Central Centaur IV Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
1919 |
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Centaur IV: |
8 - The Central Aircraft Company, Kilburn |
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Type Specification | |
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Applies to: |
Central Centaur IVA |
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Type: |
Joyriding and instructional aircraft |
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Wing: |
Two bay biplane with equal span, unstaggered, unswept wings. Ailerons on all four wings |
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Fuselage: |
Rectangular section fuselage with faired top mounted on lower wing |
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Tail Unit: |
Braced tailplane with elevator at base of fin together with single fin and balanced rudder |
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Landing Gear: |
Fixed gear of cross axle type under lower wing with fixed tailskid |
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Power Plant: |
One 70 hp Renault engine mounted in nose driving a four blade propeller |
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Accommodation: |
Seats for three in open cockpit between wings |
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Dimensions | |
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Span: |
34 ft 2.5 in |
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Length: |
27 ft 6 in |
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Height: |
Unknown |
Weights | |
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Tare: |
1,096 lb |
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All-up: |
1,600 lb |
Performance | |
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Max Speed: |
70 mph |
Preserved in British Museums | |
None known | |
Web Sites | |
None known | |