Cutaway and 3-view drawings and description of transition trainer; side by side seating featured; span 39 ft 5 in.; length 43 ft 8 in.; height 15 ft 4 in.; weight empty 7820 lb; gross weight 11,250 lb; wing area 342 sq ft; powered by Rolls Royce Derwent IX engine, static thrust at combat rating at 14,700 rpm, 3600 lb. (See also Aviation Week v 55 n 5 July 30 1951 p 29-30, 33)


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    Title :

    Fokker S.14 jet trainer takes to air


    Additional title:

    Aeroplane


    Contributors:
    Stone, I. (author)

    Published in:

    Aeroplane ; 81 , n 2087


    Publication date :

    1951


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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