[1][2] The aircraft is derived from the Egon Scheibe Uli 1 and was re-designed to comply with the German 120 kg (265 lb) class ultralight rules.

It features a cable-braced high-wing, a single-seat open cockpit without a windshield, fixed conventional landing gear and a single engine in pusher configuration.

The standard engine available is the 30 hp (22 kW) Briggs & Stratton industrial four-stroke powerplant with a V-belt reduction drive, powering a two bladed wooden propeller.

The design incorporates a ballistic parachute whole-aircraft rescue system that includes an ignition cut-off upon firing.

[1][2][3] Data from Bayerl, Tacke and Weller[1][2][3]General characteristics Performance