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.; Aeroplane, vol. 36, no. 14, Apr. 3, 1929, p. 548, 1 fig.)


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    Titel :

    Fairchild 21 low-wing monoplane


    Weitere Titelangaben:

    Western Flying


    Erschienen in:

    Erscheinungsdatum :

    1929


    Anmerkungen:

    1 Fig.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    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