Supermarine Seagull ASR.I Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
14 July 1948 |
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Seagull ASR.I: |
2 - Supermarine |
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Type Specification | |
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Applies to: |
Supermarine Seagull ASR.I |
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Type: |
Air sea rescue and reconnaissance flying boat |
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Wing: |
Cantilever parasol wing mounted on a pylon over the fuselage. All metal construction with unswept leading edge and forward swept trailing edge |
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Hull: |
Hull structure comprises two longerons and the chines, with a series of light alloy frames, all covered in flush riveted Alclad sheet |
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Tail Unit: |
All metal cantilever tailplane and elevators with 20 degree dihedral. Fins and rudders are mounted on the ends of the tailplane and are mounted at 90 degrees to tailplane |
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Landing Gear: |
Retractable tricycle type. Main gear retracts rearward into recesses on side of hull |
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Power Plant: |
One 1,815 hp Rolls-Royce Griffon 29 driving two three blade contra rotating propellors. Engine mounted at junction of pylon and wing |
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Accommodation: |
Crew of three all seated in hull, with pilot and copilot in enclosed cockpit with last crew member in cabin behind |
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Dimensions | |
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Span: |
52 ft 6 in |
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Length: |
44 ft 1.5 in |
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Height: |
15 ft 10.5 in |
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Wing Area: |
432 sq ft |
Weights | |
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Empty: |
10,510 lb |
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Loaded: |
14,500 lb |
Performance | |
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Max Speed: |
260 mph |
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Max Rate of Climb: |
1,430 ft/min |
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Service Ceiling: |
23,700 ft |
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Range: |
875 miles |
Preserved in British Museums | |
None known | |
Web Sites | |
None known | |