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The Antonov An-14 Pchelka was a Soviet utility aircraft which was first flown on 15 March 1958.It was a twin-engined light STOL utility transport, that was supposed to replace the aging An-2 fleet, but failed to meet its requirements. It itself was later replaced by the Antonov An-28. The An-14 featured a non-retractable tricycle landing gear and 2 300hp engines mounted on the wing.
Specifications
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General Characteristics
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- Wingspan 62.7ft (19.1m)
- Length 34.4ft (10.5m)
- Height 13.8ft (4.2m)
- Empty Weight 8,359lbs (3,791kg)
- Loaded Weight 15,637lbs (7,092kg)
Performance
- Horse Power/Weight Ratio 0.127
- Wing Loading 19.6lbs/ft2 (95.8kg/m2)
- Wing Area 797.1ft2 (74.1m2)
- Drag Points 8520
Parts
- Number of Parts 70
- Control Surfaces 6
- Performance Cost 382
