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  UL-JIH Colibri
The Jaroslav Sedláček UL-jih Colibri was an easy built aircraft, with two side-by-side seats, braced wing, powered by a Rotax 503 UL/DCDI in pusher configuration.
With sprung landing gear with a nose wheel, the fuselage is aluminium and steel tubes, wings aluminum tubes, PU ribs, aluminum structure ailerons, and steel support structure with thin wall steel tubes. Wing fuel tanks were optional.
Engine: Rotax 503 UL/DCDI
Span: 9,44 m
Length: 5,5 m
Wing area: 12 sq.m
Weight: 195 kg
Speed range: 62 - 140 km/h

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