1. Makholet, comprising a hull with a cockpit, an engine, a chassis, a tail of horizontal and vertical tail, a wing consisting of central and external segments interconnected by hinges, attached to the hull by means of suspension units, an aircraft flight control system, characterized in that the wing is a single unit and is attached to the frame of the body by means of two hinged attachment points that separate the center part and two cantilever parts in the wing, with the hinge axes parallel to the chord to It was found, and spaced symmetrically with respect to the longitudinal plane of symmetry of the body, to a distance that allows the wing, under the action of alternating vertical forces from the engine, to elastically bend in the vertical plane with an amplitude different for the central part of the wing and the wing ends of not more than 15%, and to compensate for changes in the length of the central when it bends part of the wing, an additional compensating element, for example, an additional hinge, is installed on one of the two hinged attachment points. 2. Makholet according to claim 1, characterized in that the wing surface can be twisted (skewed), i.e. the angle of attack of the chord of the profile of the middle of the wing and the ends of the wing may differ depending on the angle of attack of the incoming air flow, due to the fact that the wing has a skeleton in which ribs can swivel around a round spar, and the skeleton shell has sufficient elasticity and elasticity for this .3. Makholet according to claim 2, characterized in that the wing is divided into two or more wings, identical in design to the original wing with the same wingspan, having a chord that is several times smaller than the chord
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