Here ya go, I'll throw you out a bone...
Specification of the North American B-25D Mitchell:
Engines: Two Wright R-2600-13 Double Cyclone fourteen-cylinder air-cooled radials, each rated at 1700 hp each for takeoff, 1500 hp at 2400 rpm. Equipped with Holley 1685HA carburetors. Performance: Maximum speed 284 mph at 15,000 feet. Cruising speed 233 mph at 15,000 feet. Initial climb rate 1100 feet per minute. An altitude of 15,000 feet could be reached in 16.5 minutes. Service ceiling 24,000 feet, Range 1500 miles with 3000 pounds of bombs. Weights: 20,300 pounds empty, 34,000 pounds maximum loaded. Dimensions: wingspan 67 feet 67.7 inches, length 53 feet 0 inches, height 15 feet 9 inches, wing area 610 square feet. Fuel: The fuel capacity consisted of four tanks in the inner wing panels, with a total capacity of 670 US gallons. In addition, a 515-gallon tank could be installed in the bomb bay for ferrying purposes, bringing total fuel capacity to 1255 US gallons. Later versions had additional auxiliary fuel tanks in the outer wing panels. Later versions could also have 125-gallon tanks fitted in side waist positions, a 215-gallon self-sealing fuel tank installed in the bomb bay, and provisions could be made for a droppable 335-gallon metal bomb-bay fuel tank. Armament: Two 0.50-inch machine guns in dorsal turret. Two 0.50-inch machine guns in retractable ventral turret. One 0.30-inch machine gun in flexible mount in the nose. Starting with B-25D-5 the 0.30-inch nose gun was removed and replaced by a flexible 0.50-inch machine gun in the extreme nose and two fixed 0.50-inch machine mounted in the nose and firing through holes cut into the side of the Plexiglas glazing. Normal bomb load was 3000 pounds but could be increased on the B-25D-1-NA with external underwing racks to a maximum of 5200 pounds.
