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Technical Data Civil Version Military Version

Technical Data 3 Baseline Aircraft Definition The helicopter in the definition, presented hereafter, meets the certification standards for day and night VFR operations, set by the following airworthiness authorities: EASA, FAA, TCCA, ANAC, CAAC, IAC-AR. This list is not restrictive and the status of approval by other airworthiness authorities must be checked. Additional equipment item may be required by the relevant operational or certification regulation (most of them are available in catalogue). GENERAL_ • Lifting points • Mooring fixtures • Structural reinforcements for cable cutter...

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Technical Data AVIONICS_ • 1 Emergency Locator Transmitter 1 ICS + passenger interphon e 1 transponder (mode S - ADSB-out) 1 avionics master switch POWER PLANT • 1 twist grip on pilot side (for engine reduction in case of tail rotor failure and autorotation training) • 1 magnetic plug and 1 chip detector • 1 engine lubrication and oil cooling system • 1 fire detection system • 1 air-intake protective grids • 1 torque-measurement pick-up • 1 ARRIEL 2D turbine engine complete with starting, fuel supply and dual channel digital engine control system (FADEC) and 1 back-up control system that...

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AIRBUS © AIRBUS HELICOPTERS, Aeroport International Marseille Provence - 13725 Marignane Cedex -France - 2019 - All rights resei^ed 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: © Airbus Helicopters/Ned Dawson Printed by SPI...

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