Top speed 230 km/h Length 8.58 m Manufacturer Utva Aviation Industry | Wingspan 10 m First flight August 1956 | |
![]() | ||
The UTVA Aero 3 was a piston-engined military trainer aircraft built in Yugoslavia to replace the Ikarus Aero 2 then in service. One hundred ten were built, in Yugoslav Air Force service from 1958 to mid-1970s. It was superseded by the UTVA 75.
Contents

Design and development
First flown in 1956 the Aero 3 was designed to meet a Yugoslav Air Force requirement for a primary trainer that could also be used in the army co-operation role.

The Aero 3 was a low wing cantilever monoplane that seated the student and instructor in tandem under a bubble canopy. Of all wood construction it had a fixed, tailwheel landing gear and powered by a nose-mounted 190 hp (142 kW) Lycoming O-435-A piston engine.
Former military operators

Aircraft on display
A UTVA Aero 3 prototype and UTVa Aero 3 are on display [1]
Specifications
Data from
General characteristics
Performance