First flight 1989. Strutted highwing one-seater from aluminum alloy tubes with fabric covered wings and empenage and pusher Rotax 447 engine. Maximal cruise speed 120 km/hod, stall speed 45km/hod, needed airstrip 75m.

Out of production.

First flight 1993. Strutted highwing with aluminum alloy airframe and composite side-by-side canopy with pusher Rotax 462 - 912ULS engine. Maximal cruise speed 140-160 km/hod.

Production : Interplane sro , Zbraslavice - Czech republic

First flight 2004. Allmetal 2-seat strutted higwing with Rotax 912 engine and three wheel undercarriage. Composite cockpit shell with forward opened large doors. Cruise speed 200-220 km/hod, VNE 275.

Production: GRYF Aircraft, spol s r.o. Hluk was stopped in 2006 and moved to company Flyitalia srl, Dovera - Italy -actually in liquidation.

Two-seat light sport aircraft, designed to be ideal for cross-country flying – with easy access and extremely wide outlook, enabling feeling wings are not divided part of pilot-aircraft complex. Designed according to Czech and Germany UL and US Light Sport Aircraft requirements.:

Still in development.

High-performance composite tandem-seat light sport low-wing, designed to be ideal for really fast cross-country flights - and - flying for fun . COMPlex of exclusive performances with comfortable cockpit and uncompromising styling enables feeling You are truly a Shark on the Sky.

Produced by Shark.aero s.r.o...

Gryf MD-line is the group of aircraft projets with the same technology - family of all-metal aircraft prepared originally with Marián Mečiar, after good experiences with original Raven technology, coming from Mr. Pottier. First of all we prepared MD1, MD2 and MD3 studies (low-wing, tandem and high-wing) to find new investor. After MD3 was chosen and developed for Flyitalia s.r.l., we continued with next studies enlarging good experiences we received with MD3 ... Together with Marián, we created as a first needed aircraft definition (weights, areas, requirements, load envelopes) and aerodynamically-technological structure of wing - with strength structure and flaps geometry, coming from our former works in bigger aircraft industry. Max. permissible speed VNE 275 km/hr covered all our needs, so stayed the same for all members of family - to be able to use subassemblies for all types.