Utva produced light utility aircraft, including the Utva 56 four-seater, first flown in 1956, and thereafter developed through a number of U60 air-taxi/tourer/freight/agricultural/ ambulance and floatplane versions.
Derived from the UTVA-56 of 1959, the UTVA-60 differs primarily in having a Lycoming GO-480 engine in place of the GO-435.
Five versions of the basic aircraft were developed.
U60-ATI
four seat utility aircraft
Engine: 270 hp Lycoming GO-480-B1A6
Wingspan: 37 ft 5 in
Length: 26 ft 11.5 in
Height: 8 ft 11 in
Empty weight: 2100 lb
Normal loaded weight: 3192 lb
MTOW: 3571 lb
Wing area: 194.5 sq.ft
Max speed: 157 mph
Max cruise: 143 mph
ROC: 1260 fpm
Service ceiling: 17,060 ft
Range: 485 mi
AT2
dual control
U-60-AG
equipped for agricultural roles
U-60-AM
Ambulance – 2 stretchers and attendant
U-60-H
twin float seaplane
Engine: 296 hp Lycoming GO-480-G1H6
All Aero 