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H215M

Product catalog summary

General Specifications
The document outlines the technical specifications for the Super Puma and Cougar helicopters, including both civil and military versions. Key features include a crashworthy fuselage, monocoque tail boom, and high energy absorption landing gear. The fuselage is designed for multiple functionalities, including storage and transmission deck usage.

Cockpit Features
The cockpit is equipped with adjustable pilot and copilot seats, dual flight controls, and NVG-compatible lighting. It includes various control panels, safety features, and de-icing systems for the windshield.

Instrument Panel
The instrument panel features multifunction LCD displays, a Vehicle Monitoring System, and various navigation and communication systems. All instruments are NVG compatible.

Cabin Specifications
The cabin includes reinforced flooring, sliding doors, and soundproofing. It is equipped for troop transport and cargo, with provisions for casualty installations.

Power Plant
The helicopter is powered by two Turbomeca Makila 1A1 turbine engines, with a comprehensive fuel system and fire detection/extinguishing systems.

Transmission System
The transmission system includes a main gearbox with various sensors and cooling systems, as well as intermediate and tail gearboxes.

Rotor and Flying Controls
The helicopter features a main rotor with composite-material blades and a dual digital autopilot system.

Electrical Installation
The electrical system includes alternators, batteries, and NVG-compatible lighting systems, along with various power receptacles.

Hydraulic Systems
Two independent hydraulic systems support the servo-units, autopilot, landing gear, and rotor brake.

Airborne Kit
The airborne kit includes various protective covers, mooring fittings, and an access ladder.

Disclaimer
The document is for informational purposes only and does not constitute an offer or contract. All data is subject to change without notice.

Catalog excerpts

Technical Data

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Technical Data SUPER PUMA (Civil Version) COUGAR (Military Version)

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Technical Data 3 Baseline Aircraft Definition GENERAL • Crashworthy design fuselage including cockpit and cabin • Polyurethane white paint and Dinol AV30 re-inforced anticorrosive treatment • • Monocoque tail boom with prop for tail rotor protection and stabilizer • • Front part of the tail boom arranged as a storage • • Fuselage upper part used as transmission deck • • Fuselage lower part fittable with the floatation gear and • the crashworthy installation (tanks, seats) • • Engine cowlings serving as a work platform when in the • High energy absorption, retractable,...

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Technical Data POWER PLANT • 2 Turbomeca Makila 1A1, 1,400Kw (1,877 shp) turbine engines in two separate groups with own starting, feeding, lubricating, cooling and governing systems • 1 fuel system of 1,984 liters (524 US gal.) usable capacity comprising 6 crashworthy fuel tanks, housed in the fuselage bottom structure, two of which with self-sealing 12.7mm projectile protection, arranged in 2 groups, 4 booster pumps, 1 transfer pump and a low/high fuel level warning system. The pipes are of the crashworthy types. • Provisions for ferrying, central auxiliary and external tanks • 2 engine...

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AIRBUS © AIRBUS HELICOPTERS, Aeroport International Marseille Provence - 13725 Marignane Cedex -France 2017 - All rights reserved Airbus Helicopters' logo and the names of its products and services are registered trademarks. Airbus Helicopters reserves the right to make configuration and data changes at any time without notice. The facts and figures contained in this document and expressed in good faith do not constitute any offer or contract with Airbus Helicopters. Designed by AIRBUS HELICOPTERS Photos: © AIRBUS HELICOPTERS Cover photo: © Anthony Pecchi - 2013 Printed by SPI (France) 215M AL...

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