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H225

H225

Civil Helicopters
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Basic Information
Name
H225
Designation
H225
Alternate Designation
EC 225 Super Puma, EC225
Equipment Type
Civil Helicopters
Manufacturer
Airbus Helicopters
Date of Introduction
2004
Description

The Airbus Helicopters H225, formerly the Eurocopter EC 225, is the latest development of Cougar/Super Puma family of helicopters for heavy transport in the 11-ton class segment. The H225 features a five-blade main rotor of the 'Spheriflex' type that provides optimum lift performance and reliability. The main rotor blades are equipped with a very advanced airfoil shape providing the aircraft with an extremely low vibration level. It is powered by two Makila 2A turbo shaft engines with dual-channel full authority digital engine control (FADEC) system and anti-icing system for operation in extremely cold climate. The helicopter gearbox has been reinforced incorporating advanced materials and new structural solutions such as rigid frames. Eurocopter is marketing the EC225 twin-engine helicopter for a wide range of missions for the commercial market. It can assume offshore transport roles carrying up to 24 passengers and one cabin attendant in addition to the crew. It the Very Important Person (VIP) transport version the EC225 can accommodate from 8 to 10 passengers. Search and rescue missions can be assigned to this aircraft as well. However, offshore and VIP transport remain the primary roles. Overall performance stays highly reliable and the helicopter handle characteristics benefit from a full digital glass-cockpit and a digital 4-axis autopilot. The first EC225 prototype performed the maiden flight in November 2000. It shares lots of characteristics and design solutions with Eurcopter's EC 725, which is intended for the military market. To date, 22 EC225/EC725 helicopters have been ordered and the total amount of Cougar/Super Pumas produced stands at 682. The first EC225 civil helicopter was delivered to the government of Algeria after rolling off the assembly line at Marignane, France, on December 22, 2004.

Air & Air Defense Specifications
Crew 2
Max Speed 324.0 km/h
Range 984.0 km
Service Ceiling 5900 m
Overview (Deagel)
Group Civil Helicopters
Status Active
Also Known As EC 225 Super Puma, EC225
Origin France
Contractor Airbus Helicopters
Initial Operational Capability (IOC) December 22, 2004
First Flight November 2000
Total Production 272
Unitary Cost EUR €23 million
Specifications (Deagel)
Crew 2
Main Rotor Blades 5
Number of Engines 2
Passengers 24
Tail Rotor Blades 4
Dimensions — Height 4.6 meter
Dimensions — Length 16.8 meter
Dimensions — Main Rotor Diameter 16.2 meter
Dimensions — Width 3 meter
Mass — Empty Weight 5,256 kilogram
Mass — Max Takeoff Weight 11,200 kilogram
Mass — Payload 5,744 kilogram
Performance — Ceiling 5,900 meter
Performance — Max Range 984 kilometer
Performance — Min Range 839 kilometer
Power — Max Power at TakeOff 3,740 shp
Speed — Cruise Speed 275 kph
Speed — Top Speed at High Altitude 324 kph
Time — Flight Endurance 5 hour
Gear (Deagel)
Item 1 Turboshaft Engines: Makila 2A (2)
Variants
Variant 1 SA 330 Puma
Variant 2 AS 532 Cougar
Variant 3 AS 332 Super Puma
Variant 4 AS 532SC Cougar
Variant 5 H225
Variant 6 H225M
Variant 7 EC225e
Variant 8 H215
Details
Country of Origin France
Category Rotary Wing Aircraft
Air > Rotary Wing Aircraft
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
16.8 m
Width
3 m
Height
4.6 m
Weight
11200 kg
Operators (20)
China
United States
France
Germany
United Kingdom
Japan
South Korea
Ukraine
Brazil
Spain
Algeria
Argentina
Canada
Denmark
Ireland
Kazakhstan
Malaysia
Morocco
Norway
Vietnam
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