A successor to the Cicare CH-7. It first flew in 2015.

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 configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 1

Crew seating: Side-by-side

Landing gear: Skids

Overall Dimensions

Data on aircraft size

Overall Height: 1.65 m (5.4 ft)

Overall Length: 7.80 m (25.6 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Rotax Rotax 618 reciprocating

Engine manufacturer: BRP-Powertrain GmbH & Co KG

Take-off / rated power: 55 kW (74 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 480 kg (1058 lb)

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