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Short
Crusader

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Design Company: |
Short Brothers (Rochester &
Bedford) Ltd |
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First Flight: |
4 May 2020 |
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Crusader: |
1 - Short, Rochester |
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Type
Specification |
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Applies to: |
Short Crusader |
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Type: |
Racing seaplane
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Wing: |
Low wing monoplane. Wings
of nearly elliptical plan with maximum chord and thickness at half
span with bracing wires to fuselage and floats. Wings of wooden
construction |
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Fuselage: |
Fuselage of circular
section is of wooden construction aft of cockpit and metal
construction forward |
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Tail Unit: |
Cantilever monoplane tail
attached to fuselage with single fin and rudder |
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Landing Gear: |
Twin single step floats of
metal construction |
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Power Plant: |
One 808 hp Bristol Mercury
I 9 cylinder, single row, air cooled radial engine in nose |
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Accommodation: |
Single seat for pilot in
open cockpit at wing trailing edge |
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Dimensions |
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Span: |
26 ft 6 in |
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Length: |
25 ft |
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Height: |
Unknown |
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Wing Area: |
120 sq ft |
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Weights |
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Empty: |
1,938 lb |
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All-up: |
2,712 lb |
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Performance |
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Max Speed: |
270 mph |
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