Antonov An-74

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An-74
File:Antonov-An-74.jpg
An An-74T formerly operated by Antonov Airlines
General information
TypeTransport aircraft
National originSoviet Union / Ukraine
ManufacturerAntonov
StatusIn service
Primary usersRussian Air Force
Number built195 (An-72 & An-74)[1]
History
Manufactured1986–present
Introduction date1983
First flightSeptember 29, 1983 [2]
Developed fromAntonov An-72
File:Antonov An-74P, MChS Rossii - Russia Ministry for Emergency Situations AN2171485.jpg
Front view which suggested the nickname "Cheburashka"

The Antonov An-74 (Russian: Антонов Ан-74, NATO reporting name: Coaler) is a Soviet/Ukrainian transport aircraft developed by Antonov. It is a development of the An-72, with upgraded equipment, upgraded radar, extended range, a crew of five, a larger avionics bay and capabilities to be equipped with ski gear.

The An-72 and An-74 get their nickname, Cheburashka, from the large engine intake ducts,[3] which resemble the oversized ears of the popular Soviet animated character of the same name.

Design and development

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The An-74 was initially an upgrade of the An-72 test aircraft, intended to be used in the Arctic and Antarctica; and had the designation An-72A "Arctic".[4] The aircraft's main purpose is to deliver cargo, equipment and personnel over short- and medium-range routes in any climatic conditions ranging from −60 to 45 °C (−76 to 113 °F) and at any latitude, including the North Pole, and high altitudes. It can operate to and from low grade airstrips such as concrete, pebble, ice and snow aerodromes.

Produced in tandem with the An-72, the An-74 can be fitted with wheel-ski landing gear, de-icing equipment and a number of other upgrades allowing the aircraft to support operations in Arctic or Antarctic environments.

File:Antonov An-74 2.jpg
An-74 on landing with thrust reversers deployed

An unusual design feature of the An-74 (as well as An-72) is the use of the Coandă effect to improve STOL performance, utilizing engine exhaust gases blown over the wing's upper surface to boost lift. The powerplant used is the Lotarev D-36 turbofan engine. The An-74 bears some resemblance to the Boeing YC-14, a prototype design from the early 1970s which had also used overwing engines and the Coandă effect.

The rear fuselage of the aircraft has a hinged loading ramp with a rear fairing that slides backwards and up to clear the opening. The An-74 has a payload of around 11 tons including up to ten passengers in the cargo version, or up to 52 seats in the passenger version; the operating ceiling is 10,100 metres (33,100 ft) and cruising speed is 550 to 700 kilometres per hour (300 to 380 kn; 340 to 430 mph).[5] The aircraft may also be used for highly specialized operations:

  • pilotage and vessel escort;
  • establishing and servicing of drifting stations;
  • research operations in Arctic or Antarctic regions;
  • visual ice patrol;
  • fishery reconnaissance.

Operational history

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The first An-74 flight took place on September 29, 1983, four years after the An-72, its parent aircraft. Almost immediately after, cold-weather testing and Arctic operations began taking place, fulfilling the intentions of the aircraft designers. Notably, an An-74 evacuated the crew of Arctic station SP-32 on March 6, 2004.[6]

As of January 1, 2006, twenty-three out of thirty aircraft registered in Russia were in operation.[citation needed]

Variants

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File:Antonov An-74TK-200VIP, Ministry of Internal Affairs of Ukraine AN1532079.jpg
Ministry of Internal Affairs of Ukraine An-74TK-200VIP
File:Antonov An-74D AN1528064.jpg
Shar Ink An-74D
  • An-74: Arctic/Antarctic support model with room for five crew, increased fuel capacity, larger radar in bulged nose radome, improved navigation equipment, better de-icing equipment, and can be fitted with wheel-skis landing gear.
  • An-74-200: Military transport based on the An-74T
  • An-74-200D: VIP/executive transport version of the An-74TK-200. Also called An-74D.
  • An-74A: Passenger or freighter model.
  • An-74MP: Marine Patrol version. Can transport 44 soldiers, 22 paratroops, 16 stretchers with medical staff, or ten tonnes of cargo.
  • An-74T: Freighter version equipped with an internal winch, roller equipment, and cargo mooring points, can also be fitted with static lines for paratroops or dropping air cargo.
  • An-74T-100: Cargo version with four crew.
  • An-74T-200: Cargo version with two crew.
  • An-74T-200A: Military Transport aircraft[7][8]
  • An-74TK-100: Convertible version of the An-74T-100. It could be configured for passengers, cargo or both.
  • An-74TK-100S: Medevac version of An-74TK-100.
  • An-74TK-200: Convertible version of the An-74T-200.
  • An-74TK-200C: Cargo variant of An-74TK-200
  • An-74TK-200S: Medevac version of An-74T-200.
  • An-74TK-300: Combi aircraft with underslung engines. Developed into the An-148.
  • An-74TK-300D: VIP version of An-74TK-300.
  • An-74-400: Proposed stretch model of the An-74TK-300 with a fuselage insert to extend its length by 26 ft (8 m) and uprated engines. Also called An-174.
  • File:Antonov An-74TK-300D 3.jpg
    The An-74TK-300D variant, with underslung engines
    An-148: An-74 model designed primarily for civil customers with more fuel-efficient, conventionally mounted engines that trade the STOL capabilities of earlier models for lower operating costs and higher speed. Additional emphasis is placed on improved avionics and passenger comfort features. It was initially designated An-74TK-300, making its first flight in 2004.[9]

Operators

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Civilian

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File:RA-74051 AN72(74TK-100) UTair Cargo - United Nations livery VKO UUWW 1 (33619839673).jpg
An UTair Cargo An-74TK-100 with United Nations livery
File:Flag of Iran.svg Iran
File:Flag of Russia.svg Russia
File:Flag of Ukraine.svg Ukraine

Military

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File:An An-74TK-200 of IRGC.jpg
An An-74TK-200 of the Iranian Islamic Revolutionary Guard Corps
File:Flag of Egypt.svg Egypt
File:Flag of Iran.svg Iran
File:Flag of Turkmenistan.svg Turkmenistan

Notable accidents and incidents

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Specifications

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Data from The Osprey Encyclopaedia of Russian Aircraft 1875–1995

General characteristics

  • Crew: five (captain, first officer, navigator, flight engineer, loadmaster)
  • Capacity: up to 52 passengers
  • Length: 28.07 m (92 ft 1 in)
  • Wingspan: 31.89 m (104 ft 7.5 in)
  • Height: 8.65 m (28 ft 4.5 in)
  • Wing area: 98.62 m2 (1,062 sq ft)
  • Empty weight: 19,050 kg (42,000 lb)
  • Gross weight: 34,500 kg (76,058 lb)
  • Powerplant: 2 × Lotarev D-36 series 1A , 63.9 kN (14,330 lbf) thrust each

Performance

  • Maximum speed: 700 km/h (435 mph, 378 kn)
  • Cruise speed: 550 or 600 km/h (342 or 373 mph, 297 or 324 kn)
  • Range: 4,325 km (2,688 mi, 2,336 nmi)
  • Service ceiling: 10,100 m (33,136 ft)

See also

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Aircraft of comparable role, configuration, and era

Related lists

References

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  14. ^ Accident description for 15-2255 at the Aviation Safety Network
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