J2K-1

The Fairchild J2K‑1 is a twin‑engine, high‑wing utility aircraft that entered service in the early 1960s. Developed from the earlier Fairchild F‑27 series, the J2K‑1 was designed to meet the growing demand for rugged short‑takeoff and landing (STOL) platforms that could operate from unprepared fields in remote regions. Its first flight took place on 12 March 1962 and the type received certification from the FAA later that year. Powered by two 850‑hp Pratt & Whitney R‑2800 radial engines, the aircraft features a reinforced all‑metal airframe, large flaps, and a high‑lift wing with leading‑edge slats, giving it a stall speed of just 55 kt and a take‑off distance of 1,200 ft. The spacious cabin, configurable for up to 18 passengers, cargo, or medevac missions, is equipped with double‑door access and a reinforced floor to accommodate heavy loads. Over 300 units were built, serving civil operators in North America, Africa, and South America, as well as several air forces for liaison and transport duties. The J2K‑1’s durability, low operating costs, and versatility helped establish Fairchild’s reputation for reliable utility aircraft and influenced the design of later STOL models such as the Fairchild 227.