The aircraft is supplied complete and ready-to-fly-aircraft or as a kit for amateur construction.

It was designed to comply with the European Class 6 microlight helicopter rules, in particular the French Class 6 Microlight Category, at a gross weight of 450 kg (992 lb).

It features a single main rotor and tail rotor, a two-seats-in side-by-side configuration enclosed cockpit with a bubble canopy, skid landing gear and a four-cylinder, liquid and air-cooled, four stroke 100 hp (75 kW) Rotax 912ULS engine, a Dynali-developed fuel-injected 110 hp (82 kW) conversion Rotax 912ULS-1 engine or a 115 hp (86 kW) turbocharged Rotax 914 powerplant.

[1][2] The aircraft's gross weight varies from 450 kg (992 lb) for the microlight category, with heavier weights available depending on installed power in other national categories, such as light-sport aircraft.

[1][2] The aircraft fuselage frame is made from welded stainless steel tubing.