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
Design authority: Cicaré S.A.
Primary manufacturer: Cicaré S.A.
Parent type: No type defined
Aircraft status: Operational
VTOL type: Helicopter
Lift devices: 1 Single main rotor
Dedicated control device: 1 Tail rotor
Crew required: 1 in Other arrangement
Landing gear: Skids