Airbus Helicopters H175/EC175
Previously designated EC175. Seeking to increase MGW to 7800kg (17200lb)
Overview
Data on design, manufacture and statusDesign authority: Airbus Helicopters
Primary manufacturer: Airbus Helicopters
Parent type: Airbus Helicopters H175/EC175
Aircraft status: Operational
Configuration
Primary flight and mechanical characteristicsVTOL type: Helicopter
Lift devices: 1 Single main rotor
Dedicated control device: 1 Tail rotor
Crew required: 2 in Side-by-side arrangement
Landing gear: Wheels (non-retractable)
Key Characteristics
Data on key physical featuresAircraft Details
Data on aircraft configuration, weights, flight performance and equipmentReferences
References and sources used
Airbus H175 Technical Data 2016
Airbus Helicopters
Airbus Helicopters, 09/24/2018
Report or Technical Manual
Airbus Helicopters, 09/24/2018
Report or Technical Manual
Related VFS Resources
Resources related to the H175/EC175 , provided by the Vertical Flight Society.Forum Proceedings
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Related Public Resources
Resources related to the H175/EC175 , provided by public sources across the internet.Publicly-funded resources provided by the US Government
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Public resources provided by select scholarly and academic sources
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