Culver Aircraft Company

XUC

The Culver XUC, introduced in 1946, was the company's first post‑war attempt to produce a light, two‑seat utility aircraft aimed at both private owners and flight schools. Developed at Culver’s Wichita facility, the XUC evolved from the wartime Culver LFA trainer, incorporating a more powerful 90‑hp Continental C‑90 engine and a redesigned low‑wing monoplane structure with all‑metal skin. Its most notable feature was the patented “spinner‑ejector” system, a small aerodynamic vane that automatically reduced propeller drag during engine failure, improving glide performance and safety. The aircraft also offered generous cabin visibility through large, rounded windows and a removable rear seat, allowing it to serve as a trainer, crop‑duster, or personal transport. Only 124 units were built before production ceased in 1949 due to financial pressures and competition from larger manufacturers. Nevertheless, the XUC left a lasting imprint on general aviation by demonstrating the viability of advanced safety devices in small aircraft and influencing later designs such as the Piper Cherokee. Today, surviving XUCs are prized by collectors for their sleek lines, innovative engineering, and role in the transition from wartime to civilian aviation.
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Design & Classification

Manufacturer
Culver Aircraft Company
Military Designation
XUC
Wikidata ID
Q133840084