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Utva Aero 3The 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 1956 to 1964. It was superseded by the UTVA 75. Description The Aero 3 was a low wing design that seated the student and instructor in tandem under a bubble canopy to enclose them. It had fixed, tailwheel undercarriage Specifications (Aero 3) General characteristics - Crew: two, student and instructor
- Length: 8.58 m (28 ft 2 in)
- Wingspan: 10.50 m (30 ft 5 in)
- Height: 2.69 m (8 ft 10 in)
- Wing area: 18.9 m² (203 ft²)
- Empty: 679 kg (1,494 lb)
- Loaded: kg ( lb)
- Maximum takeoff: 1,198 kg (2,636 lb)
- Powerplant: 1x Lycoming O-435-A, 142 kW (190 hp)
Performance - Maximum speed: 230 km/h (144 mph)
- Range: 745 km (466 miles)
- Service ceiling: 6,800 m (22,304 ft)
- Rate of climb: m/min ( ft/min)
- Wing loading: kg/m² ( lb/ft²)
- Power/Mass: kW/kg ( hp/lb)
Related content Related development: Comparable aircraft: de Havilland Chipmunk Designation sequence: Aero 2 Aero 3
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