Abstract: An aircraft comprising at least one propulsion assembly comprising: at least one electric motor, a transmission system, at least one coupling module comprising a freewheel inserted between inner and outer shafts coupled by first and second coupling mechanisms to the output and input shafts of the electric motor and of the transmission system, at least one of the first and second coupling mechanisms comprising an angle gearset, at least one hollow intermediate element in which the output shaft of the electric motor, the input shaft of the transmission system and the inner and outer tubes of the coupling module are at least partially positioned.

Abstract: An aircraft comprising at least one engine mounting system which connects a propulsion unit and a wing and which comprises a primary structure, engine mounts connecting the primary structure and the propulsion unit, as well as at least first, second and third wing mounts connecting the primary structure and the wing structure, the first and second wing mounts being offset height-wise with respect to one another, the third wing mount being offset in the longitudinal direction toward the rear with respect to the first and second wing mounts.