| In the early 'twenties, William Beardmore & Company
initiated work on a tandem two-seat fighter under Latvian
contract. Of mixed construction with plywood
skinning and designated W.B.26, the fighter was designed
by W.S. Shackleton and, powered by a 360hp
Rolls-Royce Eagle IX liquid-cooled engine, was flown
for the first time in 1925. Featuring aerofoil-section
interplane bracing struts and angularly-clean lines, the
W.B.26 had two Constantinesco-synchronised Beardmore-
Farquhar machine guns and a similar weapon on
a Scarff mounting in the rear cockpit. The slab-sided fuselage was suspended between the wings, the lower
wing being faired into the fuselage by a Lamblin
radiator block. Despite a creditable performance only
the single prototype of the W.B.26 was built.
 | A three-view drawing (1280 x 948) |
WEIGHTS |
Take-off weight | 1805 kg | 3979 lb |
Empty weight | 1159 kg | 2555 lb |
DIMENSIONS |
Wingspan | 11.28 m | 37 ft 0 in |
Wing area | 33.07 m2 | 355.96 sq ft |
PERFORMANCE |
Max. speed | 233 km/h | 145 mph |
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