Short 360
Summary
Category | Transport aircraft |
Origin country | 🇬🇧 United Kingdom |
First flight | 1 June 1981 |
Year of introduction | 1982 |
Number produced | 165 units |
Description
The Short 360 is a military aircraft developed primarily for tactical transport and utility tasks. Designed and manufactured by British aerospace company Short Brothers plc, the Short 360 was first introduced in the 1980s. The aircraft is known for its twin turboprop engines, high-wing configuration, and spacious cabin, which enables it to carry cargo, passengers, or a combination of both. With its robust construction and versatile capabilities, the Short 360 has been utilized by various military branches worldwide, providing support in logistics, troop transport, medical evacuation, and other mission requirements.
Technical specifications
Version: 360-300 | |
---|---|
Maximum speed | 451 km/h (280 mph) |
Wing area | 42 m² (452.1 sqft) |
Wingspan | 22.8 m (74.8 ft) |
Height | 7.3 m (23.9 ft) |
Length | 21.6 m (70.8 ft) |
Service ceiling | 7620 m (25000 ft) |
Empty weight | 7870 kg (17350 lbs) |
Max. takeoff weight | 12292 kg (27099 lbs) |
Climb rate | 4.7 m/s (15.4 ft/s) |
Powerplant | 2 × turboprops Pratt & Whitney Canada PT6A-67R |
Current operating countries
Country | Units | ||
---|---|---|---|
Venezuela | 2 |
Numbers in parentheses, e.g. '(+5)', indicate units ordered but not yet delivered.