Eurocopter AS332 Super Puma

AS332 Super Puma H215(M)
HAF AS332C1 Super Puma of 384SAR Sq.
Role	Medium utility helicopter
National origin	France
Manufacturer	Aérospatiale Eurocopter Airbus Helicopters
First flight	13 September 1978
Status	Active
Primary users	Armée de l'air CHC Helicopter Bond Offshore Helicopters Spanish Air Force
Produced	1978–present
Unit cost	US$15.5 million, €12.5 million (2006)
Developed from	Aérospatiale SA 330 Puma
Variants	Eurocopter AS532 Cougar
Developed into	Eurocopter EC225 Super Puma Eurocopter EC725

The Eurocopter AS332 Super Puma (now Airbus Helicopters H215) is a four-bladed, twin-engine, medium-size utility helicopter developed and marketed by Aérospatiale and Eurocopter (now Airbus Helicopters). It is an enlarged and re-engined version of the original Aérospatiale SA 330 Puma. First flying in 1978, the Super Puma succeeded the SA 330 Puma as the main production model of the type in 1980; since 1990, Super Pumas in military service have been marketed under the AS532 Cougar designation. In civilian service, a next generation successor to the AS 332 was introduced in 2004, the further-enlarged Eurocopter EC225 Super Puma.

In 1974, Aérospatiale commenced development of a new medium transport helicopter based on its SA 330 Puma. The project was publicly announced at the 1975 Paris Air Show. While the new design maintained a similar generator layout to the preceding AS 330, it was powered by two of the new and more powerful Turbomeca Makila turboshaft engines, which drove a four-bladed main rotor which made use of composite materials. A great level of attention was paid to making the new model withstand damage better; a more robust fuselage structure was adopted along with a new crashworthy undercarriage, the rotor blades are also able to withstand a level of battle damage, as are the other key mechanical systems across the rotorcraft.

External distinguishing features from the SA 330 include a ventral fin underneath the tail boom and a more streamlined nose. From the onset, the new rotorcraft was planned to be available with two fuselage lengths; these were a short fuselage version that offered a similar capacity to the SA 330 while providing superior performance under "hot and high" conditions, and a stretched version which allowed for more internal cargo or passengers to be carried in circumstances where aircraft weight was less critical.