This Military Service Page was created/owned by
SSgt Robert Bruce McClelland, Jr.
to remember
Johnson, Russell David ("The Professor"), 1st Lt.
If you knew or served with this Airman and have additional information or photos to support this Page, please leave a message for the Page Administrator(s) HERE.
Aircraft/Missile Information
Model North American B-25C Mitchell Length 52.92 ft | 16.13 m Width 67.55 ft | 20.59 m Height 15.75 ft | 4.80 m Engine(s) 2 x Wright Cyclone R-2600-19 air-cooled piston engines delivering 1,700hp each. Empty Weight 20,300 lbs | 9,208 kg MTOW 34,000 lbs | 15,422 kg Max Speed 272 mph | 438 km/h | 237 kts Max Range 1,350 miles | 2,173 km Ceiling 24,196 ft | 7,375 m | 4.6 miles Climb Rate 1,666 ft/min (507.796 m/min) Hardpoints Up to 8 (model dependent) Armament Model-specific armament included:
8 x 12.7mm machine gun array OR 1 x 75mm cannon in forward-fixed nose assembly.
2 x 12.7mm machine guns in forward-fixed lower-left side fuselage position (beneath and behind cockpit position). 2 x 12.7mm machine gun in forward-fixed lower-right side fuselage position (beneath and behind cockpit position). 2 x 12.7mm machine guns in ventral turret (powered turrets in some models). 2 x 12.7mm machine guns in dorsal turret (powered turrets in some models). 1 x 12.7mm machine gun in left waist port position. 1 x 12.7mm machine gun in right waist port position. 2 x 12.7mm machine guns in tail gun position (some models removed). 1 x Torpedo in under-fuselage arrangement (model-specific fitting). 8 x 250lb bombs on 8 external hardpoints (model-specific fitting).
Maximum internal bombload of 3,000lbs (1,361 kg). Accommodations 5 Operators the United States of America
