Aircraft (1) comprising a fuselage (3) and two aerodynamic wings with at leasttwo respective propeller drives (11,12, 13, 14) disposed thereon at a distance from one another in the span widthdirection of the wings, each of said propeller drivescomprising a propeller rotating axle (11a, 12a, 13a, 14a), wherein theaircraft (1) comprises a control device for controlling thepropeller drives (11, 12, 13, 14), wherein in an operating mode of the controldevice for producing propulsion, the propeller drives(11, 12, 13, 14) are actuated in such a way that the outer section of arespective propeller attached to the respective propellerrotating axle is moved downward from above on the side facing the fuselage(3).
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