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 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 and mounts flaps. Standard engines available are the Rotax 912UL, the Rotax 912ULS and the Rotax 914 four-stroke powerplants. The cabin width is . 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. Specifications (Puma) See also Aero-Service Panda References External links Puma 2010s Polish ultralight aircraft Single-engined tractor aircraft