The Utva 65 was originally an agricultural aircraft, developed as the U66 to serve various utility roles and including the armed U66V version.
The UTVA-66 first flew in 1965.
The UTVA-66 was a development of the basic four-seat UTVA-60-AT1. It could be used for glider towing.
The UTVA-66-AM was an ambulance version.
The UTVA-66-H was a twin float version similar to the standard UTVA-66 but with the optional auxiliary fuel tanks fitted as standard.
UTVA-66
Engine: Lycoming GSO-480-B1J6, 270 hp
Wingspan: 37 ft 5 in / 11.40 m
Length: 27 ft 6 in / 8.38 m
Empty weight equipped: 2756 lb / 1250 kg
MTOW: 4000 lb / 1814 kg
Max cruise: 124 kt / 143 mph / 230 kph
ROC SL: 885 fpm / 270 m/min
Service ceiling: 22,000 ft / 6700 m
Range std fuel: 404 nm / 466 mi / 750 km
Seats: 4
Cabin length: 4 ft 11 in / 1.50 m
Cabin width: 3 ft 5 in / 1.05 m
Cabin height: 3 ft 11 in / 1.20 m
All Aero 