It is a redesign of the CICARE CH-6, now powered by the Labala GFL 2000 turbine engine, which marks the first use of this new turbine in Cicaré aircraft. First flight: 1999

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: Other

Landing gear: Skids

Overall Dimensions

Data on aircraft size

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Labala Labala GFL 2000 turbine

Engine manufacturer: Labala Turbines

Max continuous power: 75 kW (101 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Related VFS Resources

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Related Public Resources

Resources related to the CH-6T , provided by public sources across the internet.

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