Hudson II

The Hudson II was a twin‑engine, low‑wing transport aircraft produced by the Lockheed Corporation in the late 1930s as an evolution of the original Hudson (Model 14). First flown in 1938, the Hudson II incorporated a strengthened fuselage, upgraded Wright Cyclone radial engines delivering 1,050 hp each, and a revised wing with a larger span for improved lift. The aircraft could accommodate up to eight passengers or a crew of three, while retaining a cargo capacity of 1,200 lb, making it popular with both civil airlines and military operators. During World War II the United States Army Air Forces requisitioned the type for coastal patrol, anti‑submarine warfare, and light transport duties, where its robust construction and reliable powerplants proved decisive in harsh northern Atlantic conditions. After the war, the Hudson II returned to civilian service, where its relatively low operating cost and dependable performance helped shape the development of post‑war regional airliners. Although only 120 units were built, the Hudson II demonstrated the value of a versatile, medium‑range transport and contributed to Lockheed’s reputation for engineering aircraft that could transition seamlessly between commercial and military roles. Its legacy endures as a benchmark for pragmatic design and operational flexibility.

Lockheed Corporation

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Design & Classification