M.Goodall, A.Tagg British Aircraft before the Great War (Schiffer)
Deleted by request of (c)Schiffer Publishing
PIGGOTT biplane
The third, and final, Piggott aircraft was a small two-seater biplane entered for the Military Trials of August 1912 (No. 29), for which puipose it was unsuited, being under powered, and consequently unable to perform any of the tests.
The design was of conventional tractor layout, but featured three bay wings, with a narrow gap, and single interplane struts. The crew sat exposed above the level of the top wing and were vulnerable if the machine should overturn. The tailplane extended well forward along the fuselage sides and a crescent shaped rudder extended, equally above and below the fuselage.
Power: 25-35hp Anzani three-cylinder Y-type air-cooled radial.
Data
Span 25ft 6in
Gap 2ft 6in
Area 100 sq. ft
Weight 300 lb.
Weight allup 700lb.
Length 17ft 6in
Max speed 55 mph
P.Lewis British Aircraft 1809-1914 (Putnam)
Piggott Military Biplane
As their entry for the Military Trials of 1912, Piggott Brothers and Co. Ltd., 220-224 Bishopsgate, London, E.C., built a small two-seat biplane with two cockpits in tandem. It was No. 29 in the contest, and was piloted by S. C. Parr, who qualified for his Royal Aero Club Aviator's Certificate No. 184 on 20th February, 1912, with a Bleriot at Hendon. The engine was the 35 h.p. Anzani, driving a 7 ft. Normale propeller, and the three-bay wings of only 100 sq. ft. area had single interplane struts. The pilot was seated above the upper wings, but the machine was too small to lift two occupants, and was unable even to take-off with only the pilot aboard. Span, 25 ft. 6 ins. Length, 17 ft. 6 ins. Wing area, 100 sq. ft. Weight empty, 300 lb. Weight loaded, 400 lb. Maximum speed, 55 m.p.h.