The SIPA S.251 Antilope was a low-wing monoplane, seating four or five and powered by a single turboprop engine, developed in France in the early 1960s. It set a number of class records but was not put into production.
The Antilope was one of the first turboprop powered light aircraft. Apart from its engine, it was a conventional all-metal low-wing machine. The cantilever wing was built around two spars and was a semi-monocoque structure, carrying unslotted ailerons and electrically powered, single slotFowler flaps. The fuselage was also of semi-monocoque construction. The tail unit included a variable incidence tailplane and a rudder with a trim tab. It had an electrically actuated tricycle undercarriage, the main wheels retracting inwards into the wings. The cabin had seats for four or five, two at the front and a bench seat behind. In a proposed air ambulance configuration, the Antilope would have carried two stretchers and a medic. Access to the cabin was via a large rear hinged door on the starboard side. The Antilope was powered by a 665 hp Turbomeca Astazou X driving a 3-bladed propeller, on a long spinner, well ahead of the surrounding air intake. It first flew on 7 November 1962 and gained certification in April 1964. That autumn, P. Bonneau set six international Class C1c records with it, achieving for example a speed of 432.9 km/h over a 3 km course and reaching an altitude of 10,420 m. Early in 1965 it flew with a four-bladed propeller and improved on one of its own records. A three-blade propellor was re-installed and the aircraft was exhibited at the 1965 Paris Air Show wearing registration F-BJSS. By mid 1966 development had been completed without a decision to commence production. The production version would have been known as the SIPA S.2510 Antilope but none were built; the prototype carried the designation S.251 on its fin. The sole Antilope is undergoing restoration in a private museum, owned by the Association Antilope, at Montpelier-Mediterranee Airport, in southern France.
