Jump to content
  • Nanchang CJ-6

    198 views


    0 comments

    Description

    The Nanchang CJ-6 is a Chinese basic trainer aircraft designed and built by the Nanchang Aircraft Factory (now Hongdu Aviation) for use by the People's Liberation Army Air Force (PLAAF).

    General Information

    The CJ-6 is an all-original Chinese design that is commonly mistaken for a Yak 18A. Its predecessor, the Nanchang

    CJ-5, was a licence-built version of the Yak-18. However, advancements in pilot training brought a need for a new aircraft with improved performance and a tricycle landing gear. When the Soviet Union developed the Yak-18A, PLAAF engineers decided that its performance and design would not suit China's needs.

     

    During late 1957 Aeronautical Engineers Cheng Bushi and Lin Jiahua began work in Shenyang on a trainer design that addressed the shortcomings of the Yak-18A. The design they delivered featured an aluminum semi-monocoque fuselage, flush-riveted throughout, and introduced a modified Clark airfoil wing design with pronounced dihedral in the outer sections. The dihedral and an angular vertical tail distinguish it externally from the otherwise rather similar Yak-18A. Wind tunnel testing validated the design, and in May 1958 the program was transferred to the Nanchang Aircraft Manufacturing factory where Chief Engineer Gao Zhenning initiated production of the CJ-6. The first flight of the CJ-6 was completed on August 27, 1958 by Lu Maofan and He Yinxi.

     

    Power for the prototype was provided by a Czech-built horizontally-opposed piston engine, but flight testing revealed the need for more power, so a locally manufactured version of the Soviet AI-14P 260 hp radial, the Housai HS-6, was substituted along with a matching propeller, and with that change the CJ-6 was approved for mass production. In 1965 the HS-6 engine was upgraded to 285 hp and redesignated the HS-6A, and the aircraft equipped with the new power plant were designated the CJ-6A.

     

    A total production run estimated at more than 3,000 aircraft supplied CJ-6 aircraft for PLAAF training, as well as for export (as the PT-6) to countries including Albania, Bangladesh, Cambodia, North Korea, Tanzania, and Sri Lanka.

     

    Specfications below are for the improved and more powerful CJ-6A variant.

     

     

    Nanchang  CJ-6 61563.jpg

    Nanchang  CJ-6 2132018.jpg

    Nanchang  CJ-6 N147M.jpg

    Nanchang CJ-6 VH-LNM YMAV 20150301.JPG

    Nanchang.JPG

    Specifications

    Seats:
    2
    Length:
    8.46 m (27 ft 9 in)
    Wingspan:
    10.22 m (33 ft 6 in)
    Height:
    3.3 m (10 ft 10 in)
    Empty Weight:
    1,095 kg (2,414 lb)
    MTOW:
    1,400 kg (3,086 lb)
    Powerplant:
    1 × Zhouzhou (SMPMC) HS-6A radial engine, 213 kW (286 hp)
    Vne:
    370 km/h (230 mph, 200 kn). Maximum speed: 300 km/h (190 mph, 160 kn)
    Range:
    700 km (430 mi, 380 nmi)
    Service Ceiling:
    6,250 m (20,510 ft) +

    User Feedback

    Recommended Comments

    There are no comments to display.



    Create an account or sign in to comment

    You need to be a member in order to leave a comment

    Create an account

    Sign up for a new account in our community. It's easy!

    Register a new account

    Sign in

    Already have an account? Sign in here.

    Sign In Now

×
×
  • Create New...