Universal aeroplane with electric driveo with passenger cabin (10,11,2)o with aerodynamic carrying surfaces (3,6,7)o with supporting surface components adjustable in the supporting surfaces (4.1,,5.1)o with movable propeller retractors arranged in the supporting surface components (4,5)o with an electronic control of the angle position of the rotary motors,o with stowage compartments in the lower part of the passenger compartment for the housing of traction batteries (10,11,2),o where the supporting surfaces and the variable supporting surface components are located in the upper part of the passenger compartment;o where the propeller blade diameters (5) are so measured that they do not touch the floor of the runway when the tiltors are positioned in a bold position,o and the vertical tilt rotors at the vertical start are positioned in at least 2,5 m above the runway floor of the take-off area,marked by it,that the electrical organs (8,22) are arranged for the propeller drive (5) and for the adjustment (9) of the tiltrotators in the floating surface components (4).
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