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 Western Flying, vol. 5, no. 1, Jan. 1929, pp. 54, 56, 1 fig.; and Aeroplane, vol. 36, no. 14, Apr. 3, 1929, p. 548, 1 fig.)


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    Titel :

    Fairchild 21 low-wing monoplane


    Weitere Titelangaben:

    Airway Age


    Erschienen in:

    Airway Age ; 10 , n 1


    Erscheinungsdatum :

    1929


    Format / Umfang :

    2 pages


    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