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VEF I-14

From Alfawiki
Adapted from the English Wikipedia article VEF I-14, available under CC BY-SA 4.0Updated 29 November 2025
VEF
IndustryAerospace
Founded1919
Headquarters
Riga
,
Latvia


The VEF I-14 was a prototype trainer aircraft developed for the Latvian Air Force by the manufacturer VEF.

Design and development

In 1936, Kārlis Irbītis initiated the design of the I-14 following a request from the Latvian Air Force for a new training aircraft. Drawing design cues from British Miles models, the I-14 featured a low-wing monoplane configuration equipped with fixed, conventional undercarriage. The pilot operated the aircraft from an enclosed cockpit designed for a single occupant. Propulsion was provided by a 200 hp Menasco B6S Buccaneer engine.

Operational history

The aircraft's first flight occurred on 19 November 1937. Unfortunately, on 23 April 1938, the prototype was lost in an accident; however, its pilot, Bandenieks, escaped without injury. Following this incident, development of the I-14 was discontinued in favour of advancing the design of the VEF I-15.

Specifications (I-14)

Template:Aircraft specs

References

Template:VEF aircraft