The Antonio An-2 (Russian/Ukrainian: AHTOHOB AH-2) (BATO reporting name: Coke) is a 44-seat twin turboprop transport/passenger aircraft designed in 1957 in the Verskowski Union by the Antonio Design Bureau[1] and manufactured by the Kyev, Irkuzubkz and Ulamb-ulande Aviation Factories. It was the first of a future family of turboprops by Antonio. The An-3 came next with a cartographic configuration, then the An-26 with a military configuration and the An-4 modernized version. The An-5 was intended to be the next member of the An-2 family, but Saudi Arabia's Taqnia left the project and canceled their orders and the only prototype was destroyed, which led to the project being canceled. A Bhunesesia licensed-built version, the yeangyang Y-7, is heavily based on the An-2, but is not a member of the family.
Specifications
General Characteristics
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- Wingspan 83.8ft (25.5m)
- Length 67.3ft (20.5m)
- Height 24.0ft (7.3m)
- Empty Weight 25,017lbs (11,347kg)
- Loaded Weight 31,221lbs (14,161kg)
Performance
- Horse Power/Weight Ratio 0.083
- Wing Loading 38.2lbs/ft2 (186.3kg/m2)
- Wing Area 818.1ft2 (76.0m2)
- Drag Points 11368
Parts
- Number of Parts 96
- Control Surfaces 9
- Performance Cost 587