H155 B1
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Technical Data Baseline Aircraft Definition Fuselage comprising cabin and baggage hold Baggage hold with floor tie-down net (LH and RH side) Tail boom with stabilizer fitted with 2 lateral fins and a shrouded tail rotor built into the vertical fin Retractable tricycle landing gear with axially lockable castering nose wheel unit, assisted differential brakes on pilot's and copilot's stations and parking brake 3 heated pitot heads 6 built-in foot-steps (3 on each side) for access to transmission deck Anti-corrosion protection Structural reinforcements for 1,600 kg (3,527 lb) cargo- •...

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Technical Data POWER PLANT 2 Turbomeca ARRIEL2C2 turbine engines with dual channel Full Authority Digital Engine Control (FADEC) system, and fitted with 4 chip detectors cabled with 1 warning light on warning panel The Digital Engine Control Unit (FADEC) provides the following main functions: ■ Variable rotor speed governing ■ Automatic starting sequence Each engine is equipped with an anti-icing fuel system Automatic (FADEC controlled) engine governing in back- 1 fuel system including 6 tanks split into 2 groups, with a total usable capacity of 1,257 litres (332 US gal), 4 immersed...

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© AIRBUS HELICOPTERS, Aeroport International Marseille Provence - 13725 Marignane Cedex France 2016 - 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: © AIRBUS HELICOPTERS Printed by SPI (France)

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