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EC145

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EC145

Product catalog summary

Baseline Aircraft Definition

General Features: The EC145 features an energy-absorbing fuselage, a tail boom with a fixed horizontal stabilizer, and skid-type landing gear. It includes a cold weather kit and built-in maintenance steps.
Cockpit, Cabin, and Cargo: The aircraft has a one-level cabin with integrated rails, glazed canopy, and multiple doors for access. It includes adjustable pilot seats with safety belts, interior paneling, and various cockpit controls and instruments.

Basic Instrumentation

Central Panel: Equipped with a Central Panel Display System (CPDS) featuring LCD displays for caution and advisory information, engine parameters, and more. It includes backup conventional instruments and various warning systems.
Air Data: Features a dual pitot static system and ADC MEGHAS sensors.

Power Plant

Powered by two TURBOMECA ARRIEL 1E2 turbine engines with crash-resistant fuel systems and independent oil cooling systems. Includes fire detection and extinguishing systems.

Transmission System

Includes a main transmission with redundant lubrication and monitoring sensors, and a rotor brake system.

Rotor and Flight Controls

Features a hingeless main rotor with reinforced blades and a semi-rigid tail rotor. Includes dual hydraulic boost systems for control and a Stability Augmentation System (SAS).

Electrical Installation

Comprises a power generation system with starter/generators and a Nickel-Cadmium battery. Includes comprehensive lighting and radio systems.

Ground Handling Kit

Includes ground-handling wheels, aircraft covers, and various keys and tools for maintenance.

Documentation

Comes with a range of technical documentation, including a Flight Manual, Pilots Checklist, and various maintenance manuals available in both paper and digital formats.

Catalog excerpts

Technical Data

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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 • Glazed...

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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 system...

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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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