It features a single main rotor, a two-seats in side-by-side configuration enclosed cockpit with optional doors, skid-type landing gear and a four-cylinder, horizontally opposed, air-cooled, two-stroke, dual-ignition 95 hp (71 kW) Hirth F-30 engine.
Its 23.00 ft (7.0 m) diameter two-bladed rotor employs an ATI 012 (VR-7 mod) airfoil at the blade root, transitioning to an ATI 008 (VR-7 mod) airfoil at the tip.
The tail rotor is ring-mounted and the horizontal tailplane mounts end-fins for directional stability.
With full fuel of 16 U.S. gallons (61 L; 13 imp gal) the payload for crew and baggage is 494 lb (224 kg).
[1] The manufacturer estimated the construction time from the supplied kit as 60 hours.