Rahul Sharma (Editor)

Antonov An 14

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Range
  
650 km

Length
  
11 m

Weight
  
2,600 kg

Manufacturer
  
Wingspan
  
22 m

Cruise speed
  
180 km/h

First flight
  
1958

Antonov An-14 Oldprops Antonov An14

The Antonov An-14 Pchelka (Russian: «Пчелка», "Little Bee", (NATO reporting name Clod) is a Soviet utility aircraft which was first flown on 15 March 1958. It was a twin-engined light STOL utility transport, with two 300 hp Ivchenko AI-14RF radial piston engines. Serial production started in 1966, and about 300 examples were built by the time production ended in 1972. The An-14 failed to replace the more successful An-2 biplane, which was manufactured until 1990, (the An-2 is still manufactured on special orders). The An-14's successor, the An-28 with turboprop engines, is still manufactured at PZL Mielec factories in Poland under the names PZL M28 Skytruck and PZL M28B Bryza.

Contents

Antonov An-14 Oldprops Antonov An14

With very stable flight characteristics, the An-14 could be flown by most after a few hours of basic training. A small number of An-14 are still in airworthy condition.

Antonov An-14 Antonow Antonov An14 Specifications Technical Data Description

Operators

 Afghanistan
  • The Afghan Air Force operated 12 from 1985 through 1991.
  •  Bulgaria
  • Bulgarian Air Force
  •  East Germany
  • East German Air Force
  •  Mongolia
  • Mongolian People's Air Force- operated 2 from early 1970s through 1980
  •  Guinea
  • Military of Guinea
  •  Soviet Union
  • Soviet Air Force
  • Aeroflot
  • Specifications (An-14)

    Data from Soviet Transport Aircraft since 1945

    General characteristics

    Antonov An-14 Antonov An14 Pchelka Little Bee on Behance

  • Crew: two
  • Capacity: 6–8 passengers or 720 kg (600 kg) cargo
  • Length: 11.36 m (37 ft 3 in)
  • Wingspan: 21.99 m (72 ft 1¾ in)
  • Height: 4.63 m (15 ft 2¼ in)
  • Wing area: 39.72 m² (427.5 ft²)
  • Aspect ratio: 12.15:1
  • Empty weight: 2,600 kg (5,732 lb)
  • Loaded weight: 3,450 kg (7,606 lb)
  • Max. takeoff weight: 3,600 kg (7,936 lb)
  • Powerplant: 2 × Ivchenko AI-14RF air-cooled radial engines, 224 kW (300 hp) each
  • Performance

    Antonov An-14 Antonov An14 Ulyanovsk

  • Cruise speed: 180 km/h (97 knots, 112 mph)
  • Range: 650 km (350 nmi, 564 mi)
  • Service ceiling: 5,000 m (16,400 ft)
  • Landing Speed: 80 km/h (43 knots, 50 mph)
  • Landing Roll: 110 m (360 ft)
  • Takeoff Roll: 100–110 m (328–360 ft)
  • Cabin size: 3.1 x 1.53 x 1.6 m (10 ft 2 in x 5 ft x 5 ft 3 in)

  • Antonov An-14 Antonov An14 Photos history characteristics of the aircraft

    Antonov An-14 httpsuploadwikimediaorgwikipediacommonsthu

    Antonov An-14 Bulgarian Air Antonov An14 LZ7001 for FS2004

    References

    Antonov An-14 Wikipedia