Details of two-place semi-cantilever monoplane; Genet 80-hp. engine; tail wheel; wide wheel tread; welded chrome-molybdenum tube fuselage with reinforced joints; wings of wood; elevators and rudder unbalanced and jigged for interchangeability high speed 105 m.p.h.; 40 m.p.h. landing speed. (See also Airway Age, vol. 10, no. 1, Jan. 1929, pp. 71-72, 1 fig.; Western Flying, vol. 5, no. 1, Jan. 1929, pp. 54, 56, 1 fig.)


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    Title :

    Fairchild 21 low-wing monoplane


    Additional title:

    Aeroplane


    Published in:

    Aeroplane ; 36 , n 14


    Publication date :

    1929


    Remarks:

    1 Fig.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Fairchild 21 low-wing monoplane

    Engineering Index Backfile | 1929


    Fairchild 21 low-wing monoplane

    Engineering Index Backfile | 1929


    Fairchild using genet in low wing monoplane

    Engineering Index Backfile | 1929


    Fairchild using genet in low wing monoplane

    Engineering Index Backfile | 1929


    Fairchild using genet in low wing monoplane

    Engineering Index Backfile | 1929