The prototype of this strut braced parasol monoplane flew for the first time in March 1966. Plans are available.

TYPE: Single-seat sporting homebuilt.

AIRFRAME: All-wood structure, plywood and fabric covered. Wing section NACA 2412. Non-retractable tailwheel landing gear.

POWER PLANT (prototype): One 134 kW (180 hp) Textron Lycoming O-360. Fuel capacity 75 litres (20 US gallons; 16.7 Imp gallons). Other engines available optionally include those listed under Jungster I description, plus 119 kW (160 hp) Textron Lycoming O-320 and 134 kW (180 hp) Textron Lycoming O-360.

DIMENSIONS, EXTERNAL:

• Wing span: 6.81 m (22 ft 4 in)
• Length overall (tail up): 5.16 m (16 ft 11 in)
• Height to top of wings (tail up): 2.06 m (6 ft 9 in)
• Propeller diameter: 1.68 m (5 ft 6 in)