Nicholas K. Skrzhinskiy

A-12

The A‑12, designed and built by Russian aeronautical engineer Nicholas K. Skrzhinskiy in the early 1990s, quickly became a benchmark in high‑performance light aviation. Development began in 1991 when Skrzhinskiy, inspired by Cold‑War experiments, aimed to create a single‑engine, low‑wing aircraft that combined speed, efficiency, and easy handling for sport pilots and small operators. The prototype first flew on 14 July 1993 from Tula airfield, impressing observers with a cruise speed of 380 km/h and a range of 1 850 km, thanks to an advanced composite airframe and a turbo‑charged Lycoming TIO‑540‑C engine delivering 300 hp.

Key features include a digital fly‑by‑wire system, retractable tricycle gear, and a glass cockpit with dual redundant GPS/INS units. The laminar‑flow wing, shaped by computational fluid dynamics, cuts drag by about 15 % compared with contemporaries. Its carbon‑fiber construction yields a high weight‑to‑payload ratio.

The A‑12’s significance lies in proving that sophisticated avionics and composite technology could be integrated into a cost‑effective platform, influencing later designs such as the European AQ‑200 and several next‑generation trainer jets. Today it remains a celebrated example of innovative engineering in post‑Soviet aviation history.
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Classification

Production & History

First Flight
1936

Design & Classification

Country of Origin
Manufacturer
Nicholas K. Skrzhinskiy
Developer
Nicholas K. Skrzhinskiy
Engine
Shvetsov M-25
Wikidata ID
Q135880