The A.115 was a developed version of the Bell 47J-3. Featuring an open rear fuselage structure and powered by a 480shp Turbomeca Astazou II turboshaft, one prototype, I-AGUC, was built.
Agusta A-115
Engine: 1 x 480hp Turbomeca Astazou II turboshaft
Main rotor diameter: 11.33m
Length rotors turning: 13.30m
Fuselage length: 9.90m
Height: 2.94m
Take-off weight: 1350kg
Empty weight: 730kg
Max speed: 170km/h
Cruising speed: 150km/h
Dynamic ceiling: 4750m
HIGE: 4206m
HOGE: 3399m
Range: 260km
All Aero 