Design of monoplane powered with Pratt and Whitney Wasp engine in nacelle above wing; plane is produced by Fokker Aircraft Corp. of America; undercarriage consists of axles provided by sponsons, and vertical strut to front spar carrying shock-absorber gear; provision of standard outboard motor for maneuvering on water; 125-m.p.h. maximum speed; 59-ft. wing span. (Aeronautical Eng. Supp.) (see also Aero Digest, vol. 14, no. 1, Jan. 1929, p. 74, 2 figs.; Aviation Eng., vol. 2, no. 1, Jan. 1929, p. 23, 1 fig.; Can. Aviation, vol. 2, no. 1, Jan. 1929, p. 23, 1 fig.; Airway Age, vol. 10, no. 1, Jan. 1929, pp. 66-67, 1 fig., and West. Flying, vol. 5, no. 1, Jan. 1929, p. 58, 1 fig., and translation in Aeronautique, vol. 11, no. 123, Aug. 1929, p. 264, 1 fig)
The Fokker FII monoplane amphibian
Aeroplane
Aeroplane ; 36 , n 13
1929
2 Figs.
Aufsatz (Zeitschrift)
Englisch
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The Fokker FII monoplane amphibian
Engineering Index Backfile | 1929
The Fokker FII monoplane amphibian
Engineering Index Backfile | 1929
The Fokker FII monoplane amphibian
Engineering Index Backfile | 1929
The Fokker FII monoplane amphibian
Engineering Index Backfile | 1929
The Fokker FII monoplane amphibian
Engineering Index Backfile | 1929