Some more info on B25H found at
http://pages.prodigy.com/jing_bao/b25h.htmVery similar to the site that Smut found, in fact looks word for word the same.
Specification of the North American B-25H Mitchell:
Two Wright R-2600-13 Double Cyclone fourteen-cylinder air-cooled radials, rated at 1700 hp each for takeoff and 1500 hp at 2400 rpm. Equipped with Holley 1685HA carburetors.
Performance: Maximum speed 275 mph at 13,000 feet, 230 mph cruising speed. An altitude of 15,000 feet could be reached in 19 minutes. Service ceiling 23,800 feet. Range 1350 miles with 3000 pounds of bombs.
Weights: 19,600 pounds empty, 35,000 pounds maximum loaded.
Fuel: The fuel capacity consisted of four tanks in the inner wing panels, with a total capacity of 670 US gallons. In addition, 304 US gallons of fuel could be carried in auxiliary tanks in the outboard wing panels, for a normal total fuel load of 974 US gallons. A 515-gallon tank could be installed in the bomb bay for ferrying purposes, 125 gallons of fuel could be carried 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: One 75-mm T13E1 cannon in nose with 21 rounds. Four 0.50-inch machine guns in the nose with 400 rpg.
Two 0.50-inch machine guns in individual blisters on the right hand side of the fuselage with 400 rpg.
Beginning with B-25H-5 No. 43-4405, two 0.50-inch machine guns were added in blisters on the left hand side of the forward fuselage.
Two 0.50-inch machine guns in top turret, 400 rpg.
Two 0.50-inch machine guns in waist position, 200 rpg.
Two 0.50-inch machine guns in tail turret, 600 rpg.
Normal internal bomb load was 3000 pounds.