Category A Brakes
PD.13.10 Boeing Proprietary
Intentionally
Blank
787 Flight Crew Operations Manual
Performance Dispatch Chapter PD
Text Section 14
FAA
Category A Brakes
FAST-Doc PI/PD Template 9/1/99
Boeing Proprietary PD.14.1
PD.14 Performance Dispatch-Text
Text
Introduction
This chapter contains self dispatch performance data intended primarily
for use by flight crews in the event that information cannot be obtained
from the airline dispatch office. The data provided is for a single takeoff
flap at max takeoff thrust. The range of conditions covered is limited to
those normally encountered in airline operation. 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.
Takeoff
The maximum allowable takeoff weight will be the least of the Field,
Climb, Brake Energy, and Obstacle Limit Weights as determined from the
following tables. Tire Limit is not shown as it is not limiting for the range
of conditions shown in this chapter.
Field Limit Weight - Slope and Wind Corrections
These tables provide corrections to the field length available for the effects
of runway slope and wind component along the runway. Enter the Slope
Correction table with the available field length and runway slope to
determine the slope corrected field length. Now enter the Wind Correction
table with slope corrected field length and wind component to determine
the slope and wind corrected field length.
Field and Climb Limit Weight
Tables are presented for selected airport pressure altitudes and show both
Field and Climb Limit Weights. Enter the appropriate table for pressure
　
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