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AS350 Ecureuil

AS350 Ecureuil

Civil Helicopters
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Basic Information
Name
AS350 Ecureuil
Designation
AS350 Ecureuil
Alternate Designation
AS 350B2 Ecureuil, AS 350B3 Ecureuil, AS 350D AStar (USA version), Z-11 (Chinese-built version)
Equipment Type
Civil Helicopters
Manufacturer
Airbus Helicopters
Date of Introduction
1978
Description

The single-engine AS350 is a lightweight utility helicopter that first flew on June 27, 1974 and the first delivery happened in April 1978. The AS 350B2 Ecureuil commercial helicopter powered by a single engine Arriel 1D1 was introduced in the early 1990s. It assumed civilian-oriented tasks such as utility helicopter, fire fighting, police mission, or medical evacuation. In 1997, Eurocopter introduced the AS 350B3 Ecureuil powered by a single Turbomeca Arriel 2B turboshaft engine along with its military counterpart AS 550C3 Fennec. The new helicopter can conduct the same missions of its predecessor as well as training suing three crashworthy seats. The Arriel 2B engine was equipped with FADEC (Full Authority Digital Electronic Control) and is more powerful than Arriel 1D1 engine which allows to increase the takeoff weight. This model performs better than early generations in hot climate and mountainous terrain/high altitudes. In late November 2005 Eurocopter delivered the 3,000th single-engine Ecureuil/Fennec helicopter family to the South African Police which received an AS 350 B3 aircraft. Eurocopter stated that up to 432 AS 350 B3 helicopters were in service when the 3,000 single-engine helicopter mark was achieved.

Air & Air Defense Specifications
Crew 1
Max Speed 288.0 km/h
Range 467.0 km
Service Ceiling 7000 m
Overview (Deagel)
Group Civil Helicopters
Status Active
Also Known As AS 350B2 Ecureuil, AS 350B3 Ecureuil, AS 350D AStar (USA version), Z-11 (Chinese-built version)
Origin France
Contractor Airbus Helicopters
Initial Operational Capability (IOC) April 1978
First Flight June 27, 1974
Total Production 2,992
Unitary Cost EUR €2.3 million
Specifications (Deagel)
Crew 1
Main Rotor Blades 3
Number of Engines 1
Passengers 6
Tail Rotor Blades 2
Dimensions — Height 3.2 meter
Dimensions — Length 10.9 meter
Dimensions — Main Rotor Diameter 10.7 meter
Dimensions — Width 1.9 meter
Mass — Empty Weight 1,232 kilogram
Mass — Max Takeoff Weight 2,800 kilogram
Performance — Ceiling 7,000 meter
Performance — Max Range 467 kilometer
Power — Max Power at TakeOff 728 shp
Speed — Cruise Speed 238 kph
Speed — Top Speed at High Altitude 288 kph
Time — Flight Endurance 3.3 hour
Gear (Deagel)
Item 1 Turboshaft Engines: Arriel 1D1 (1)
Item 2 Turboshaft Engines: Arriel 2B (1)
Item 3 Turboshaft Engines: LTS101 (1)
Variants
Variant 1 AS350 Ecureuil
Variant 2 AS355 Ecureuil
Variant 3 AS550 Fennec
Variant 4 AS555 Fennec
Variant 5 AS555 SN Fennec
Variant 6 EC130
Variant 7 AS355 NP Ecureuil
Variant 8 H125
Variant 9 H130
Variant 10 H125M
Details
Country of Origin France
Category Rotary Wing Aircraft
Air > Rotary Wing Aircraft
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
10.9 m
Width
1.9 m
Height
3.2 m
Weight
2800 kg
Operators (23)
Russia
China
United States
France
United Kingdom
India
Brazil
South Africa
Spain
Andorra
Angola
Argentina
Australia
Botswana
Canada
Chile
Ecuador
Greece
Iraq
Namibia
Norway
Peru
Vietnam
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