Short Golden Hind Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
21 July 1939 |
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S.26 G-Boat: |
3 - Short, Rochester |
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Type Specification | |
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Applies to: |
Short S.26 Golden Hind |
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Type: |
Commercial flying boat |
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Wing: |
High wing cantilever monoplane. All metal construction |
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Hull: |
All metal construction with one step hull |
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Tail Unit: |
Cantilever monoplane type. Single fin and rudder |
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Landing Gear: |
None |
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Power Plant: |
Four 1,400 hp Bristol Hercules radial air cooled engines on leading edge of wing |
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Accommodation: |
Crew of seven with up to 40 passengers |
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Dimensions | |
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Span: |
134 ft |
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Length: |
101 ft 4 in |
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Height: |
Unknown |
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Wing Area: |
2,160 sq ft |
Weights | |
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Empty: |
37,705 lb |
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All-up: |
74,500 lb |
Performance | |
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Max Speed: |
209 mph |
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Range: |
3,200 miles |
Preserved in British Museums | |
None known | |
Web Sites | |
None known | |