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The Pilots Desk
Helicoptersutility helicopter family by Sud Aviation

Aérospatiale Alouette III

Aérospatiale Alouette III

The Aérospatiale Alouette III (French pronunciation: [alwɛt], Lark; company designations SA 316 and SA 319) is a single-engine, light utility helicopter developed by French aircraft company Sud Aviation. Introduced in the early 1960s, more than 2,000 units were built during its production run that extended for six decades. The Alouette III was developed as an enlarged derivative of the earlier successful Alouette II. It shared many design elements with its predecessor while offering an extra pair of seats and other refinements. It quickly became a commercial success and was operated by a range of civil and military customers. Further variants were also developed; amongst these was a high-altitude derivative, designated as the SA 315B Lama, which entered operational service during July 1971. The Alouette III was principally manufactured by Aérospatiale, after its take over of Sud Aviation in 1970. The type was also built by various licensed manufacturers such as Hindustan Aeronautics Limited in India (as HAL Chetak), by Industria Aeronautică Română in Romania (as IAR 316), and by Eidgenössisches Flugzeugwerk in Switzerland (as F+W Emmen). Similar to the Alouette II, in military service, it was used to perform missions such as aerial observation and photography, air-sea rescue, communication liaison, transport, and training. It could also be armed with anti-tank missiles, anti-ship torpedoes, and a fixed cannon. In a civilian capacity, the helicopter was commonly used for casualty evacuation (often fitted with a pair of external stretcher panniers), crop spraying, personnel transportation, and for carrying other external loads. By the 2010s, many operators were in the process of drawing down their fleets and replacing them with more modern types; the French Armed Forces intended to replace their Alouette IIIs with the newly developed Airbus Helicopters H160 and the Indian Armed Forces with the HAL Dhruvs.

Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.

Manufacturer
Sud-Aviation
Category
Helicopters
Country of origin
France
First flight
1959-02-28
Length
10.03 m

Specifications

Cruise speed
100 kt
Max speed
110 kt
Range
290 nm
Service ceiling
10,500 ft
Rate of climb
850 ft/min
Max takeoff weight
4,850 lb
Empty weight
2,520 lb
Powerplant
Turbomeca Artouste IIIB
Engines
1
Seats
7
Length
32.9 ft
Height
9.8 ft
Number built
2,000

Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).

Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.