Chincol

The Chincol was a two-seater aircraft designed for primary training, developed and built by the Fabrica Nacional de Aeronaves in Santiago, Chile. It first took to the air on December 14, 1955, marking a significant step for Chilean aviation.

Design and Propulsion

This aircraft was equipped with a 215 hp Continental O-470-11 engine and featured a mixed construction. These characteristics made it suitable for basic flight instruction.

Military Interest and Financial Setbacks

The Chilean Air Force showed significant interest in the Chincol, leading to preparations for the serial production of 50 units. However, despite the initial enthusiasm, the project was ultimately cancelled due to financial problems, preventing its large-scale implementation.

Technical Specifications

Modification	Chincol
Wingspan, m	10. 40
Length, m	7. 22
Height, m	2.10
Wing area, m2	15. 70
Empty weight	740
Maximum takeoff weight	1050
Engine type	1 Piston engine Continental 0-470-11
Power, hp	1 x 215
Maximum speed, km/h	210
Cruising speed, km/h	183
Practical range, km	650
Rate of climb, m/min	246
Crew, crew members	2

Image and diagram gallery of the Chincol

Chincol	Chincol
Chincol