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Antonov An-14



 
 
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Old January 12th 20, 03:46 PM posted to alt.binaries.pictures.aviation
Miloch
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Default Antonov An-14

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
19651972

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: 100110 m (328361 ft)
Landing run: 110 m (361 ft)



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