Augusto Cicaré developed the CH-5 at the request of the Argentine Air Force for a lightweight helicopter with the ability to perform agricultural tasks, mainly fumigations. This robust helicopter is powered by a Lycoming engine, it has a frame of steel tubing, with blades and cabin made of composite materials. First flight: 1986

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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