[1][2] The P-Mentor was designed to comply with the European Union Aviation Safety Agency EASA CS-23 regulations for certified light aircraft.

[1][3] The design features a cantilever low-wing, two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed tricycle landing gear with wheel pants and a single engine in tractor configuration, driving a two-bladed variable pitch propeller.

The standard engine employed is the 75 kW (101 hp) Rotax 912iSc four-stroke certified powerplant.

[1][4] The design uses a new tapered planform wing, employing a laminar flow airfoil, which meets the EASA CS-23 requirements for low speed handling and stall characteristics without a ballistic parachute, although a parachute is approved and available as a factory option.

[1][3] Data from AVweb, Flying, Manufacturer[1][3][4]General characteristics Performance Avionics