Xian Y-7

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Xian Yunshuji Y-7
President Airlines XAC Y7-100C KCS.jpg
Xian Y-7-100C
Type: Short-haul transport aircraft
Design country:

China People's RepublicPeople's Republic of China People's Republic of China

Manufacturer:

Xi'an Aircraft Company

First flight:

December 25, 1970

Commissioning:

January 1984

Number of pieces:

approx. 200

The Xian Yunshuji Y-7 (also: Y-14) is a Chinese version of the Soviet short-haul passenger aircraft Antonov An-24 of the Xi'an Aircraft Company, developed by reverse engineering from 1987, with modified aerodynamics and seats for 48 to 52 passengers.

description

Development began in April 1966. The first flight of four prototypes took place on December 25, 1970. Approval was only obtained in January 1984, as the first machines did not achieve certification in 1977 due to the weak engines. In 1980 an improved version followed with WJ-5A-1 engines with 2,137 kW instead of the 1,879 kW original engines. In contrast to the Antonov, the Y-7 was initially powered by two Wongan WJ5E engines developed with the help of General Electric, and from 1998 (as the Y7-200A) by two Pratt & Whitney PT127J turboprops , each with 2,026 kW. The Chinese Air Force operates around 30 Y-7s, according to US estimates. A total of around 200 Y-7s were built, with the freight version Y7H-500 still being produced around 2009. Outside of China , the Y-7 is also operated in Iran , Cambodia , Laos and Mauritania and Zimbabwe .

In 1995, China tried to have the aircraft certified in the USA, but it did not succeed. After the Wuhan Air accident in 2000, the aircraft was also withdrawn from passenger transport in China.

variants

  • Y-7-100: improved version with a modified cockpit (only three instead of five seats in the cockpit) and a modified cabin and winglets .
  • Y-7-200: Version with new avionics and without winglets
  • Y-7-200A: Version with two Pratt & Whitney PW127C turboprops. First flight in 1993, registration in 1998 The MA60 was developed on this basis .
  • Y-7-200B: Version for the Chinese market
  • Y-7-300: version with reduced weight
  • Y-7H: (also initially Y-14-100) an unlicensed version based on the An-26. First flight in 1988.
  • Y-7-500H: Freighter version based on the An-26 with WJ-5E engines. First flight on March 24, 1992, registration on December 30, 1993

Incidents

There were a total of seven accidents involving this type.

Technical specifications

Parameter Data of the Y-7-100
length 23.71 m
span 29.64 m
height 8.55 m
Wing area 75 m²
Wing extension 11.71
Wing loading
  • minimum (empty weight): 199 kg / m²
  • maximum (max. takeoff weight): 290 kg / m²
Empty mass 14,900 kg
Max. Takeoff mass 21,800 kg
Engines two Wongan WJ-5A with 2080 kW each

See also

Web links

Commons : Xian Y-7  - collection of pictures, videos and audio files

Individual evidence

  1. ^ Rejected at Home, Chinese Planes Crash Abroad , Epoch Times , October 3, 2013
  2. Sinodefence: Y-7 Transport Aircraft ( Memento of the original dated February 6, 2009 in the Internet Archive ) Info: The archive link was automatically inserted and not yet checked. Please check the original and archive link according to the instructions and then remove this notice. @1@ 2Template: Webachiv / IABot / www.sinodefence.com
  3. FliegerRevue February 2009, pp. 10–14, The land of the middle takes off
  4. ^ A Tarnished Turboprop Clouds China's Aviation Dream , WSJ, March 20, 2016
  5. Jane's Defense: Xian (Antonov) Y-7
  6. Accident Statistics Xian Y-7 , Aviation Safety Network (English), accessed on August 15, 2016.
  7. Wuhan Airlines Xian Yunshuji Y7-100C 06/22/2000 ( Memento from February 28, 2005 in the Internet Archive )
  8. ^ Accident report B-3479 , Aviation Safety Network , accessed on August 15, 2016.
  9. Airliners.net: The Antonov An-24/26/30/32 & Xian Y-7