The Antonov An-26 (NATO reporting name: Curl) is a twin-engined turboprop civilian and military transport aircraft, designed and produced in the Soviet Union from 1969 to 1986.[2] It is the third member of the Antonov An-24 family, coming after the An-24 and An-30, while preceding the An-32 and canceled An-132. Enjoy :7
Specifications
General Characteristics
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- Wingspan 77.9ft (23.8m)
- Length 164.0ft (50.0m)
- Height 24.6ft (7.5m)
- Empty Weight 14,001lbs (6,351kg)
- Loaded Weight 16,278lbs (7,383kg)
Performance
- Power/Weight Ratio 2.07
- Horse Power/Weight Ratio 0.122
- Wing Loading 36.4lbs/ft2 (177.5kg/m2)
- Wing Area 447.8ft2 (41.6m2)
- Drag Points 12760
Parts
- Number of Parts 60
- Control Surfaces 7
- Performance Cost 394