Short 360 — British twin-engined commuter turboprop

Design and characteristics

The aircraft features a high-wing layout and a boxy, spacious cabin that prioritizes internal volume and ease of loading. Its propulsion consists of two turboprop engines, providing economical cruise performance for short sectors. Notable design elements include large rectangular windows for cabin light and visibility, a straightforward systems architecture for maintainability, and a robust undercarriage suited to smaller airfields.

History and development

The Short 360 was developed as a derivative of the earlier Short 330, sharing many structural elements while offering increased capacity and improved aerodynamic refinements. Its first test flight in 1981 marked the start of a production run that continued through the 1980s. The type was assembled in Belfast and sold to operators around the world.

Uses and variants

Operators employed the Short 360 on domestic flights and short regional links, and in special missions such as freight, aerial survey, and light military transport. Some airframes were modified into combi or freighter configurations. The basic, practical layout made it attractive to small carriers and charter operators.

Operational notes and production

Production of the model ran from 1981 to 1991. Throughout its service life the type was valued for low operating costs on short sectors and for its simple, utilitarian design. While many examples have been retired, several remain in use in niche roles or as conversions.

Key facts

• Type: airliner with twin turboprops (twin-engined configuration).
• Origin: Built by Short Brothers in Belfast.
• Seating: Typically around 30 passengers.
• Lineage: Developed from the Short 330.
• Service entry and production: First flew in 1981; produced until 1991.

Today the Short 360 is remembered as a practical and unadorned commuter workhorse that met the needs of regional airlines during the 1980s and beyond.