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Not What You Meant?  There are 22 definitions for Puma.

Aérospatiale Puma

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SA 330 Puma
Westland Puma HC1 of the RAF
Type Utility helicopter
Manufacturers Sud Aviation (later Aérospatiale)
Westland Aircraft
Maiden flight 1965-04-15
Introduced 1968
Primary users Royal Air Force
Various
Produced 1968-1987
Number built 697
Variants Eurocopter Super Puma
Atlas Oryx
IAR 330

The Aérospatiale Puma is a medium-sized twin-engined transport/utility helicopter originally manufactured by Aérospatiale of France. It is also known under the designation SA 330.

Contents

Development

The SA 330 Puma was originally developed by Sud Aviation to meet a requirement of the French Army for a medium-sized all-weather helicopter. The helicopter also had to be capable of operating by day and night as well as in a wide variety of climates. In 1967, the Puma was also selected by the Royal Air Force (RAF) and given the designation Puma HC Mk.1. As a result of this decision, the SA 330 was included in a joint production agreement between Aerospatiale and Westland Helicopters of the UK. The first of two Puma prototypes flew on 15 April 1965. Six pre-production models were also built, the last of which flew on 30 July 1968. The first production SA 330 Puma flew in September 1968. Two years later, in 1970, Sud Aviation merged with Nord Aviation and SÉREB to form Aérospatiale, and the helicopter has been associated with that name ever since, though it still retained the "SA" (for "Sud Aviation") model designator. On 25 April 1978 the SA 330J Puma achieved the distinction of becaming the first helicopter outside the (then) Soviet Union to be certificated for all-weather operations, including icy conditions. Production of the SA 330 Puma by Aérospatiale ceased in 1987, by which time a total of 697 had been sold. The Puma was then replaced by an upgraded and improved version, the AS 332 Eurocopter Super Puma.

Variants

Portuguese Air Force Puma in support of a Space Shuttle Recovery Exercise at Lajes Field, Azores
Portuguese Air Force Puma in support of a Space Shuttle Recovery Exercise at Lajes Field, Azores

Aérospatiale versions

  • SA 330 A: Prototypes, originally called "Alouette IV".
  • SA 330 B: Initial production version for the French Army Aviation.
  • SA 330 "Orchidee": SA 330 modified to carry an "Orchidee" surveillance system for the French Army.
  • SA 330 C: Initial export production version.
  • SA 330 E: Version produced by Westland Helicopters for the RAF under the designation HC Mk 1.
  • SA 330 F: Initial civilian export production version with Turbomeca Turmo IIIC4 turboshaft engines.
  • SA 330 G: Upgraded civilian version with Turbomeca Turmo IVC engines and composite main rotor blades.
  • SA 330 H: Upgraded French Army and export version with Turbomeca IVC engines and composite main rotor blades. Designated SA 330B by the French Air Force.
  • SA 330 J: Upgraded civil transport version.
  • SA 330 L: Upgraded version for so-called "hot and high" conditions.
  • SA 330 S: Export version for the Portuguese Air Force.
  • SA 330 Z: Prototype with "fenestron" tail rotor.

Versions by other manufacturers

Atlas Aircraft Corporation Oryx
This is a remanufactured and upgraded SA 330 Puma built for the South African Air Force.
IPTN NAS 330 J
This is a version that was assembled by IPTN of Indonesia under the local designation NAS 330 J and the Aerospatiale designation of SA 330 J. Eleven units were produced.
ICA IAR 330
This is a licence-built version of the SA 330 Puma manufactured by ICA of Romania. Designated as the SA 330 L by Aerospatiale.
Westland Puma HC Mk.1
This is the SA 330 E version assembled by Westland Helicopters for the RAF.

Operators

Military operators

Aérospatiale Puma of the 801 Squadron of Spanish Air Force
Aérospatiale Puma of the 801 Squadron of Spanish Air Force

Civil operators

The Puma is also operated by several civilian operators.

Specifications (SA 330 Puma)

General characteristics

  • Crew: 3
  • Capacity: 16 passengers
  • Length: 18.15 m (59 ft 6 in)
  • Rotor diameter: 15.0 m (49 ft 3 in)
  • Height: 5.14 m (16 ft 10 in)
  • Disc area: 176.71 m² (1,905 ft²)
  • Empty weight: 3,770 kg (8,310 lb)
  • Max takeoff weight: 7,400 kg (16,300 lb)
  • Powerplant:Turboméca Turmo IVC turboshafts, 1,175 kW (1,575 hp) each

Performance

Armament

For an explanation of the units and abbreviations in this list, please see .

References

External links

Related content

Related development

Comparable aircraft

Related lists

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Aérospatiale Puma from Wíkipedia. ©2006 by Wíkipedia. Licensed under the GNU Free Documentation License. View a list of authors or edit this article.

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