Cicaré 8
A successor to the Cicare CH-7. It first flew in 2015.
Overview
Data on design, manufacture and statusDesign authority: Cicaré S.A.
Primary manufacturer: Cicaré S.A.
Parent type: No type defined
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: 1 in Side-by-side arrangement
Landing gear: Skids
Key Characteristics
Data on key physical featuresAircraft Details
Data on aircraft configuration, weights, flight performance and equipmentRelated VFS Resources
Resources related to the 8 , provided by the Vertical Flight Society.Forum Proceedings
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