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UTVA UTVA-75А21


General information


ManufacturerUTVA
ModelUTVA-75
ModificationUTVA-75А21
CountryYugoslavia
Years1976
TypeReconnaissance aircraft
Main rotor diameter-
Tail rotor diameter-
Wingspan9.73 m
Length7.11 m
Height3.15 m
Wing area14.63 m2
Zero fuel weight-
Empty weight685 kg
Maximum takeoff weight960 kg
Normal takeoff weight-
Flight duration-
Engine1 Textron Lycoming IO-360-B1F
Power1 x 180 HP
Thrust-
Maximum speed215 km/h
Cruising speed185 km/h
Rate of climb-
Practical range2000 km
Service ceiling4000 m
Hovering ceiling-
Crew2