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.)
Mohawk, the Mohawk "Pinto."
Flight
Flight ; 20 , n 4
1928
2 pages
2 Fig.
Article (Journal)
English
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Engineering Index Backfile | 1928
Engineering Index Backfile | 1930
Engineering Index Backfile | 1930
Engineering Index Backfile | 1927
The Mohawk Pinto two-place low-wing monoplane
Engineering Index Backfile | 1929