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Encyclopedia - Antonov An-14/An-28
The Antonov An-14 was designed as a STOL freighter/feederliner, with handling characteristics which would make it possible to be flown by inexperienced pilots. Although design started in 1957, it was not until 1965 that the first aircraft went into service.
The development of the turboprop-powered An-28 Cash was even slower than that of its predecessor. It was announced in 1967 that development had started, but it was not until September that the prototype first took to the skies. It was powered by two TVD-850 turboprops, each rated at 604kW (810shp). The fuselage was stretched to accommodate 15 passengers.
Both the An-14 and the An-28 have the same pod-and-boom layout, allowing for easy loading of freight. The high wing has full-span double-slotted flaps and slats, with ailerons in the outer flap sections.
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Antonov An-14 | Powerplant | | Number Of Engines : | Two | | Powerplant type : | Ivchenko AI-14RF radial piston engines | | Max Power Rating : | 224kW (300hp) | Dimensions | | Length : | 11.36m (37ft 3.5in) | | Height : | 4.63m (15ft 2.5in) | | Wingspan : | 22.00m (72ft 3in) | | Wing Area : | 39.72m2 (422.8sq ft) | Weights | | Empty Weight : | 2,600kg (5,700lb) | | Max Take-off Weight : | 3,630kg (8,000lb) | Performance | | Cruising Speed : | 97kt (180km/h; 112mph) | | Range with maximum payload : | 350nm (650km; 406mi) | | Service Ceiling : | 16,400ft (5,000m) | | Minimum Take-off Distance : | 110m (360ft) | | Minimum Landing Distance : | 110m (360ft) | Antonov An-28 | Powerplant | | Number Of Engines : | Two | | Powerplant type : | PZL-built Glushenkov TVD-10V turboprops | | Max Power Rating : | 715kW (960shp) | Dimensions | | Length : | 12.98m (42ft 7in) | | Height : | 4.6m (15ft 1in) | | Wingspan : | 22.06m (72ft 4.5in) | | Wing Area : | 40.28m2 (433.5sq ft) | Weights | | Empty Weight : | 3,500kg (7,716lb) | | Max Take-off Weight : | 6,100kg (13,448lb) | Performance | | Cruising Speed : | 189kt (350km/h; 219mph) | | Range with maximum payload : | 275nm (510km; 319mi) |
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