Antonov An-28

1972

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Antonov An-28

Carrying the NATO reporting name Cash, the An-28 is a development of the piston-engined An-14. It is a short-range twin-turboprop light general-purpose aircraft, expected to enter production with WSK-PZL-Mielec of Poland in 1980. The first prototype flew in September 1969 and had a retractable landing gear and Isotov TVD-850 engines. The An-28 now has a non-retractable tricycle type landing gear and two 723kW Glushenkov TVD-10B turboprops. A much larger cabin accommodates up to 19 passengers or a variety of alternative payloads, including scientific, medical or agricultural spraying equipment.

Antonov An-28

Specification 
 CREW1-2
 PASSENGERS15-26
 ENGINE2 x turbo prop TVD-10B, 705kW
 WEIGHTS
  Take-off weight5100 kg11244 lb
  Empty weight3000 kg6614 lb
 DIMENSIONS
  Wingspan22.1 m73 ft 6 in
  Length13.0 m43 ft 8 in
  Height4.5 m15 ft 9 in
 PERFORMANCE
  Max. speed350 km/h217 mph
  Cruise speed300 km/h186 mph
  Ceiling6000 m19700 ft
  Range w/max.fuel1300 km808 miles
  Range w/max payload1000 km621 miles

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