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Aérospatiale Alouette III

From Wikipedia, the free encyclopedia

SA 319 Alouette III
An Alouette III of the 22S wing of the French Navy on the landing pad of Lanvéoc base
Type Light utility helicopter
Manufacturer Sud Aviation
Aérospatiale
Maiden flight 1959-02-28
Retired 2004
Status Active duty in some nations
Primary users French Armed Forces
Indian Air Force
Produced 1961-1985
Number built 2,000+
Developed from Aérospatiale Alouette II
Variants Aérospatiale Gazelle

The Aérospatiale Alouette III (Skylark) is a single-engine, light utility helicopter developed by Sud Aviation and later manufactured by Aérospatiale of France. The Alouette III is the successor to the Alouette II, being larger and having more seating. Originally powered by a Turbomeca Artouste IIIB turboshaft engine, the Alouette III is recognised for its mountain rescue capabilities and adaptability.

Contents

[edit] Development

Close-up of the turbine of an Alouette III
Close-up of the turbine of an Alouette III

The first version of the Alouette III, the SE-3160 prototype, first flew on 28 February 1959. Production of the SA-316A (SE-3160) began in 1961 and remained in production until 1968, when it was replaced by the SA-316B.

[edit] Operational History

The Alouette III entered in service with the French Armed forces in 1960.

Served in Indo-Pakistani War of 1971 when 2 planes of the PAF were lost in the war,[1] and the Portuguese Colonial War, during 60's and 70's with large utilization in Angola, Mozambique and Guinea, where it proved its qualities.

French Navy Alouette III on the frigate La Motte-Picquet
French Navy Alouette III on the frigate La Motte-Picquet

The SA-316B and the SA-319B both remained in series production up to the early 1980s, when the main production line in France was closed down. However, HAL of India continues to licence-build Alouette IIIs as the Chetak. Versions of the Alouette III were also either licence-built or assembled by IAR in Romania (as the IAR 316), F+W Emmen in Switzerland and by Fokker and Lichtwerk in the Netherlands.

Production numbers are as follows:

  • France: 1453
  • India: 300+ (Still in production.)
  • Romania: 230
  • Switzerland: 60

June 2004, the Alouette III was retired from the French Air Force after 32 years of successful service. It will be replaced by the Eurocopter EC 155 Twin Squirrel. In the same year, the Swiss Armed Forces announced the retirement of the Alouette III, from the front line by 2006, and entirely by 2010. Venezuelan Air forces retired the Alouette III in the late 90's.

[edit] Variants

  • The SA-316A was the first production version.
  • The SA-316B is powered by a 425 kW (570 shp) Turboméca Artouste IIIB turboshaft engine, with strengthened main and tail rotor for greater performance. The SA-316B was built under licence in India as the HAL Chetak, and again under licence in Romania as the IAR 316.
  • The SA-319B was a direct development of the SA-316B, it was powered with a 649 kW (870 shp) Turboméca Astazou XIV turboshaft engine, but it was derated to 447 kW (660 hp).
  • The SA-316C was powered by a Turbomeca Artouste IIID turboshaft engine. The SA-316C was only built in small numbers.
  • G-Car and K-Car : Helicopter gunship versions for the Rhodesian Air Force. The G-Car was armed with two side-mounted Browning machine guns. The K-Car was armed with one 20mm Mauser cannon, fitted inside the cabin, firing from the port side of the helicopter.
  • IAR-317 Skyfox: A Romanian helicopter gunship project based on the IAR 316. Only three prototypes were ever built.[verification needed]
  • Atlas XH-1 Alpha: A Two-seat attack helicopter project. It was used in the development of the Denel AH-2 Rooivalk‎.

When used as an aerial ambulance, the Alouette III can accommodate a pilot, two medical attendants and two stretcher patients.

[edit] Operators

Austrian Alouette III over Alps
Austrian Alouette III over Alps
Dutch SA-316B Alouette III
Dutch SA-316B Alouette III
Royal Netherlands Air Force SA-316B Alouette III in Search and Rescue (SAR) markings
Royal Netherlands Air Force SA-316B Alouette III in Search and Rescue (SAR) markings
Irish Air Corps SA-316B Alouette III, 212 from 3 Operations Wing at RNAS Yeovilton in July 2006
Irish Air Corps SA-316B Alouette III, 212 from 3 Operations Wing at RNAS Yeovilton in July 2006
Portugal Alouette III in Africa
Portugal Alouette III in Africa
Aérospatiale SA-316 Alouette III of the Swiss Air Force
Aérospatiale SA-316 Alouette III of the Swiss Air Force

[edit] Specifications (SA-316B)

General characteristics

  • Crew: 2
  • Capacity: 5 passengers
  • Length: 10.03 m (32 ft 11 in)
  • Rotor diameter: 11.02 m (36.2 ft)
  • Height: 3.09 m (10.14 ft)
  • Disc area: m² (ft²)
  • Empty weight: 1,108 kg (2,442 lb)
  • Max takeoff weight: 2,200 kg (4,850 lb)
  • Powerplant:Turboméca Artouste IIIB turboshaft, 425 kW (570 shp)

Performance

[edit] References

    [edit] External links

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