The VEF I-14 was a Latvian Air Force trainer aircraft prototype, built by VEF.
== Design and development == Kārlis Irbītis began work on the I-14 in 1936 in response to an order placed by the Latvian Air Force for a new trainer aircraft. Taking inspiration from the British Miles aircraft, the I-14 was a low-wing monoplane with fixed, conventional landing gear. The single pilot sat in an enclosed cockpit. It was powered by a 200 hp Menasco B6S Buccaneer.
== Operational history == The I-14 made its maiden flight on 19 November 1937. On 23 April 1938, the aircraft was destroyed in a crash, its pilot, Bandenieks, was unhurt. Development of the I-14 was abandoned in favor of the more advanced VEF I-15.
== Specifications (I-14) == Data from General characteristics Crew: 1 Length: 7.3 m (23 ft 11 in) Wingspan: 8 m (26 ft 3 in) Height: 2 m (6 ft 7 in) Empty weight: 410 kg (904 lb) Max takeoff weight: 665 kg (1,466 lb) Powerplant: 1 × Menasco B6S Buccaneer air-cooled inline engine, 150 kW (200 hp)