Fairchild Swearingen Metroliner
Summary
Category | Transport aircraft |
Origin country | πΊπΈ United States |
First flight | 26 August 1969 |
Year of introduction | 1972 |
Number produced | 600 units |
Description
The Fairchild Swearingen Metroliner, initially designed as a commuter airliner, is a twin-engine turboprop aircraft that found utilization in various military roles. Developed in the late 1960s, it first entered service as a regional transport aircraft for civilian operators. However, its robustness and versatility led to its adoption by military organizations worldwide. The Metroliner has been employed in missions ranging from reconnaissance and surveillance to electronic warfare and even as a light transport platform. With its relatively compact size and impressive endurance, it has proven to be a valuable asset in both civilian and military operations across different regions.
Technical specifications
Version: C-26A | |
---|---|
Maximum speed | 533 km/h (331 mph) |
Wingspan | 14.1 m (46.3 ft) |
Height | 5.1 m (16.8 ft) |
Length | 12.9 m (42.2 ft) |
Service ceiling | 9449 m (31001 ft) |
Max. takeoff weight | 6350 kg (13999 lbs) |
Powerplant | 2 Γ turboprops AlliedSignal TPE331-11U-601G delivering 1044 kW |
Current operating countries
Country | Units | ||
---|---|---|---|
United States | 31 | ||
Peru | 3 | ||
Trinidad and Tobago | 2 | ||
Venezuela | 2 |
Numbers in parentheses, e.g. '(+5)', indicate units ordered but not yet delivered.
All operators
Australia β’ Peru β’ Sweden β’ Trinidad and Tobago β’ United States β’ Venezuela