FIELD: aeronautical engineering; design of seaplanes. SUBSTANCE: seaplane has a fuselage, power plant, tail unit and hydro-ski secured on strut articulated to fuselage nose; seaplane is of canard-aeroplane configuration. Lower portion of fuselage is oval; seaplane is provided with low-set wing; three hydrofoils are mounted on lower portion of fuselage through shock absorbers; incidence of hydrofoils may be changed. Hydrofoils are provided with three-point supports and strut of fore hydro-ski is flexible. EFFECT: enhanced reliability. 3 cl, 2 dwg
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