ARMSNET
Military Equipment Database
Initializing 0%

SA 319B Alouette III French Light Utility Helicopter

SA 319B Alouette III

Utility Helicopter
Spotted an error? Sign in to suggest an edit.
Basic Information
Name
SA 319B Alouette III French Light Utility Helicopter
Designation
SA 319B Alouette III
Alternate Designation
SA 319B Alouette III
Equipment Type
Utility Helicopter
Manufacturer
Date of Introduction
1960
Description

SA 319B Alouette III Astazou Similar to SA316B except for its 870-shp Turbomeca Astazou XIV engine (derated to 600 shp), from which the name is derived. Some were outfitted for naval operations with the anticorrosion finish, folding main rotor, the ability to carry air-to-surface missiles, torpedoes, and a magnetic anomaly detector (MAD). The Aérospatiale Alouette III (French pronunciation: ​[alwɛt], Lark; company designations SA 316 and SA 319) is a single-engine, light utility helicopter developed by the French aircraft company Sud-Aviation. During its production life, it proved to be a relatively popular rotorcraft; including multiple licensed manufacturers, in excess of 2,000 units were constructed. The Alouette III was developed as an enlarged derivative of the earlier and highly successful Alouette II. Sharing many elements with its predecessor while offering an extra pair of seats and other refinements, it quickly became a commercial success amongst both 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 in July 1971. The Alouette III was principally manufactured by Aérospatiale; the type was also built under license by Hindustan Aeronautics Limited (HAL) in India as the HAL Chetak, by Industria Aeronautică Română (IAR) in Romania as the IAR 316 and F+W Emmen in Switzerland. Similar to the Alouette II, in military service, it was used to perform missions such as aerial observation, photography, air-sea rescue, liaison, transport, and training; it could also be armed with anti-tank missiles, anti-shipping torpedoes, and a fixed cannon. In a civilian capacity, the Alouette III was commonly used for casualty evacuation (often fitted with a pair of external stretcher panniers), crop-spraying, personnel transportation, and carrying 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 military intend to replace their Alouette IIIs with the newly developed Airbus Helicopters H160.

Air & Air Defense Specifications
Crew 1
Engine Turboshaft (870 hp)
Max Speed 220.0 km/h
Range 480.0 km
Rotor Diameter 11.00 m
Variants
SA 316A the first production version. Original designation SE 3160.
SA 316B 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 license in India as the HAL Chetak, and again under licence in Romania as the IAR 316.
SA 319B The SA 319B was a direct development of the SA 316B, it was powered with a 649 kW (870 shp) Turbomeca Astazou XIV turbo shaft engine, but it was derated to 447 kW (660 hp).
SA 316C 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 .303 or a single 7.62mm MAG machine guns. The K-Car was armed with a 20 mm MG 151 cannon, fitted inside the cabin, firing from the port side of the helicopter.
SA.3164 Alouette-Canon Modified in 1964 as a gunship version armed with a 20mm gun in the nose and external hardpoints for missiles mounted on each side of the fuselage. Only one prototype was built
IAR 317 Airfox A Romanian helicopter gunship project based on the IAR 316. Only three prototypes were ever built.
Atlas XH-1 Alpha South African two-seat attack helicopter project. It was used in the development of the Denel Rooivalk.
K-1 'Chetak', informally- 'Frenchman' 8 HAL Chetaks were bought by the Soviet Union for testing purposes at Kacha airfield, Sevastopol, in 1985, and later 2 of them were used by DOSAAF from Karagoz airfield[
System
Alternative Designation SA 319B Alouette III
Type Light Utility Helicopter
Crew 1 (pilot) ea
Blades, Main Rotor 3 ea
Blades, Tail Rotor 3 ea
Number of Engines 1 ea
Number of Hard Points INA
Dimensions
Length 10.02 m
Height 3.09 m
Rotor Diameter 11.00 m
Disc Area 95.0 m sq
Empty Weight 1,122 kg
Maximum Takeoff Weight 2,200 kg
Automotive
Engine Name 1 x Turbomeca Astazou XIV
Engine Type Turboshaft
Engine Power 870 shaft hp derated to 600 shp
Fuel Capacity 573 liters internal
Maximum Speed 220 km/h
Cruising Speed 197 km/h
Ceiling, Hover IGE 3,100 m
Ceiling, Hover OGE 1,700 m
Maximum Range 480 km
Rate of Climb 885 m/min
Ceiling 3,200 m
Main Gun System
Note 1 x 7.62-mm gun firing to the side; or 1 x 20-mm open turret gun mounting
Missile Weapon Systems
Note 4 x AS11 anti-tank missiles; or 2 x AS12 anti-ship missiles
Rocket Weapon Systems
Note 2 x 68-mm rocket pods
Fire Control and Avionics
Fire Control Radar INA
Navigation Radar INA
Protection
Add on Armor INA
Stealth Properties No
Heat Signature Reduction No
NBC Protection Yes
EW Counter Measures/CCM INA
Counter Measures (Chaff/Flares) INA
Details
Country of Origin France
Category Rotary Wing Aircraft
Air > Rotary Wing Aircraft
Filter Label
S
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
10.02 m
Width
Height
3.09 m
Weight
2200 kg
Operators (37)
France
India
Pakistan
South Africa
Argentina
Austria
Belgium
Burkina Faso
Cameroon
Chad
Congo, Republic of the
Ecuador
Equatorial Guinea
Ethiopia
Ghana
Greece
Guinea
Guinea-Bissau
Lebanon
Malaysia
Malta
Morocco
Myanmar
Namibia
Nepal
Netherlands
Portugal
Romania
Senegal
Suriname
Switzerland
Tanzania
Togo
Tunisia
Venezuela
Zimbabwe
French Guiana
Something went wrong. Please reload the page. Reload