Development of the Y-9 may have begun as early as 2002 as theY-8X program. The program was a collaborative effort withAntonov – the designers of theAn-12 that it was ultimately derived from – and was aimed at competing with theLockheed Martin C-130J Super Hercules. By September 2005, the Y-9 designation was being used.[4] The Y-9 received design features originally intended for the Y-8F600,[4] which was cancelled in 2008.[5]
Shaanxi had hoped to conduct the first flight as early as 2006, but it was delayed. Design changes were made in 2006,[3] with the design being frozen by January 2010. After the design freeze, it was suggested that the first flight would depend on securing a launch customer; construction had also not yet commenced.[5] The aircraft finally flew in November 2010.[6]
The Y-9 is powered by fourWoJiang WJ-6Cturboprop engines. The propellers are six-bladed and made with Chinese JL-4 composites. The WJ-6C is replaced by thePratt & Whitney Canada PW150B in the Y-9E export variant.[4]
The cruise speed is 300knots (560 km/h; 350 mph) with an endurance of around 10.5 hours.[7]
The cargo bay has an internal volume of 155 m3 and is fitted with cargo handling rollers and tie-down rings. The rear entrance to the cargo bay also functions as a ramp.[1][8]
^abcdFisher, Richard D. Jr. (2008).China's Military Modernization: Building for Regional and Global Reach. Greenwood. pp. 180–81.ISBN978-0-275-99486-0.
^abcdefRupprecht, Andreas (29 October 2018).Modern Chinese Warplanes: Chinese Air Force - Aircraft and Units. Harpia Publishing. p. 92.ISBN978-09973092-6-3.
^Yunpeng, Li; Lina, Chen (20 December 2017)."陆军部队第二架运-9型运输机列装".Ministry of National Defence of the People's Republic of China. Archived fromthe original on 26 December 2017. Retrieved26 December 2017.