It incorporates a 20% larger tail which gives it a wider center of gravity range, while also enhancing pitch and yaw stability.
[1] The aircraft features a cantilever low-wing, a four-seat enclosed cabin, fixed tricycle landing gear with wheel pants and a single engine in tractor configuration.
The standard engine used is the 300 hp (224 kW) Lycoming IO-540 four stroke, air-cooled, six cylinder powerplant.
With full fuel of 92 U.S. gallons (350 L; 77 imp gal) the payload for pilot, passengers and baggage is 808 lb (367 kg).
[1] In December 2013 three examples were registered in the United States with the Federal Aviation Administration.