the fuselage executed in the form of a wing of small lengthening, центроплан, consoles I covered, the power plant, tail plumage, the chassis with management mechanisms, it is supplied with the poles located on each side центроплана and along its axis of symmetry, rigidly fixed on its bottom surface and supplied not movably fixed at the bottom end faces of poles underwater wings, at this chassis it is executed wheel, and mechanisms of management of the chassis are placed in poles.
In process of speed increase from 0 to the speed of effective work of underwater wings the amphibian comes to a surface of the water, overcoming power factors of interaction with water.
By the time of an exit to gliding the air passable between a surface of the water and the bottom surface центроплана 1, withheld from an overflowing from sides by poles 2, thanks to narrowing of the channel slows down, being transformed to pressure surpassing atmospheric, i.e. Rn> Ro, and creating effect of the dynamic airbag
With a further growth of speed power parameters of the airbag increase, tearing off the amphibian surfaces of wings 6 and 7 from a water surface, providing that in contactless movement with water a fast gain of speed and transfer to keeping and to ascent.
Further flight of the amphibian up to passing of a point of alignment when landing doesn't differ the dynamics from the plane with being cleaned wheel chassis.