Technical Data

Technical Data (Civil Version) (Military Version)

Technical Data 3 Baseline Aircraft DefinitionGENERAL • Fuselage comprising the cabin and luggage hold • Nose capable of accommodating various radars (long radome) • Luggage hold with floor, tie-down net and access door (RH) • Tail boom with stabilizer fitted with 2 lateral fins and terminated by a shrouded tail rotor built into the vertical main fin • Retractable tricycle landing gear with axially lockable castering nose wheel unit, assisted differential brakes on pilots and copilot's stations and parking brake • 3 heated pitot heads • 2 ADU3200 Air Data Units • 2 Aircraft Piloting Inertial Reference...

Technical Data POWER PLANT • 2 Turbomeca ARRIEL 2C turbine engines providing each 717 kW (974 ch - 961 shp) super contingency rating, Full Authority Digital Engine Control system. The Digital Engine Control Unit (FADEC) provides the following main functions: variable rotor speed governing, training mode, automatic starting sequence. Each engine is equipped with an anti-icing fuel system (efficient down to O A T. = -20°C) • 1 fuel system including 5 tanks split into 2 groups, with a total usable capacity of 1,135 litres (300 US gal), 4 immersed canister booster pumps, 1 transfer pump and an indication...

© 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 - 2012 Printed by SPI (France)