The Cicare CH-14 is the first of a family of helicopters designed for armed forces, security, and civil markets. First flight was in Mar 2007.

Overview

Data on design, manufacture and status

Design authority: Cicaré S.A.

Primary manufacturer: Cicaré S.A.

Parent type: No type defined

Aircraft status: In development

Configuration

Primary flight and mechanical characteristics

VTOL type: Helicopter

Lift configuration: Single main rotor

Dedicated control device: Tail rotor

Crew required: 1-2

Crew seating: Tandem

Landing gear: Skids

Overall Dimensions

Data on aircraft size

Overall Length: 11.61 m (38.1 ft)

Engine Details

Aircraft powerplant (lift and/or propulsion)

Total number of engines: 1

Engine designation: RR M250-C20B turbine

Engine manufacturer: Rolls-Royce Corporation

Max continuous power: 276 kW (370 hp)

Take-off / rated power: 313 kW (420 hp)

Weights and Performance

Data on aircraft weight and flight characteristics

Max Gross Weight (ground): 1450 kg (3197 lb)

Max Gross Weight (airborne): 1828 kg (4030 lb)

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