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.)
Fairchild 21 low-wing monoplane
Aeroplane
Aeroplane ; 36 , n 14
1929
1 Fig.
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
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