Description of improved Skylark two-place open land biplane; principal changes were in extension of lower wing and shortening of upper; upper wing span 28 ft. 3 in.; chrome-molybdenum steel tubing in fuselage; spruce spars and duralumin ribs in wings; top speed 95 m.p.h.; Rover 55-hp. engine.
Driggs aircraft corporation
West. Flying
Western Flying ; 6 , n 4 ; p 62 + 64
1929
1 Fig.
Aufsatz (Zeitschrift)
Englisch
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Emerald Group Publishing | 1964
British aircraft corporation 111
Engineering Index Backfile | 1961
Engineering Index Backfile | 1929
|Bethlehem Aircraft Corporation "Skylark"
Engineering Index Backfile | 1921