Westland F.7/30 Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
23 March 1934 |
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F.7/30: |
1 - Westland |
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Type Specification | |
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Applies to: |
Westland F.7/30 |
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Type: |
Interceptor fighter to specification F.7/30 |
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Wing: |
Single bay biplane with staggered, unswept, unequal span wings. All wings have dihedral with the upper wing roots an increased dihedral angle. All metal structure with fabric covering. Ailerons on upper wing only |
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Fuselage: |
All metal fuselage of oval section filling the interplane gap. |
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Tail Unit: |
Braced tailplane at base of fin with rudder and split, balanced elevators |
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Landing Gear: |
Divided type fixed gear with each mainwheel attached to lower longeron by oleo leg and radius rod with axles meeting on a pillar under the fuselage. Tail wheel |
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Power Plant: |
One 600 hp Rolls-Royce Goshawk IIS twelve-cylinder V inline evaporatively-cooled engine mounted between the wings driving a two-blade wooden propeller in the nose |
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Accommodation: |
Pilot in enclosed cockpit forward of the upper wing |
Armament: |
Four fixed Vickers guns mounted in the fuselage sides |
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Dimensions | |
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Span: |
38 ft 6 in |
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Length: |
29 ft 6 in |
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Height: |
10 ft 9 in |
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Wing Area: |
370 sq ft |
Weights | |
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Empty: |
3,624 lb |
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Loaded: |
5,170 lb |
Performance | |
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Max Speed: |
185 mph at 15,000 ft |
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Climb: |
17.5 min to 20,000 ft |
Preserved in British Museums | |
None known | |
Web Sites | |
None known | |