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Start | Agusta | CP-111



Agusta CP-111


General information


ManufacturerAgusta
ModelCP-111
ModificationCP-111
CountryItaly
Years1951
TypeLight aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan10.60 m
Length7.40 m
Height2.75 m
Wing area-
Zero fuel weight-
Empty weight-
Maximum takeoff weight1100 kg
Normal takeoff weight-
Flight duration-
Engine1 Avco Lycoming 0-435-1
Power1 x 185 HP
Thrust-
Maximum speed220 km/h
Cruising speed190 km/h
Rate of climb-
Practical range650 km
Service ceiling-
Hovering ceiling-
Crew1
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