The P2006T is the lightest twin-engined certified aircraft available, with liquid-cooled Rotax engines that can run on 92 octane unleaded automotive gasoline as well as 100LL. The P2006T is a twin-engined four-seat cantilever high-wing monoplane with a retractable tricycle landing gear. Its stabilator is attached to the fuselage, mostly aft of the vertical fin (the stabilator is a single unit with a cutout in its leading edge where it mounts to the tailcone). The nosewheel of the tricycle landing gear retracts into the nose cone; the trailing-link main units retract into stubs which extend from the lower fuselage. The fuselage section is a slightly rounded rectangle, higher than it is wide. A door on each side of the fuselage provides access to the seating area; in addition an escape hatch is provided above the two forward seats, to be used if fuselage deformation in a crash prevents those doors from being operable. The link between the flight controls and the flight surfaces is by pushrod, rather than the usual cables. Variants P2006T Standard civilian version. P2006T MRI Maritime patrol variant.[9] P2006T MMA Multi-Mission variant modified with mission equipment by Airborne Technologies. T2006A Italian military designation for aircraft delivered in the Training role to 70° Stormo of the Italian Air Force on 5 July 2016 for multi-engine pilot training. "Fly it like a Cessna 172": Flying magazine pilot report.
