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H215-Technical-Data

H215-Technical-Data
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Technical Data

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

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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 • Monocoque tail boom with tail rotor protection and stabilizer • • Polyurethane white paint and Dinol AV30 re-inforced anti-corrosive treatment • • Front part of the tail boom arranged as a luggage • • Fuselage upper part used as transmission deck • • Fuselage lower part fittable with the floatation gear and the crashworthy installation (tanks) • Engine cowlings serving as a work platform when in the open position • Provisions for external...

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Technical Data POWER PLANT__ turbine engines in two separate groups with own starting, feeding, lubricating, cooling and governing systems • 1 fuel system of 2,043 litres (540 US gal.) usable capacity comprising 6 tanks, arranged in 2 groups, 4 booster pumps, 1 transfer pump and a low/high fuel level warning system. The pipes are of the crashworthy type • Provisions for ferrying, central auxiliary and external tanks • 2 engine bay fire-detection systems • 1 two-cylinder selective fire-extinguishing system • 2 engine chip detectors • Engine air intakes protected against icing by grids...

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© 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 - 2016 Printed by SPI (France)

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