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Helicopter CH-14

The Cicare CH-14 Helicopter is the first design of a family of helicopters which objective is to provide national solutions for the requirements of the armed forces, security, and civil market.

In January 2006, Cicare S.A. began the design and production of the experimental prototype of the ch-14. The stage of design and development were done under FAR 27.

In March 2007, the first test flights were performed. What was a dream two years ago, today is the most important helicopter development in Latin America. It counts with the participation of the Technical Department of the Army Aviation Command, the 601 Aircraft Supply and Maintenance Battalion and the Aeronautical Engineering Faculty of the National University of La Plata, of CITEFA and numerous national suppliers.

Specifications

Engine

Rolls Royce Allison 250-C20-B.
Max Take Off power: 420HP.
Max Continuous: 370 HP.

Weight

MTOW: 1450 Kg.
Empty Weight: 750 Kg.
Useable weight 700 Kg.

Performance

VNE: 240 Km.
Cruise Speed: 210Km.
Vertical speed; 8M/S.
Service Ceiling: 4500 Meters.