Short 360

The Short 360 is a twin‑engine, turboprop commuter aircraft developed by Short Brothers in the United Kingdom during the early 1980s. It evolved from the earlier Short 330, incorporating a longer, more aerodynamically refined fuselage and a redesigned tailplane that improved cruise performance and payload capacity. The first prototype flew on 27 March 1981 and certification was achieved in 1982, leading to entry into service with regional airlines around the world. Powered by two Pratt & Whitney Canada PT6A-65R engines, the 360 can carry up to 39 passengers in a high‑mounted, boxy fuselage that offers quick turn‑around and low operating costs. Its rugged fixed landing gear and short‑field capabilities make it well suited for operations from austere airports and remote airfields. Over 150 units were built, and the type became a workhorse for feeder routes, cargo conversions, and military transport. Later variants, such as the 360N, featured enhanced avionics and increased fuel capacity, extending range and improving safety. Many airframes have been converted to freight or sky‑diving roles, demonstrating the type’s adaptability and enduring value in aviation community.

Short Brothers

Classification

Dimensions

Performance

Production & History

Design & Classification