Agusta CP-111

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 and diagram gallery of the Agusta CP-111

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Agusta CP-111