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BD-12

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BD-12

In 1995, American designer Jim Bede, attempting to retain the original order for the Monitor Jet MJ-7 “Bede Jet,” developed a two-seater variant of the popular BD-5 light aircraft. The new aircraft, designated BD-12, was a composite low-wing monoplane with streamlined contours.

Design and Performance

The BD-12 was equipped with a 100 hp (75 kW) four-cylinder Continental O-200A engine. Additionally, a 150 hp four-cylinder Lycoming O-320 engine could be used as a standard powerplant.

Equipped with the 150 hp engine, the BD-12 could achieve a maximum speed of 346 kilometers per hour and fly a distance of nearly 1300 kilometers.

Production Ambitions and Fate

The aircraft was being prepared for release as a kit-set. Bede also planned to start production of a four-seater version, the BD-14. However, the BD-12 did not generate significant interest.

In 1997, investors once again declared Jim Bede bankrupt. The two-seater project naturally did not develop, and the four-seater aircraft remained only in drawings. Currently, BedeCorp owns the development rights.

Technical Specifications

Modification BD-12
Wingspan, m 7.01
Aircraft length, m 6.55
Aircraft height, m 2.39
Wing area, m2 8.64
Empty weight 308
Maximum takeoff weight 594
Fuel, l 140
Engine type 1 Piston engine Lycoming O-320
Power, hp 1 x 150
Maximum speed, km/h 346
Cruising speed, km/h 322
Practical range, km 1287
Rate of climb, m/s 564
Practical ceiling, m 6400
Crew 2

Image and diagram gallery of the BD-12

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United States

ArchivoAéreo Editorial Team

A group of aviation researchers and enthusiasts dedicated to documenting and preserving global aeronautical history. All articles are reviewed to ensure historical accuracy.

Sources & Accuracy

The information presented in this technical sheet has been compiled from declassified flight manuals, historical archives, and specialized literature. While we strive for maximum accuracy, some performance data may vary depending on the specific variant or operational conditions.