It is an ultra-light, single-seat, conventional helicopter. It’s the first one in this category, built with the same mechanical solutions than the standard category helicopters. The engine is a two-strokes, two opposed cylinders, developed by Augusto Cicaré starting from motorcycle engines parts. First flight: 1982

Overview

Data on design, manufacture and status

Design authority: Cicaré S.A.

Primary manufacturer: Cicaré S.A.

Parent type: No type defined

Aircraft status: Operational

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift devices: 1 Single main rotor

Dedicated control device: 1 Tail rotor

Crew required: 1 in Other arrangement

Landing gear: Skids

Key Characteristics

Data on key physical features

Aircraft Details

Data on aircraft configuration, weights, flight performance and equipment

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