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UTVA ( Ikarus ) Aero 3
par Damien Jeu 28 Juin 2012, 01:08
Le monomoteur d'école UTVA ( Ikarus ) Aero 3 de 1956 sur Wikipedia.en
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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It was superseded by the UTVA 75.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.
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-------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------
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It was superseded by the UTVA 75.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.
Damien- CLUB
- Messages : 1064
Re: UTVA ( Ikarus ) Aero 3
par Damien Jeu 28 Juin 2012, 01:17
Specifications
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)
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)
Damien- CLUB
- Messages : 1064
Re: UTVA ( Ikarus ) Aero 3
par Damien Jeu 28 Juin 2012, 01:19
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)
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)
Damien- CLUB
- Messages : 1064
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