Build for battery swap.
Needs more info on the % of consumed energy contributing to forward flight fuel vs electric, and MTOPS limits for safe landing.
Does any of the fuel burn contribute thrust directly or is it all post turbine and the fan is the predominant thrust? (Not that it matters)
Fuel consumption in flight reduces landing weight. Battery weighs the same landing and take off. Harder landing costs.
What about an imputed hybrid ? Reduced fuel burn not no fuel burn?
