![]() ![]() To report results of comparative speed tests on the B-26A airplane, A.C. manifold pressure or wide open when below:Ī. manifold presure or wide when below, high blower usdedĪbove 10,000 ft. Climb data, low blower used up to 10,000 ft. ![]() Cruising data in low blower ratio at 15,000 ft.:ġ0. The airplane will not meet Air Corps cooling requirements when leaned for maximum power.ĩ. Speed, wide open throttle with mixture controls set for maximum power at 14,250 ft., is 326 mph at 2400 rpm at 1480 bhp per engine. High speed, wide open throttles in high blower ratio, mixture controls automatic rich at 14,250 ft., is 323 mph at 2400 rpm at 1440 bhp per engine. Propellers equipped with cuffs, radio antenna in place, de-icer equipment not installed, airplane not camouflaged.ī. Landing gear retracted, wing flaps neutral, cowl flaps zero degrees, oil cooler flaps flush with cowling, carburetor cold, except where otherwise stated. Gross weight normal military load 26,734 lbs., c.g. Report on flight tests of Martin Medium Bomber (B-26) airplane equipped with two (2) Pratt-Whitney R-2800-5 engines and four-bladed constant speed propellers, blade design No.
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