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UTVA Aero 3

From Wikipedia, the free encyclopedia

Aero 3
Aero 3 - Letalski center Maribor
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. One hundred ten were built, in Yugoslav Air Force service from 1958 to mid-1970s.[1] It was superseded by the UTVA 75.

First May 1960 in Ljubljana Aero 2 and Aero 3 aircraft

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Transcription

Design and development

First flown in 1956,[2] 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.[2]

The Aero 3 was a low-wing cantilever monoplane that seated the student and instructor in tandem under a bubble canopy.[2] Of all wood construction, it had a fixed, tailwheel landing gear and was powered by a nose-mounted 190 hp (142 kW) Lycoming O-435-A piston engine.[2]

Former military operators

Aircraft on display

Serbia

A UTVA Aero 3 prototype and UTVa Aero 3 are on display [1]

Specifications

Data from [2]

General characteristics

  • Crew: 2 a teacher and student
  • Capacity: 2
  • 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 sq ft)
  • Gross weight: 1,198 kg (2,646 lb)
  • Powerplant: 1 × Lycoming O-435-A piston engine , 142 kW (190 hp)

Performance

  • Maximum speed: 230 km/h (143 mph, 124 kn)
  • Cruise speed: 180 km/h (112 mph, 97 kn)
  • Range: 680 km (422 mi, 367 nmi)
  • Service ceiling: 4,300 m (14,100 ft)

See also

Aircraft of comparable role, configuration, and era

References

Notes

  1. ^ Ugolok Neba
  2. ^ a b c d e Orbis 1985, page 36

Bibliography

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

External links

Wikimedia Commons has media related to UTVA Aero 3.
This page was last edited on 27 January 2024, at 02:39
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