Supermarine Sea Eagle Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
June 1923 |
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Sea Eagle: |
3 - Supermarine |
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Type Specification | |
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Applies to: |
Supermarine Sea Eagle |
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Type: |
Commercial flying boat |
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Wing: |
Equal span three bay biplane |
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Hull: |
Wooden hull |
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Tail Unit: |
Monoplane type mounted half way up the single fin with single rudder |
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Landing Gear: |
Retractable main gear with fixed tail skid |
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Power Plant: |
One 360 hp Rolls-Royce Eagle IX engine mounted between the wings in pusher configuration |
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Accommodation: |
Pilot and mechanic in cockpit just forward of the wing with enclosed cabin for 6 passengers forward |
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Dimensions | |
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Span: |
46 ft |
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Length: |
37 ft 4 in |
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Height: |
15 ft 11 in |
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Wing Area: |
620 sq ft |
Weights | |
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Empty: |
3,950 lb |
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Overload: |
6,500 lb |
Performance | |
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Max Speed: |
93 mph |
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Climb: |
19 min to 5,000 ft |
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Range: |
230 miles |
Preserved in British Museums | |
None known | |
Web Sites | |