Definitions
Eurocopter_Ecureuil

Eurocopter Ecureuil

The Eurocopter AS350 Ecureuil ("Squirrel") and AS355 Ecureuil 2 are a family of light helicopters originally manufactured by Aérospatiale (now part of Eurocopter Group). The AS350 (marketed as the AStar in North America) is the single-engined version, while the AS355 (TwinStar) uses two engines. The EC130B is a recent adaptation of the AS350 airframe.

Design and development

Development began in the early 1970's to replace the Alouette II, and the first flight took place on 27 June 1974. A twin-engined version, known as the Ecureuil 2, Twin Squirrel, or in North America as the TwinStar, first flew on 3 October 1979. Despite the introduction of the EC130, production of the Eurocopter AS350 and AS355, and the AS550 and AS555 Fennec military versions remains strong.

Both single and twin-engined versions have been built under licence by Helibras in Brazil.

Operational history

On May 14, 2005 a standard-configured Ecureuil AS350 B3 piloted by Eurocopter test pilot Didier Delsalle touched down on the top of Mt. Everest, at 8,850 meters (29,035 feet) . This record has been confirmed by the Fédération Aéronautique Internationale.

Variants

Single engine

AS350

Prototype.AS350 Firefighter
Fire fighting version.AS350B
Powered by one Turbomeca Arriel 1B engine.AS350 B1
Powered by one Turbomeca Arriel 1D engine.AS350 B2
Higher gross weight version powered by one Turbomeca Arriel 1D1 engine.AS350 B3
High-performance version, is powered by a Turbomeca Arriel 2B engine equipped with a Full Authority Digital Engine Control (FADEC) system. This helicopter is the first ever to land on Mount Everest. Recently introduced AS350 B3/2B1 variant introduces enhanced engine with dual digital FADEC, dual hydraulics and a 2,370 kg (5,225 lb) M.T.O.W.AS350 BA
Powered by a Turbomeca Arriel 1B engine and fitted with wider chord main rotor blades.AS350 BB
AS350 B2 variant selected to meet rotary-wing training needs of UK MoD, through its Defence Helicopter Flying School in 1996. Powered by a derated Turbomeca Arriel 1D1 engine to improve the helicopters' life cycle.;Eurocopter Squirrel HT.1
Designation of AS 350BB in operation with British RAF as a training helicopter.;Eurocopter Squirrel HT.2
Designation of AS 350BB in operation with British Army Air Corps as a training helicopter.AS350 C
Initial variant of Lycoming LTS-101-600A2 powered version developed for the North American market as the AStar. Quickly superseded by AS350D.AS350 D
Powered by one Lycoming LTS-101 engine for the North American market as the AStar. At one stage marketed as AStar 'Mark III.'AS350 L1
Military derivative of AS350 B1, powered by a 510-kW (684-shp) Turbomeca Arriel 1D turboshaft engine. Superseded by AS350 L2.AS350 L2
Military derivative of AS350 B2, powered by a 546-kW (732-shp) Turbomeca Arriel 1D1 turboshaft engine. Designation superseded by AS550 C2.HB350 B Esquilo
Unarmed military version for the Brazilian Air Force. Brazilian designations CH-50 and TH-50. Built under licence by Helibras in Brazil. HB350 B1 Esquilo
Unarmed military version for the Brazilian Navy. Brazilian designation UH-12. Built under licence by Helibras in Brazil.HB350 L1
Armed military version for the Brazilian Army. Brazilian designation HA-1. Built under licence by Helibras in Brazil.

