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U. S. Military Aircraft

LB-6

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The Keystone light bomber had their origins in the Huff-Daland XLB-1 prototype that was bought by the US. Army in 1923 and evaluated with an 800-hp Packard 1A-2540 engine. The followed 10 LB-1 production bomber with the improved 2A-2540 engine. Next came the prototype with two 240-hp liberty V-1410 inlines on the lower wings to allow the relocation of the bombardier to the optimum nose position, this machine was reneged with 410-hp Pratt & Whitney R-1340-1 radials as the XLB-3A. However the XLB-5 prototype reverted to Liberty engines, and the 10 LB-5 bomber had the same power plant. Jest before this Huff-Galand had become Keystone, and the 25 L-5A bombers with a revised tail unit were Keystone rather than Huff-Daland aircraft. The XLB-6 prototype of 1927 introduced new wings and two 525-hp Wright R-1750-1 radials, and was followed by 17 LB-6 bombers. The 18 LB-7s were identical apart from their different engines, and two of these were evaluated as an LB-8 and LB-9 with 550-hp Pratt & Whitney R-1860-3 and 575-hp Wright GR-1750 radials respectively.

 

 

TECHNICAL DATA

Description Specifications
Manufacturer: Keystone Length: 43 ft. 5 in.
First Flight: Height: 18 ft. 1 in.
Model: LB-6 Wing Span: 75 ft. 0 in.
Crew: Five Wing Area: 1,148.0 sq. ft.
Nickname:  Empty Weight: 6,836 lb.
Basic Role: Light Bomber Max. Weight: 13,440 lb.
Other Versions: LB-1 with one packard 2A-2540 inline. LB-5 with two liberty V-1410 inlines. LB-6 with two Wright R-1750 radials. LB-7 with Pratt & Whitney R-1690-3 radials. Armament: Five 0.303-in 7.7-mm machine guns, and up to 2,000 lb. of bombs.
Principal User: USA.

Propulsion

Performance

Power Plant: Wright R-1750-1 radial piston engines.
Range: 632 miles. Horsepower: 536-hp.
Max. Speed: 114 mph. No. Of Engines: Two  
Ceiling: 11,650 ft.  
Climb Rate: 500 ft. per minute.  

 

 

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