Antonov An-28

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Antonov An-28
PZL-Mielec An-28, Chaika Avia Company AN1414321.jpg
Type: Passenger plane
Design country:

Soviet UnionSoviet Union Soviet Union

Manufacturer:

Antonov

Production time:

1978 to 1993

Number of pieces:

191

The Antonov An-28 ( NATO code name : "Cash") is a passenger aircraft developed in the Soviet Union . It originated from the Antonov An-14 . The main differences are the use of propeller turbines and the larger cabin. The machine has STOL properties.

history

A prototype of the An-14 with a propeller turbine drive already existed. This was further developed and so the flight tests could be completed in 1972. Preparations for production of the actual prototype began in 1973. In April, the prototype received the 974 hp Gluschenko TWD-10 engines that were also intended for the series . Series production was outsourced to PZL Mielec , where the second prototype was completed in the summer of 1978.

Series production in Poland began with an initial order for 15 machines. 163 machines had been ordered by January 1, 1991.

construction

The aircraft, designed as a strutted shoulder- wing aircraft, is powered by two propeller turbines. The vertical tail is divided into two parts and is located at the end of the horizontal tail. The nose wheel landing gear is not retractable. The main landing gear wheels are on small stub wings. The machine is made entirely of metal. The cabin has no pressure ventilation .

Versions

There were attempts to use the Pratt & Whitney PT6A65B in 1991 . The An-28 PT variant equipped with it took off on its maiden flight in the spring of 1993. As the PZL M-28 Skytruck , the machines are manufactured in small numbers.

An extended variant of the An-28 has been developed as the Antonov An-38 .

Incidents

From the first flight in 1969 to November 2017, the An-28 / PZL M-28 suffered 32 total aircraft losses. 112 people were killed in 14 of them. Examples:

Technical specifications

Parameter Data
crew 1-2
Passengers 18th
length 13.10 m
span 22.06 m
height 4.90 m
Wing area 39.72 m²
Wing extension 12.25
Cabin dimensions
(width × height × length)
1.74 x 1.60 x 5.26 m
payload 2000 kg
Empty mass 3900 kg
Max. Takeoff mass 6500 kg
permissible load multiple +3 g
Top speed 390 km / h
Cruising speed 350 km / h at an altitude of 3000 m
Take-off speed 135 km / h
Initial rate of climb 500 m / min
Take-off run 260 m
Landing runway 170 m
Service ceiling 6000 m
Range 560 to 1365 km
drive two turboprop engines Gluschenko TWD-10 B with 974 PS (716 kW) each
Propeller diameter 2.80 m

See also

Web links

Commons : Antonov An-28  - Collection of images, videos and audio files

Individual evidence

  1. ^ Accident statistics Antonov An-28 / PZL M-28 , Aviation Safety Network (English), accessed on December 17, 2017.
  2. Crash: Petropavlovsk-Kamchatsky AN28 near Palana on Sep 12th 2012, missing aircraft impacted a slope , The Aviation Herald, February 6, 2013.