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https://en.wikipedia.org/wiki/Antonov_An-14
The Antonov An-14 Pchelka (Russian: «??????», "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 order). 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. With very stable flight characteristics, the An-14 could be flown by most pilots after a few hours of basic training. A small number of An-14s are still in airworthy condition. Role Utility transport Manufacturer Antonov First flight 15 March 1958 Introduction 1966 Status In service as private aircraft Primary users Soviet Air Force Aeroflot Afghan Air Force East German Air Force Produced 1965–1972 Number built 332 Developed into Antonov An-28 Specifications (An-14) General characteristics Crew: two Capacity: 6-8 passengers / 720 kg (1,587 lb) payload Length: 11.36 m (37 ft 3 in) Wingspan: 21.99 m (72 ft 2 in) Height: 4.63 m (15 ft 2 in) Wing area: 39.72 m2 (427.5 sq ft) Aspect ratio: 12.15:1 Empty weight: 2,600 kg (5,732 lb) Gross weight: 3,450 kg (7,606 lb) Max takeoff weight: 3,600 kg (7,937 lb) Cabin size: 3.1 m × 1.53 m × 1.6 m (10.17 ft × 5.02 ft × 5.25 ft) Powerplant: 2 × Ivchenko AI-14RF 9-cylinder air-cooled radial piston engines, 220 kW (300 hp) each Propellers: 3-bladed variable-pitch propellers Performance Maximum speed: 210 km/h (130 mph, 110 kn) Cruise speed: 180 km/h (110 mph, 97 kn) Landing speed: 80 km/h (50 mph; 43 kn) Range: 650 km (400 mi, 350 nmi) Service ceiling: 5,000 m (16,000 ft) Take-off run: 100–110 m (328–361 ft) Landing run: 110 m (361 ft) * |
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