H215M
1 / 5ページ

お気に入りに追加する

カタログの抜粋

Technical Data

カタログの1ページ目を開く

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

カタログの2ページ目を開く

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,...

カタログの3ページ目を開く

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...

カタログの4ページ目を開く

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...

カタログの5ページ目を開く