Blackburn B-7 Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
28 November 1934 |
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Blackburn B-7: |
1 - Blackburn Aeroplane and Motor Co Ltd |
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Type Specification | |
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Applies to: |
Blackburn B-7 |
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Type: |
General purpose aeroplane to Specification G.4/31 |
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Wing: |
Biplane with unequal span and unequal chord wings. Metal structure with fabric covering. Ailerons on all four wings |
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Fuselage: |
All metal fuselage mounted on lower wing |
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Tail Unit: |
Braced tailplane at base of fin with fin and rudder |
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Landing Gear: |
Divided type fixed main gear and tailwheel |
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Power Plant: |
One 700 hp Armstrong Siddeley Tiger IV in nose |
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Accommodation: |
Two/three seats in tandem open cockpits |
Armament: |
Single forward firing gun and rear firing gun together with torpedo gear and bomb racks |
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Dimensions | |
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Span: |
46 ft |
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Length: |
35 ft 4.5 in |
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Height: |
12 ft 9 in |
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Wing Area: |
Unknown |
Weights | |
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All-up: |
8,338 lb |
Performance | |
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Speed: |
150 mph |
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Initial Climb: |
1,200 ft/min |
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Service Ceiling: |
20,000 ft |
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Range: |
540 miles |
Preserved in British Museums | |
None known | |
Web Sites | |
None known | |