~~In 1974, Aérospatiale commenced development of a new medium transport helicopter based on its SA 330 Puma, announcing the project at the 1975 Paris Air Show. While the new design was of similar layout to the AS 330, it was powered by two of the new and more powerful Turbomeca Makila turboshaft engines driving a four-bladed composite main rotor, and was designed to withstand damage better, with a more robust fuselage structure, a new crashworthy undercarriage and the ability to withstand battle damage to the rotor blades and other key mechanical systems. It was fitted with a ventral fin under the tail, a more streamlined nose compared with the SA 330, while from the start was planned to be available with two fuselage lengths, with a short fuselage version offering similar capacity to the SA 330, which gives better performance in "hot and high" conditions and a stretched version allowing more passengers to be carried when weight is less critical.

A pre-production prototype, the SA 331, modified from a SA 330 airframe with Makila engines and a new gearbox, flew on 5 September 1977. The first prototype of the full Super Puma made its maiden flight on 13 September 1978, being followed by a further five prototypes. Flight testing revealed that, in comparison with the SA 330 Puma, the AS 330 Super Puma had a higher cruise speed and range, in part due to the Makila engine having a greater power output and a 17% reduction in fuel consumption per mile; the Super Puma also demonstrated far superior flight stabilisation tendencies and was less reliant upon automated corrective systems.[6] Development of the military and civil variants was carried out in parallel, including the certification process. The first civil model was delivered in 1981.

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