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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