Twin engine

AS355

Prototype of the twin-engined Ecureuil 2 or Twin Squirrel.AS355 E
Initial production version, powered by two Allison 250 turboshaft engines. Known as the Twin Star in the United States and Canada.AS355 F
Improved version, fitted with improved rotor blades and systems.AS355 F1
Powered by the Allison C20F engine. 2,400 kg (5,291 lb) M.T.O.W. AS355 F2
Powered by the Allison C20F engine with uprated engine and transmission for higher M.T.O.W. (2,540 kg or 5,600 lb), and hydraulic accumulator for better tail rotor control.AS355 M
Initial armed version of AS355 F1.AS355 M2
Armed version of AS355 F2. Superseded by AS555 Fennec.AS355 N Ecureuil 2
Version fitted with two Turbomeca Arrius 1A engines and a Full Authority Digital Engine Control (FADEC) system for better M.T.O.W (2,600 kg or 5,732 lb) and better single engine performance. Known as the TwinStar in the United States.AS355 NP Ecureuil 2
Introduced in 2007, this version is fitted with two Turbomeca Arrius 1A1 turboshaft engines and a new AS350 B3-based main gearbox, increasing maximum take-off weight to 2,800 kg (6,173 lb).HB.355F Ecureuil 2
Licence built in Brazil by Helibras.HB.355N Ecureuil 2
Licence built in Brazil by Helibras.

Aftermarket conversions

Soloy Super D
AS350 BA powered by an LTS101-600A-3A engine.Soloy Super D2
AS350 B2 powered by an LTS101-700D-2 engine.Heli-Lynx 350FX1
AS350 BA powered by an LTS101-600A-3A engine.Heli-Lynx 350FX2
AS350 BA or AS350 B2 powered by an LTS101-700D-2 engine.Otech AS350BA+
AS350 BA powered by an LTS101-600A-3A engine .Heli-Lynx 355FX1
Powered by the Allison C20F engine. FAA, TC, and EASA approved.Heli-Lynx 355FX2
Powered by the Allison C20F engine. FAA,TC and EASA approved.Heli-Lynx 355FX2R
Powered by the Allison C20R engine. FAA and TC approved.Starflex AS355F1R
AS355 F1 powered by the Allison C20R engine. FAA, TC and EASA approved.Starflex AS355F2R
AS355 F2 Powered by the Allison C20R engine with optimised tail rotor blades. FAA, TC and EASA approved.

Operators

Military operators

Law Enforcement operators

Civilian operators

  • Heliflite Oy in the arctic Finland
  • Air Greenland
  • 3 AS350 B in service with Hungarian Air Ambulance Service, all of them received general overhaul in 2005-2007.
  • Iranian helicopter service company (IHSC)
  • 1 AS350 B2 is operated by Northflight, also do they have one more on its way.
  • Puerto Rico Electric Power Authority
  • CabAir Helicopters operate a number of Twin Squirrel "VIP Version" helicopters.

Accidents and incidents

Specifications (AS350 B3)

{{aircraft specifications

|plane or copter?= copter |jet or prop?= prop

|ref={Original Ecureuil article}

|crew= 1 |capacity= 6 |length main= 12.94 m |length alt= 42.45 ft |span main= 10.69 m |span alt= 35.07 ft |height main= 3.24 m |height alt= 10.63 ft |area main= |area alt= |airfoil= |empty weight main= 1,241 kg |empty weight alt= 2,736 lbs |loaded weight main= |loaded weight alt= |useful load main= |useful load alt= |max takeoff weight main= 2,250/2,570 kg |max takeoff weight alt= 4,960/5,225 lbs |more general=

|engine (prop)= Turbomeca Arriel 2B or 2B1 |type of prop= turboshaft |number of props= 1 |power main= 632 kW |power alt= 847 shp |power original= |cruise speed main= 259 km/h |cruise speed alt= 140 knots, 161 mph - Fast cruise (127 knots normal cruise speed). |never exceed speed main= 287 km/h |never exceed speed alt= 155 knots, 178 mph |range main= 657 km |range alt= 355 nm, 408 mi |ceiling main= 5,044 m |ceiling alt= 16,550 ft |climb rate main= 10.0 m/s |climb rate alt= 1,959 ft/min |loading main= |loading alt= |thrust/weight= |power/mass main= |power/mass alt= |more performance=

|armament=

|avionics= Vehicle and Engine Multifunction Display (VEMD) with First Limit Indicator (FLI) fitted as standard. }}

See also

References

External links

Search another word or see Eurocopter_Ecureuilon Dictionary | Thesaurus |Spanish
  • Please Login or Sign Up to use the Recent Searches feature