Single-place, open-cockpit, low-wing monoplane powered with 3-cylinder 30-hp. Anzani engine; full cantilever wing below fuselage; weight only 440 lb. empty; no external bracing; landing gear has very wide tread; tail skid is wheel mounted in rudder and fitted with brake; rectangular fuselage of welded steel tubing; manufactured by Niles Aircraft Corp. (see also Aero Digest, vol. 12, no. 4, Apr. 1928, p. 598, 2 figs., and Flight, vol. 20, no. 50, Dec. 13, 1928, pp. 1050-1051, 2 figs.)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Niles. The Williams Monoplane


    Additional title:

    Aviation


    Published in:

    Aviation ; 24 , n 14


    Publication date :

    1928


    Size :

    2 pages


    Remarks:

    5 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Niles. The Williams Monoplane

    Engineering Index Backfile | 1928


    Niles. The Williams Monoplane

    Engineering Index Backfile | 1928


    Wendt monoplane

    Engineering Index Backfile | 1938


    Wendt monoplane

    Engineering Index Backfile | 1938


    Tandem monoplane

    Engineering Index Backfile | 1943