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SOCATA Ralley 235G


General information


ManufacturerSOCATA
ModelRallye 235 Guerrier
ModificationRalley 235G
CountryFrance
Years1975
TypeAttack aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan9.74 m
Length7.25 m
Height2.80 m
Wing area12.28 m2
Zero fuel weight-
Empty weight710 kg
Maximum takeoff weight1350 kg
Normal takeoff weight1200 kg
Flight duration-
Engine1 Textron Lycoming O-540-B4B5
Power1 x 175 HP
Thrust-
Maximum speed275 km/h
Cruising speed245 km/h
Rate of climb-
Practical range1300 km
Service ceiling4500 m
Hovering ceiling-
Crew2