Britten-Norman BN-1 Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
26 May 1951 |
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BN-1: |
1 - John Britten and Desmond Norman, Bembridge |
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Type Specification | |
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Applies to: |
Britten-Norman BN-1F |
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Type: |
Single-seat light aircraft |
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Wing: |
Parasol monoplane. Wing is untapered, unswept. Attached to fuselage by struts |
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Fuselage: |
Fuselage beneath wing |
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Tail Unit: |
Braced tailplane with single fin and rudder |
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Landing Gear: |
Divided type undercarriage with tail skid |
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Power Plant: |
One 55 hp Lycoming flat-four engine mounted in the nose driving a two blade propeller |
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Accommodation: |
Single seat for pilot in open cockpit aft of wing |
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Dimensions | |
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Span: |
23 ft 0 in |
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Length: |
16 ft 7 in |
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Height: |
Unknown |
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Wing Area: |
Unknown |
Weights | |
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Tare: |
208 lb |
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All-up: |
630 lb |
Performance | |
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Max Speed: |
84 mph |
Preserved in British Museums | |
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BN-1F: |
G-ALZE - - Solent Sky, Southampton - Display |
Web Sites | |
None known | |