The Tecnam P2010 is a larger, four seat relative of the Tecnam P2008 two seat braced high wing light aircraft. Both types have metal wings and tailplane on a composite fuselage with integrated fin.[2]
The wing leading edge is straight except for some pinching at the root and the wing has constant chord on the inner section. Outboard, the trailing edge is tapered; the straight wing tips are slightly upturned. Ailerons span the outboard panels and the inner sections carry flaps. There is a single lift strut on each side, attached to the lower fuselage. The P2010 has a low set all-moving constant-chord tailplane with an anti-balance tab. The fin is swept and the rudder moves above the tailplane.[2]
The P2010 is powered by a 135 kW (180 hp) Lycoming IO-360-M1A horizontally opposed four cylinder piston engine, with a 215 hp Lycoming IO-390 option available.[3] The cabin seats the pilot and three passengers in two side-by-side rows, accessed by three doors. Its fixed tricycle undercarriage has spring cantilever main legs and a castoring nosewheel. All wheels have speed fairings.

Real Photo:

Credit to @ MAPA's for his original Tecnam P2010 / P2008