Antonov An-26

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An-26 "Curl"
An-26 of the Romanian Air Force
Type Light transport
Manufacturer Antonov
Status Operational
Primary users Soviet Air Force
Many others
Number built 1,403
Developed from Antonov An-24
Variants Antonov An-30, Antonov An-32

The Antonov An-26 (NATO reporting name: "Curl") is a twin-engined light turboprop transport aircraft and is a development of the Antonov An-24, with particular attention made to the potential military use. First seen in 1969, it has a modified rear fuselage with a large cargo ramp. The An-26 is also manufactured without a licence in China by Xian Aircraft Factory as the Y-14, though the designation later changed back to the Y-7 series.

Contents

[edit] Design and development

  • In 1981, An-26B was introduced. The main character of it is that it is equipped with roller gangs which can be swung up against the cabin walls when not in use. It was also equipped with two ZMDB Progress(Ivchyenko)Al-24VT turboprop engines for more power.
  • Y-7H : Chinese production version.
  • Y-7-500 : Civilian cargo aircraft. Chinese production version.


[edit] Operators

[edit] Military

Image:An-26 sfrj.jpg
Yugoslav Air Force An-26 cargo aircraft.
Image:An26.jpg
An-26 aircrafts of FRY Air Force during the Batajnica Air Show.
Source: Aerospace Source Book 2007[1]
Image:Flag of Afghanistan.svg Afghanistan
Image:Flag of Angola.svg Angola
Image:Flag of Bangladesh.svg Bangladesh
Image:Flag of Belarus.svg Belarus
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Image:Flag of Bulgaria.svg Bulgaria
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Image:Flag of the People's Republic of China.svg China
Image:Flag of the Republic of the Congo.svg Republic of the Congo
Image:Flag of Cuba.svg Cuba
Image:Flag of the Czech Republic.svg Czech Republic
Image:Flag of the Democratic Republic of the Congo.svg Democratic Republic of the Congo
Image:Flag of Ethiopia.svg Ethiopia
Image:Flag of Germany.svg Germany
Image:Flag of Guinea-Bissau.svg Guinea-Bissau
Image:Flag of Hungary.svg Hungary
Image:Flag of Iraq.svg Iraq
Image:Flag of Kazakhstan.svg Kazakhstan
Image:Flag of North Korea.svg North Korea
Image:Flag of Laos.svg Laos
Image:Flag of Libya.svg Libya
Image:Flag of Lithuania.svg Lithuania
Image:Flag of Madagascar.svg Madagascar
Image:Flag of Mali.svg Mali
Image:Flag of Mongolia.svg Mongolia
Image:Flag of Mozambique.svg Mozambique
Image:Flag of Nicaragua.svg Nicaragua
Image:Flag of Niger.svg Niger
Image:Flag of Pakistan.svg Pakistan
Image:Flag of Poland.svg Poland
Image:Flag of Romania.svg Romania
Image:Flag of Russia.svg Russia
Image:Flag of Serbia.svg Serbia
Image:Flag of Slovakia.svg Slovakia
Image:Flag of the Soviet Union.svg Soviet Union
Image:Flag of Syria.svg Syria
Image:Flag of Tanzania.svg Tanzania
Image:Flag of the United States.svg United States
Image:Flag of Ukraine.svg Ukraine
Image:Flag of Uzbekistan.svg Uzbekistan
Image:Flag of Vietnam.svg Vietnam
Image:Flag of Yemen.svg Yemen
Image:Flag of Zambia.svg Zambia

[edit] Civil

Image:MIAT plane.jpg
MIAT Antonov An-26, used for domestic transportation, at Chinggis Khaan International Airport

In August 2006 a total of 267 Antonov An-26 aircraft remain in airline service. Major operators include: Lao Airlines (6), Syrian Arab Airlines (6), Aerocom (5), ARP 410 Airlines (5), Air Urga (10), Exin (9), RAF-Avia (5), Turkmenistan Airlines (5), Iraero (7), Scorpion Air (6), Yakutia Airlines (5) and Aerogaviota (18). Some 106 other airlines also operate smaller numbers of the type.[2]

[edit] Notable accidents

[edit] Specifications (An-26)

General characteristics

  • Crew: 4 (2 pilots, 1 radio operator/engineer, 1 navigator)
  • Capacity: 40 passengers
  • Payload: 5,500 kg (12,000 lb)
  • Length: 23.8 m (78 ft 1 in)
  • Wingspan: 29.2 m (95 ft 9½ in)
  • Height: 8.32 m (27 ft 3½ in)
  • Wing area: 74.98 m² (ft²)
  • Empty weight: 15,020 kg (33,110 lb)
  • Useful load: 4,500 kg (9,900 lb)
  • Max takeoff weight: 24,000 kg (53,000 lb)
  • Powerplant: 2× Progress AI-24VT turboprops, 2,820 shp (2,100 kW (plus one Tumansky Ru-19-A300 type 7,85 kN thrust small turbojet in left nacelle which serves as APU and climb rate / high altitude cruise booster)) each

Performance

  • Cruise speed: 440 km/h (240 knots, 275 mph)
  • Range: 2,550 km (with maximum fuel; 900 to 1100 km with maximum payload) (1,380 nm, 1,580 mi, 485 nm, 595 nm)
  • Service ceiling 7500 m (17,000 ft)

[edit] References

  1. ^ "", Aerospace Source Book 2007, Aviation Week & Space Technology, January 15 2007.
  2. ^ Flight International, 3-9 October 2006

COMMERCIAL AIRCRAFT and AIRLINE MARKINGS by Christopher Chant

[edit] External links

Pictures of An 26

[edit] Related content

Wikimedia Commons has media related to:
Antonov An-26

Related development

Comparable aircraft

Designation sequence

An-14 - An-22 - An-24 - An-26 - An-28 - An-30 - An-32

Related lists

See also

cs:Antonov An-26

da:Antonov An-26 de:Antonow An-26 it:Antonov An-26 hu:An–26 nl:Antonov An-26 pl:An-26 pt:Antonov An-26 ru:Ан-26 fi:Antonov An-26 sv:Antonov An-26 th:แอนโตนอฟ แอน-26

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