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Boulton Paul Sea Balliol T.21, circa 1962 During 1950, several pre-production Balliols were delivered to the RAF's Central Flying School for evaluation purposes. However, due to the change in air training policy, the Balliol was only ever delivered to a single Flying Training School, No. 7 at RAF Cottesmore , where the type promptly replaced ...
Boulton Paul Aircraft Ltd was a British aircraft manufacturer that was incorporated in 1934, although its origins in aircraft manufacturing began earlier in 1914 and lasted until 1961. The company mainly built and modified aircraft under contract to other manufacturers, but had a few notable designs of its own, such as the Defiant fighter and ...
Data from Boulton Paul Aircraft General characteristics Crew: 2 Capacity: 1 pax or supernumery Length: 35 ft 1.5 in (10.706 m) Wingspan: 45 ft 9 in (13.94 m) Height: 12 ft 6 in (3.81 m) Powerplant: 1 × Alvis Leonides LE.4M 9-cylinder air-cooled radial piston engine, 520 hp (390 kW) Propellers: 3-bladed constant-speed propeller Performance See also Related development Boulton Paul Balliol ...
John Dudley North (1893–11 January 1968), CBE, HonFRAeS, MIMechE, was Chairman and Managing Director of Boulton Paul Aircraft. [1]Born at 18 Kinver Road North, Peak Hill, Sydenham, London [1] in 1893 and educated at Bedford School, North became Chief Engineer for Claude Graham-White of the Grahame-White Aviation Co. Ltd., before the onset of World War I.
For a time, this part the business was known as Dowty Boulton Paul Ltd. [ 7 ] In the 1960s, Dowty Group contributed to several major British aviation projects, including the development and provision of fuel control systems for the Harrier jump jet and of power controls for the Concorde supersonic airliner. [ 1 ]
Boulton Paul drew up an alternative engine choice, using the new de Havilland Gipsy Queen 71 which was rated at 400 hp (300 kW), geared and supercharged. The P.115 would have had a top speed of 139 kn (160 mph; 257 km/h) and cruising speed of 122 kn (140 mph; 226 km/h), at 5,000 ft (1,500 m), climbing to 10,000 ft (3,000 m) in 10 minutes.
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The P.9 was an enlarged development of the P.6 single-engined biplane, with a 6 ft (1.8 m) longer fuselage and a 2 ft 6 in (0.76 m) increase in span. It used the same 90 hp (67 kW) RAF 1 V-8 engine as the P.6 but with an increased fuel capacity.