Antonov An-140
Summary
Category | Transport aircraft |
Origin country | πΊπ¦ Ukraine |
First flight | 17 September 1997 |
Year of introduction | 2002 |
Number produced | 33 units |
Description
The Antonov An-140 is a twin-engine turboprop military aircraft designed and developed by the Ukrainian company Antonov Design Bureau. It was primarily designed for short-haul regional transport and can accommodate up to 52 passengers. The aircraft features a high-wing design and a rugged airframe, allowing for operations in challenging environments. It has been deployed by various military forces for multiple missions, including troop and cargo transport, medical evacuation, and maritime surveillance. The An-140 has seen service in different regions around the world, proving its versatility and reliable performance in various operational scenarios.
Technical specifications
Version: An-140-100 | |
---|---|
Maximum speed | 575 km/h (357 mph) |
Wing area | 51 mΒ² (549.0 sqft) |
Wingspan | 24.5 m (80.4 ft) |
Height | 8.2 m (27.0 ft) |
Length | 22.6 m (74.1 ft) |
Service ceiling | 7600 m (24934 ft) |
Empty weight | 12810 kg (28241 lbs) |
Max. takeoff weight | 19150 kg (42218 lbs) |
Climb rate | 6.83 m/s (22.4 ft/s) |
Powerplant | 2 Γ turboprops Klimov TV3-117VMA-SBM1 delivering 1838 kW |
Current operating countries
Country | Units | ||
---|---|---|---|
Russia | 8 |
Numbers in parentheses, e.g. '(+5)', indicate units ordered but not yet delivered.