[1][2][3][4] The Puma was designed to comply with the Fédération Aéronautique Internationale microlight rules.

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

[1][2][3][4] The aircraft fuselage is made from welded steel tubing, with an aluminum sheet wing.

[2][3][4] A fixed gear version, to be called the Raptor, was under preliminary development in 2010.

[1][3] Data from Tacke and manufacturer[1][5]General characteristics Performance