[2][3] The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules, US light-sport aircraft rules and UK BCAR Section "S".

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

[2][3][4] The aircraft is made with carbon fibre sandwich construction.

[2][3][6] The design has been developed into a three to four seat aircraft, the Aerospool WT10 Advantic.

Data from Bayerl, Tacke and Aerospool[2][3][6]General characteristics Performance