EC145
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Technical Data

Technical Data Baseline Aircraft Definition GENERAL • Energy absorbing fuselage • Tail boom with fixed horizontal stabilizer and two endplates • Upper deck with fittings for main gearbox, engines, hydraulic and cooling system • Cowlings for main transmission and engines • Skid-type landing gear with skid protectors, capable of taking ground-handling wheels • Long boarding steps, LH and RH • Cold weather kit • Built-in maintenance steps and grips • Exterior painting (single color) COCKPIT, CABIN AND CARGO COMPARTMENT • One-level cabin and cargo compartment floor with integrated rails •...

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Technical Data TRANSMISSION SYSTEM • Main transmission including an independent redundant lubrication system and monitoring sensors • Rotor brake system • Tail rotor transmission and intermediate transmission with splash lubrication, magnetic plug and oil level sight gauge ROTOR AND FLIGHT CONTROLS • Hingeless main rotor (System Bölkow) with 4 glass and carbon fiber reinforced blades with erosion protection strip • Semi-rigid tail rotor with 2 twisted glass fiber reinforced blades of new technology with erosion protection strip • Basic provisions for an easy integration of a balancing...

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© AIRBUS HELICOPTERS, Aeroport International Marseille Provence - 13725 Marignane Cedex France 201 - 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: © Luis Vizcaino Printed by SPI (France)

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