CP-90 Pinocchio II
The light multi-purpose aircraft CP-90 Pinocchio II was designed and built by French engineer Claude Piel in the mid-1980s. Its prototype made its inaugural flight on August 27, 1986. This innovative aircraft was conceived as a single-seat, cantilever low-wing monoplane.
Design and Development
Initially, the CP-90 Pinocchio II was equipped with a 65 horsepower Continental engine. However, the design allowed for versatility in powerplants. Alternative options included various Continental and Lycoming engines, providing a power range from 65 to 160 horsepower.
Engine Specifications and Production
In total, two examples of the aircraft were constructed. These included the F-PLCL, fitted with a 100 horsepower engine, and the F-PRIN, powered by a 90 horsepower engine. These models demonstrated the aircraft’s adaptable engineering.
Technical Specifications
| Modification | CP-90 |
| Wingspan, m | 7.20 |
| Length, m | 6.43 |
| Height, m | 1.83 |
| Wing area, m2 | 9.65 |
| Empty weight | 430 |
| Maximum takeoff weight | 556 |
| Engine type | 1 Piston engine Continental |
| Power, hp | 1 x 90 |
| Maximum speed, km/h | 241 |
| Cruising speed, km/h | 225 |
| Practical range, km | 563 |
| Rate of climb, m/min | 347 |
| Service ceiling, m | 6000 |
| Max. operational overload | 9 |
| Crew, crew members | 1 |
Image gallery of the CP-90 Pinocchio II
