It is a two-seat conventional helicopter. The frame and the tail boom are made of steel tubes. The main transmission has a belts stage and also a 90º gear stage; the driving to the tail rotor is made through a cardan joint. The main rotor has three blades and the commands are hydraulically controlled. First flight: 1964

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: 2.35 m (7.7 ft)

Overall Length: 8.45 m (27.7 ft)

Overall Width: 7.30 m (24.0 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: Lycoming HIO-360-A1A reciprocating

Engine manufacturer: Lycoming Engines

Take-off / rated power: 134 kW (180 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 690 kg (1521 lb)

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