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H215 Super Puma French Multi-Role Helicopter

H215

Utility Helicopter
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Basic Information
Name
H215 Super Puma French Multi-Role Helicopter
Designation
H215
Alternate Designation
H215
Equipment Type
Utility Helicopter
Manufacturer
Date of Introduction
2015
Description

The Airbus Helicopters H215 is an evolution of the twin-engine AS332 C1e/L1e aircraft intended for business and industrial operators. The H215 is a versatile, economic and robust helicopter that combines advanced avionics and a reliable platform for rugged multi-mission capabilities. It offers long range capabilities, power, speed, a large useful payload and very good lifting performance in hot and high environments. Both EASA and FAA certified, the aircraft is equipped with the latest, most modern technologies meeting the latest safety requirements of the market. This includes a glass cockpit and the renowned 4-axis autopilot used on the H225. The H215 helicopter was launched in November 2015 and the first production aircraft is scheduled to roll off the assembly line in Romania by 2017.

Air & Air Defense Specifications
Crew 2
Engine Turboshaft (1780 hp)
Cruise Speed 251.0 km/h
System
Alternative Designation H215
Type Multi-Role Helicopter
Primary Function The H215 is a 9-ton class twin-engine helicopter in the famous COUGAR / SUPER PUMA family. They combine the rugged experience of the AS532 / AS332 dynamic and basic assemblies with the most advanced avionics of the H225M. They also include full glass cockpit avionics and the latest generation autopilot. These aircraft are reliable, fast helicopters and have outstanding all weather capabilities: a great power reserve and high maneuverability. The powerful MAKILA 1A1 engines give them the ability to fly almost any mission, no matter the temperature and altitude. They ensure maximum operational safety, even in the most difficult situations (discretion, low vulnerability, crash survivability and icing conditions).
Crew 2 (pilot, co-pilot)
Passengers 21-25
Number of Engines 2 ea
Number of Hard Points INA
Dimensions
Length 15.53 m
Height 4.92 m
Main Rotor Diameter 15.60 m
Disc Area 191.1 sq m
Cabin Length 6.05 m
Cabin Width 1.80 m
Cabin Height 1.55 m
Cabin Volume 11.4 cu m
Empty Weight 4,265 kg
Maximum Takeoff Weight, with Internal Load 9,000 kg
Maximum Takeoff Weight, With Sling Load 9,350 kg
Internal Load Weight 3,000 kg
Automotive
Engine Name 2 x Turbomeca Makila 1A
Engine Type Turboshaft
Engine Power 1,780 shaft hp each
Cruise Speed 251 kph
Climb Rate 426 m/min
Hovering Ceiling, in Ground Effect 2,800 m
Hovering Ceiling, Out of Ground Effect 1,650 m
Range, with Internal Tanks 871 km
Range, with External Tanks 1,260 km
Main Gun System
Note mix of air-to-surface missiles, 20-mm; or 7.62-mm gun pods, 7.62-mm door guns, and rocket pods; - or -2 x ASW torpedoes; or 2 x AM 39 Exocet missiles; or up to 6 AS15TT anti-ship missiles
Fire Control and Avionics
Fire Control System Type INA
Fire Control Radar INA
Navigation Radar INA
Protection
Add on Armor INA
Stealth Properties None
Heat Signature Reduction INA
NBC Protection INA
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
H
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
15.53 m
Width
Height
4.92 m
Weight
4265 kg
Operators (8)
China
Brazil
Argentina
Ecuador
Greece
Switzerland
Thailand
Venezuela
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