2019 H135
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Technical Data 3 Baseline Aircraft Definition GENERAL • Energy absorbing fuselage • Skid-type landing gear with skid protectors, capable of • Tail boom with fixed horizontal stabilizer taking ground-handling wheels • Vertical fin with faired-in Fenestron • Long boarding steps, LH and RH • Upper deck with fittings for main gearbox, engines, • Maintenance built-in steps and grips hydraulic and cooling system • Exterior painting (single color) • Cowlings for main transmission and engine COCKPIT, CABIN AND CARGO COMPARTMENT • One-level cabin and cargo compartment floor with integrated rails •...

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Technical Data ROTOR AND FLIGHT CONTROLS • Bearingless Main Rotor system (BMR) with improved dynamic characteristics, consisting of: • Rotor head / mast in one piece • Four fiber-reinforced composite main rotor blades with anti-erosion strips, control cuff, elastomeric lead-lag dampers and special blade tip painting • Main rotor control system with dual hydraulic boost system • Electrical trim system • Basic provisions for an easy integration of a track and balance system • Fenestron-type tail rotor with ten metal blades (asymmetric blade spacing) and stator • Tail rotor gearbox cover •...

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AIRBUS © AIRBUS HELICOPTERS, Aeroport International Marseille Provence - 13725 Marignane Cedex -France - 2018 - 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, Christian Keller Printed by...

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