Twin Engine • Short Brothers • Short 360-100, Short 360-200
| Manufacturer | Short Brothers |
| Model | 360 |
| Category | Twin Engine |
| Variants | Short 360-100, Short 360-200 |
| Production Years | 1982 – 1991 |
| Seating | 30, 36 seats |
| Typical TTAF | 18,500 hours |
| Markets | United Kingdom, United States, Canada, France, Germany |
| Price Range | $75K – $450K |
The Short Brothers 360 is a British twin-engine, high-wing commuter aircraft designed and manufactured by Short Brothers of Belfast. Developed in the 1980s, it represents an evolution of the earlier Short 330, featuring improved aerodynamics, more powerful engines, and enhanced passenger comfort. The aircraft was specifically designed for regional commuter operations and short-haul routes, accommodating up to 36 passengers in a high-density configuration. Known for its reliability and ruggedness, the 360 became popular with regional airlines, air taxi operators, and cargo services throughout the 1980s and 1990s. The aircraft features a pressurized cabin, excellent short-field performance, and twin Pratt & Whitney PT6A turboprop engines that provide dependable power in diverse operating conditions. Primary operators included various European and North American regional carriers, with particular success in United Kingdom services. The 360 is characterized by its distinctive boxy fuselage, excellent payload capacity relative to its size, and proven operational safety record. Today, remaining examples continue in service with specialized operators and cargo carriers, valued for their durability and ability to operate from unprepared airfields.
Maximum Speed: 210 knots
Cruise Speed: 180 knots
Range: 725 nautical miles
Service Ceiling: 25,000 feet
Engines: 2x Pratt & Whitney PT6A-65B turboprops
Maximum Takeoff Weight: 23,500 pounds
Empty Weight: 14,900 pounds
Cargo Capacity: 7,500 pounds
Pressurization: 7.5 psi (10,000 feet cabin altitude)