UTVA Aero 3

Aero 3
Aero 3
Role	Military trainer
National origin	Yugoslavia
Manufacturer	UTVA
First flight	August 1956
Introduction	1958
Primary user	Yugoslavia
Number built	110

The UTVA Aero 3 was a piston-engined military trainer aircraft built in Yugoslavia to replace the Ikarus Aero 2 then in service. 110 were built, in Yugoslav Air Force service from 1958 to mid-1970s. It was superseded by the UTVA 75.

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.

Operators

• Yugoslavia
  • SFR Yugoslav Air Force

Specifications

Data from

General characteristics

• Crew: 1
• Capacity: 1
• Length: 8.58 m (28 ft 1 in)
• Wingspan: 10.5 m (34 ft 5 in)
• Height: 2.7 m (8 ft 10 in)
• Wing area: 18.9 m² (203 ft²)
• Gross weight: 1198 kg (2646 lb)
• Powerplant: 1 × Lycoming O-435-A pistson engine, 142 kW (190 hp)

Performance

• Maximum speed: 230 km/h (143 mph)
• Cruising speed: 180 km/h (112 mph)
• Range: 680 km (422 miles)
• Service ceiling: 4300 m (14,100 ft)

See also

Aircraft of comparable role, configuration and era

• de Havilland Chipmunk
• Zlin Z-226
• PZL M-2
  

References

Bibliography

• The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985). Orbis Publishing. 

External links

• Photos and drawings at Ugolok Neba