Blackburn B-54 Aircraft
B-54 | |
Production Details | |
|
Design Company: |
|
|
First Flight: |
20 September 1949 |
|
B-54: |
2 - Blackburn and General Aircraft Ltd |
|
B-88: |
1 - Blackburn and General Aircraft Ltd |
|
Type Specification | |
|
Applies to: |
Blackburn B-54 |
|
Type: |
Carrier-borne, anti-submarine aircraft |
|
Wing: |
Low wing cantilever, inverted gull wing monoplane of all metal construction. |
|
Fuselage: |
All metal, semi-monocoque construction |
|
Tail Unit: |
Cantilever tailplane mounted at base of fin with dihedral. Single rudder |
|
Landing Gear: |
Retractable tricycle undercarriage. Each unit has a single wheel, nose gear retacts rearwards into fusleage. Main gear retracts inward into wing |
|
Power Plant: |
One 2,000 hp Rolls-Royce Griffon 56 engine in nose driving contra-rotating three bladed propellers |
|
Accommodation: |
Crew of three seated inline in enclosed cockpits |
Armament: |
Large enclosed bomb bay under wing |
|
Dimensions | |
|
Span: |
44 ft 2 in |
|
Length: |
42 ft 5 in |
|
Height: |
17 ft 3 in |
|
Wing Area: |
Unknown |
Weights | |
|
All-up: |
13,729 lb |
Performance | |
|
Max Speed: |
251 mph |
Preserved in British Museums | |
None known | |
Web Sites | |