Boulton & Paul P.9 Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
May 1919 |
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P.9: |
8 - Boulton & Paul |
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Type Specification | |
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Applies to: |
Boulton & Paul P.9 |
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Type: |
Two seat light aircraft developed from P.6 |
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Wing: |
Single bay, unstaggered and equal span biplane. Construction of wood with fabric covering. Ailerons on all four wings |
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Fuselage: |
Box section fuselage on lower wing. Wooden structure with fabric covering |
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Tail Unit: |
Braced tailplane with split elevators. Small fin with balanced rudder |
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Landing Gear: |
Crossaxle type gear with tailskid |
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Power Plant: |
One 90 hp RAF 1a air cooled V8 eingine in nose driving a four blade propeller |
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Accommodation: |
Tandem open cockpits, forward cockpit below upper wing, aft cockpit behind wing trailing edge |
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Dimensions | |
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Span: |
27 ft 6 in |
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Length: |
25 ft |
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Height: |
10 ft |
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Wing Area: |
323 sq ft |
Weights | |
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Empty: |
1,244 lb |
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Loaded: |
1,770 lb |
Performance | |
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Max Speed: |
104 mph at 1,000 ft |
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Climb: |
5,000 ft in 8.5 min |
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Ceiling: |
14,000 ft |
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Range: |
300 miles |
Preserved in British Museums | |
None known | |
Web Sites | |
None known | |