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Aerospatiale AS332 Super Puma

Lighter-Than-Air Craft and Rotorcraft

The Aerospatiale AS332 Super Puma, later sold as the Eurocopter AS332 and now the Airbus Helicopters H215, is a four-bladed, twin-engined, medium utility helicopter developed in France during the 1970s from the earlier SA 330 Puma. Aerospatiale redesigned the fuselage for greater damage tolerance and crashworthiness, used composite materials more widely in the rotor, streamlined the nose and fitted a pair of more powerful Turbomeca Makila turboshaft engines, which gave it a higher cruise speed, more range and lower fuel consumption than its predecessor. It was planned from the start in a short and a stretched fuselage length. The first full prototype flew on 13 September 1978 and the first civil example was delivered in 1981, after which it became the company principal utility helicopter. It has served armies and air forces, carried crews and passengers to offshore oil rigs and fought fires, and its military version is known as the AS532 Cougar.

Facts
Year
1978 1
Manufacturer or Builder
Aerospatiale, later Eurocopter and Airbus Helicopters 1
Propulsion
Turboshaft 1
Engine Class
Turboshaft 1
Status
In Production 1
Mass (kg)
9150 1
Engine
Two Turbomeca Makila turboshaft engines 1
Connections

Of Make

Source Eurocopter AS332 Super Puma (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Eurocopter AS332 Super Puma (Wikipedia)Lead
Quote, Lead
developed and initially produced by French aerospace company Aérospatiale

Originated In

Also in Geography Atlas: where this subject originated.

Source Eurocopter AS332 Super Puma (Wikipedia)Lead
Quote, Lead
developed and initially produced by French aerospace company Aérospatiale
Sources
1. Eurocopter AS332 Super Puma (Wikipedia)
  • Lead, manufacturer or builder
    developed and initially produced by French aerospace company Aérospatiale
  • Development, Origins, year
    The first prototype of the full Super Puma made its first flight on 13 September 1978
  • Lead, engine
    A pair of more powerful Turbomeca Makila turboshaft engines was used
  • Specifications, mass
    Max takeoff weight: 9,150 kg (20,172 lb)
  • Infobox: produced, status
    1978-present
  • Lead, propulsion
    A pair of more powerful Turbomeca Makila turboshaft engines was used
  • Of Make: Airbus, Lead [of-make]
    It has been subsequently manufactured by the successor companies Eurocopter and Airbus Helicopters.
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