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AS355 NP Ecureuil

AS355 NP Ecureuil

Civil Helicopters
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Basic Information
Name
AS355 NP Ecureuil
Designation
AS355 NP Ecureuil
Alternate Designation
Ecureuil 2, TwinStar (USA version)
Equipment Type
Civil Helicopters
Manufacturer
Airbus Helicopters
Date of Introduction
2007
Description

The AS 355NP high performance multi-mission aircraft is a variant of AS 355N helicopter intended as an entry product in the twin-engined rotary-wing aircraft segment. Eurocopter announced the development of the AS 355NP model in February 2006 with an in service date planned for April 2007. This new model features the ability to take-off at maximum gross weight in various climatic conditions. Performance operating on a single engine and payload are expected to be improved compared with early AS 355 models. Maintenance costs will be lowered while flight safety will be increased on the AS 355NP fitted with two Turbomeca Arrius 1A1 engines. The AS355NP helicopter was awarded EASA certification on February 15, 2007.

Air & Air Defense Specifications
Crew 1
Max Speed 278.3 km/h
Range 428.0 km
Service Ceiling 6096 m
Overview (Deagel)
Group Civil Helicopters
Status Active
Also Known As Ecureuil 2, TwinStar (USA version)
Origin France
Contractor Airbus Helicopters
Initial Operational Capability (IOC) May 2007
Total Production 21
Specifications (Deagel)
Crew 1
Main Rotor Blades 3
Number of Engines 2
Passengers 6
Dimensions — Height 3.0 meter
Dimensions — Length 10.9 meter
Dimensions — Main Rotor Diameter 10.7 meter
Dimensions — Width 1.9 meter
Mass — Empty Weight 1,437 kilogram
Mass — Max Takeoff Weight 2,800 kilogram
Performance — Ceiling 6,096 meter
Performance — Max Range 428 kilometer
Power — Max Power at TakeOff 794 shp
Speed — Cruise Speed 67.8 mps
Speed — Top Speed at High Altitude 77.3 mps
Time — Flight Endurance 2.9 hour
Gear (Deagel)
Item 1 Turboshaft Engines: Arrius 1A1 (2)
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
Height
3 m
Weight
2800 kg
Related Equipment (1)
Operators (6)
Russia
France
Spain
Canada
Malaysia
Vietnam
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