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 m72 ft 6 in
    Length13.0 m42 ft 8 in
    Height4.5 m14 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

Comments 
ronald frantzen, amsa_rfm(@)hotmail.com, 08.05.2008

dr ser
I would like to know all the information that this aircrfat having.. performance, motor , tce, thank you

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