Utva 66
| Utva 66 |
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| Utva 66 Hydro |
| Role |
Military Training Aircraft/General Aviation Aircraft |
| Manufacturer |
UTVA |
| Designer |
UTVA |
| First flight |
1966 |
| Status |
Retired |
| Number built |
130 |
The UTVA-66 is an STOL aircraft, which was produced in the former Yugoslavia. It was developed from the UTVA-60 and first flew 1966.
Description
Plane was built for landing on unprepared fields and its STOL characteristics include leading edge fixed slats, flaps and drooping ailerons. The cockpit is equipped with two flight controls. The right front and rear seats in the older version of the plane were able to accommodate two stretchers. The aircraft had floats to land on water, but they could have been exchanged for snow skis. 130 UTVA-66 aircraft were manufactured. The last aircraft were withdrawn from military service in 1999.
Variants
- 66-AM (air ambulance)
- 66H
- 66V
- 66 Super STOL
Operators
- Yugoslavia
Specifications (Utva 66)
General characteristics
- Crew: 1-2
- Capacity:
- 3 passengers
- 2 stretchers
- Length: 8.38 m (27 ft 6 in)
- Wingspan: 11.40 m (37 ft 4 in)
- Height: 3.2 m (10 ft 4 in)
- Wing area: 2.06 m² ()
- Airfoil: NACA 4412
- Empty weight: 1251 kg (2758 lb)
- Loaded weight: 1820 kg (4012 lb)
- Useful load: 569 kg (1254 lb)
- Max takeoff weight: 1820 kg (4012 lb)
- Powerplant: 1 × Lycoming GSO-480-B1J6 6 cylinder flat engine, 340 hp limited to 5 minutes. 320 hp continuous (253 kw take-off / 238 kw continuous)
Performance
See also
External links
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