Table 3
Comparison between the ATR42-600 and the test configuration aircraft in case of no-hybridization.
| ATR42-600 | Test config. | |
|---|---|---|
| OEW/MTOM | 62.9% | 61.91% |
| Fuel mass/MTOM | 12.58% | 12.17% |
| MTOM/S (kg/m2) | 341.3 | 341.3 |
| AR | 11 | 11 |
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