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 Aeroplane v 81 n 2087 July 20 1951 p 69-71)
Fokker S.14 jet trainer takes to air
Aviation Week
Aviation Week ; 55 , n 5
1951
Aufsatz (Zeitschrift)
Englisch
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Fokker S.14 jet trainer takes to air
Engineering Index Backfile | 1951
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