| 747 fuel table |
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Warning: For PC simulator use only ! Do not use for real world flight planning.
This simplified table shows the connection betwen weight and optimum
altitude, as well as the corresponding fuel flow values per engine, true
air speed (TAS) and the rpms of the low pressure compressor stage
(N1). International standard atmosphere (ISA) conditions are assumed, as
well as Mach 0.86 cruising speed and all three air conditioning packs are on.
Fuel flow figures have been rounded.
| Weight (1000kg) | Optim. altitude | Fuel flow (kg/h)/eng | TAS (kts) | N1 (%) |
| 390 | FL290 | 3400 | 509 | 94.1 |
| 360 | FL310 | 3100 | 505 | 93.6 |
| 330 | FL330 | 2800 | 500 | 92.5 |
| 300 | FL350 | 2500 | 496 | 92.0 |
| 270 | FL370 | 2300 | 493 | 91.6 |
| 240 | FL390 | 2100 | 493 | 91.2 |
| 220 | FL410 | 1900 | 493 | 91.5 |
| 200 | FL430 | 1800 | 493 | 91.7 |
N1 is higher at higher than ISA temperatures - fuel flow and TAS as well ...
Source of data: Manual for Precision Simulator 1.3 by Aerowinx
and Hardy Heinlin, original table compiled by Marc Brodbeck.
I've rounded the fuel figures and the full table in the PS1.3 manual is a lot
more comprehensive.
Last updated
13 February 2007
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