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TR02216 CHINESE F-7 II Finback

Réf. article: 1820
55,87
Description

                                           

F-7Ⅱis an aircraft developed from the F-7I. The maiden flight was on December 30,1978. Primary modifications included: self-designed ejection seats and equipment instead of those formerly designed by Russia, a backward opening canopy with fixed front windproof windows , and a modified Pen-7engine which solved the problem of hight temperature in the rear fuselage. The landing parachute is located at the end of vertical tail with enlarged fuel tanks

Eén uitvoeringen mogelijk:

 

  • Chinees proto type 1978.

Aantal onderdelen;

  • 262 onderdelen   (4X metal parts) 

Afmeting:

  • Lengte 493 
  • Spanwijdte 225 mm.

 

Notes ()
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TR02216 CHINESE F-7 II Finback


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