[2][3] The aircraft was originally designed in Spain by Vol Mediterrani to comply with the Fédération Aéronautique Internationale microlight rules and production was later moved to Sweden.

It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit, tricycle landing gear or conventional landing gear and a single engine in tractor configuration.

[2][3] The aircraft is made from high density PVC foam and epoxy resin composites.

The landing gear is made from 7175-T6 aluminum alloy and employs a freely-castering nosewheel and main wheels brakes for steering.

[2][3][4] Data from Bayerl and Aerocomp AB[2][4]General characteristics Performance