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UTVA-66    

The UTVA-66 was developed from the UTVA-60 which was similar and which first flew in 1961 powered by a 270hp(201kW) Lycoming and which had a maximum take-off weight of 3615lb(1641kg). This in turn had been derived from the UTVA-56 which had first flown in 1959 powered by a 240hp (179kW) Lycoming and with a maximum take-off weight of 2838lb (1288kg). The UTVA-66 was operated by the Yugoslav Air Force in the utility role but had provision for a machine gun pack under each wing. A small number are now in civil markings in North America.

UTVA-66

C-FJRN                 c/n 0860                 Yugoslavia

4 seat light aircraft first flown in 1966

Engine: 260hp(193kW) Lycoming GSO-480-B1J6                                                                             Length: 27’6"(8.38m)                                                                                            Height: 10’6"(3.2m)Wingspan: 37’5"(11.4m)                                                                                               No.built: 200* Range: 465miles(748km)                                                               Cruising speed: 140mph(225kmh) Empty weight: 2756lb(1251kg)                                              Maximum take-off weight: 4000lb(1816kg)

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