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1969 - 1986 ANTONOV AN-26A
Twin engine turboprop aircraft with retractable landing gear. The AN-26A seats up to 43 passengers plus 1 pilot.
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Performance specifications
Horsepower:
2 x 2,820 HP
Best Cruise Speed:
240 KIAS
Best Range (i):
1,300 NM
Fuel Burn:
328.9 GPH
Rate of climb:
1,600 FPM
Ceiling:
24,500 FT
Weights
Gross Weight:
52,911 LBS
Empty Weight:
33,113 LBS
Engine (x2)
Manufacturer:
Progress
Model:
AI-24VT
Horsepower:
2,820 HP
Overhaul (HT):
None Hrs
