Development and design of composite parts for the aircraft EV-55 Outback including assembly into the existing metallic structure of the aircraft.

Project description

Development of a multi-purpose aircraft (category FAR/CS23) for transport of passengers and cargo, taking off and landing on paved and unpaved runways, driven by two turboprop engines PT6A-21 with usable inner space of 12,67 cbm.

Primary structures of the aircraft are manufactured of light metallic alloys (Evektor), most of secondary structures are manufactured of composite materials (LA composite). This project is supported by Ministry of Industry and Commerce, Czech Republic, project identification Nr. FI-IM/039.

The project is financed by contribution of Ministry of Industry and Commerce, Czech Republic.