It features a single main rotor, a single-seat open cockpit without a windshield, skid-type landing gear and a twin cylinder, liquid-cooled, in-line two-stroke, carbureted 70 hp (52 kW) Hirth 3503 aircraft engine.
The twin cylinder, liquid-cooled, in-line two-stroke, 64 hp (48 kW) Rotax 582 has also been used.
[1][2][3] The aircraft fuselage is made from welded 4130 steel tubing, with an aluminium tail boom.
The main transmission is of belt and chain type, whileteh tail rotor is driven by a long shaft.
With full fuel of 8 U.S. gallons (30 L; 6.7 imp gal) the payload for pilot and baggage is 302 lb (137 kg).