Blackburn Airedale Aircraft
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Production Details | |
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Design Company: |
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First Flight: |
October 1925 |
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Airedale: |
2 - Blackburn |
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Type Specification | |
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Applies to: |
Blackburn R.2 Airedale |
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Type: |
Deck-landing reconnaissance monoplane to Air Ministry Specification 37/22 |
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Wing: |
Parasol monoplane with unswept, thick section wings. Wooden structure with fabric covering |
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Fuselage: |
Semi-monocoque fuselage of wooden structure with fabric covering |
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Tail Unit: |
Braced tailplane at top of fuselage with sigle fin and rudder |
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Landing Gear: |
Crossaxle type main gear fixed to fuselage lower longeron by radius rod and oleo. Tail skid |
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Power Plant: |
One 385 hp Armstrong Siddeley Jaguar III air cooled radial engine in the nose |
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Accommodation: |
Crew of three. Pilot in open cockpit ahead of wing with cabin for navigator. Behing wing was gunners position |
Armament: |
Fixed forward firing Vickers, a Lewis gun on a Scarff ring for gunner and bombs on racks under fuselage |
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Dimensions | |
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Span: |
46 ft |
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Length: |
36 ft 4 in |
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Height: |
14 ft 3 in |
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Wing Area: |
Unknown |
Weights | |
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All-up: |
4,942 lb |
Performance | |
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Max Speed: |
120 mph at sea level |
Preserved in British Museums | |
None known | |
Web Sites | |
None known | |