Features about this monoplane which make it particularly suitable for private flying; free from external bracing; fitted with 60-80-hp. Detroit Aircat air-cooled radial engine; maximum speed 110 m.p.h.; wings of full cantilever type, tapered and set at dihedral angle; ailerons of Fries type; welded steel fuselage; fuel supplied by gravity; split-axle landing gear. (see also Aeroplane, vol. 34, no. 13, Mar. 28, 1928, pp. 428 and 430, 1 fig.)


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    Title :

    Mohawk, the Mohawk "Pinto."


    Additional title:

    Flight


    Published in:

    Flight ; 20 , n 4


    Publication date :

    1928


    Size :

    2 pages


    Remarks:

    2 Fig.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Mohawk, the Mohawk "Pinto."

    Engineering Index Backfile | 1928


    New mohawk pinto

    Engineering Index Backfile | 1930


    The Mohawk "Pinto"

    Engineering Index Backfile | 1927


    New mohawk pinto

    Engineering Index Backfile | 1930


    The Mohawk Pinto two-place low-wing monoplane

    Engineering Index Backfile | 1929