Three-seater closed-cabin monoplane, powered with Curtiss OX-5 engine of 90 hp.; specially designed doors and windows, with narrow pillars; fuselage of welded chrome-molybdenum steel tubing, fabric covered; split landing gear; Rusco shock absorbers; wing cellule is of semi-cantilever monoplane type; wing structure of Alclad metal ribs mounted on routed spruce spars; welded steel tubing, fabric-covered tail surfaces; wing span 41 ft.; general characteristics and performance (See also Aero Digest vol. 12, no. 6, June 1928 pp. 966 and 968, 5 figs; West. Flying, vol. 4, no. 6, June 1928, pp. 44 and 96, 2 figs.; Automotive Industries, vol. 58, no. 19, May 12, 1928, p. 731, 1 fig)
Curtiss. Curtiss Robin
Aeroplane
Aeroplane ; 34 , n 20
1928
Article (Journal)
English
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Engineering Index Backfile | 1928
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|Engineering Index Backfile | 1929
Curtiss. New curtiss hawk army pursuit plane
Engineering Index Backfile | 1929