Antonow / Antonov An-28

Light STOL Utility Aircraft

Antonow / Antonov An-28, ES-DAB, c/n 1AJ005-13 © Clodoaldo Neto
Photo ©: Clodoaldo Neto (photos at airliners.net)
The Antonov An-28 is a twin-engined turboprop multi-purpose STOL transport aircraft developed by the Soviet design bureau OKB Antonov (today Antonov ASTC, Ukraine).
The An-28 is a turboprop-powered development of the Antonov An-14. The An-28 was license-produced by PZL-Mielec in Poland.
Crew1-2
Passengersmax. 14
Propulsion2 Turboprop Engines
Engine ModelGlushenkov TWD-10B / TVD-10B
Engine Power (each)705 kW945 shp
Speed350 km/h189 kts
  217 mph
Service Ceiling6.000 m19.685 ft
Range509 km275 NM
316 mi.
Empty Weight3.500 kg7.716 lbs
max. Takeoff Weight6.100 kg13.448 lbs
Wing Span22,06 m72 ft 5 in
Wing Area40,3 m434 ft
Length12,98 m42 ft 7 in
Height4,60 m15 ft 1 in
First FlightSeptember 1969
Production Statusout of production
Production Range1975-1993
Total Production191
ICAO CodeAN28
IATA CodeA28
NATO CodeCash
Data for (Version)Antonov / Antonow An-28