Aero-Service Puma

The Aero-Service Puma is a Polish ultralight aircraft, designed and produced by Aero-Service Jacek Skopiński of Warsaw. The aircraft is supplied complete and ready-to-fly.

Design and development
The Puma was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, retractable tricycle landing gear and a single engine in tractor configuration.

The aircraft fuselage is made from welded steel tubing, with an aluminum sheet wing. Its 9.15 m span wing employs a NACA 4415 airfoil at the wing root, transitioning to a NACA 4412 at the wing tip. The wing has an area of 11.3 m2 and mounts flaps. Standard engines available are the 80 hp Rotax 912UL, the 100 hp Rotax 912ULS and the 115 hp Rotax 914 four-stroke powerplants. The cabin width is 124 cm.

The Puma was designed in 2008, with a prototype under construction in September 2011. No first flight of the design has been confirmed.

A fixed gear version, to be called the Raptor, was under preliminary development in 2010.