Trisha Shetty (Editor)

Utva 66

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Top speed
  
230 km/h

Length
  
8.38 m

Wingspan
  
11 m

Manufacturer
  
Utva Aviation Industry

Utva 66 UTVA 66 Photos AirplanePicturesnet

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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.

Contents

Utva 66 UTVA LolaUtva UTVA 66 Specifications Technical Data Description

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Description

Utva 66 UTVA66 Specifications A photo

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 The last aircraft were withdrawn from military service in 1999.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
  • 66-A never on military service

    • Former Military Operators

     Bosnia and Herzegovina
  • Bosnian Air Force
    •  Croatia
  • Croatian Air Force
    •  Macedonia
  • Macedonian Air Force
    •  Republika Srpska
  • Republika Srpska Air Force
  • 92nd Light Multi role Aircraft Squadron
    •  Yugoslavia
  • Yugoslav Air Force
  • 461st Light Combat Aviation Squadron (1977-1988)
  • 462nd Light Combat Aviation Squadron (1977-1981)
  • 252nd Fighter-Bomber Aviation Squadron (1981–1992)

    • Aircraft on display

    Serbia
  • Museum of Aviation (Belgrade) in Belgrade

    • A number of Ultva 66 including Ultva 66H are on display. [1]

    Specifications (Utva 66)

    General characteristics

    Utva 66 Utva UTVA66 V51 Untitled Aviation Photo 1273694 Airlinersnet

  • 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)
  • Useful load: 569 kg (1254 lb)
  • Loaded weight: 1820 kg (4012 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

  • Maximum speed: 230 km/h (124 kn)
  • Range: 746 km (403 nmi)

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    Utva 66 FileUtva66 Private JP7030955jpg Wikimedia Commons

    References

    Utva 66 Wikipedia
    (Text) CC BY-SA