Back Agusta A.115
1971

Agusta A.115

Developed version of the Bell 47J-3 with open rear fuselage structure and powered by a 480shp Turbomeca Astazou II turboshaft. One prot. I-AGUC.

Agusta A.115

Technical data for Agusta A-115

Engine: 1 x 480hp Turbomeca Astazou II turboshaft, main rotor diameter: 11.33m, length with 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, hovering ceiling, IGE: 4206m, hovering ceiling, OGE: 3399m, range: 260km

Comments 
shoes, e-mail, 15.06.2011

structure and powered by a 480shp Turbomeca Astazou II turboshaft.

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