Design and Origins
Designed by engineer Ermenegildo Preti, the Agusta CP-111 first flew in 1951. It was a three-seat variant of the CP-110, sharing a wooden construction with plywood skin.
Key Features and Powerplant
This model distinguished itself from its predecessor by featuring a fixed landing gear and an improved power plant. It was equipped with an Avco Lycoming O-435-1 engine, providing enhanced performance.
Performance Challenges
Despite the installation of a more powerful engine, the flight characteristics of the CP-111 deteriorated compared to the CP-110, even with the same takeoff weight. This decline was primarily due to increased frontal drag, as the fixed landing gear and wider engine contributed significantly to this aerodynamic disadvantage.
Technical Specifications
| Modification | CP-111 |
| Wingspan, m | 10.60 |
| Length, m | 7.40 |
| Height, m | 2.75 |
| Maximum takeoff weight | 1100 |
| Engine type | 1 Piston engine Avco Lycoming 0-435-1 |
| Power, hp | 1 x 185 |
| Maximum speed, km/h | 220 |
| Cruising speed, km/h | 190 |
| Practical range, km | 650 |
| Crew | 1 crew |
| Payload | 2 passengers |
Image gallery of the Agusta CP-111
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