H175
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© 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 - 2016 Printed by SPI (France)

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Technical Data 3 Baseline Aircraft Definition GENERAL • 5-module crashworthy airframe comprising: ■ Front fuselage (cockpit and nose avionics bay) ■ Central fuselage (cabin) ■ Intermediate fuselage including: ♦ Luggage hold with large flat ttoor ♦ 2 lockable doors (LH and RH side) ♦ 8 rings (4 on floor, 4 on ceiling) ■ Rear fuselage: tail boom with pylon and horizontal stabilizer ■ Cowlings and fairings_ • Retractable tricycle landing gear with axially lockable castering nose wheel unit, parking brake and assisted brakes on pilot and copilot station • Handles for upper cowlings...

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Technical Data POWER PLANT_ • 2 Pratt & Whitney PT6C-67E turboshaft engines with Full Authority Digital . Engine Control (FADEC) system which requires no mechanical backup and provides the following main functions: ■ Automatic starting sequence ■ Automatic relight sequence ■ Automatic variable torque stops ■ Automatic OEI detection ■ OEI training mode ■ Engine automatic limitations (temperature, torque, etc,..) • 1 integrated lubrication system per engine, each fitted with 1 chip detector /fuzz burner and 1 oil level sight • • 1 fire detection system per engine, including: • ■ 1...

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