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 gallery of the Chincol
