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| General characteristics B-25J | |||
| Primary function | Medium bomber | ||
| Contractor | North American Aviation Inc. | ||
| Power plant | Two Wright R-2600-29 Cyclone 14-cylinder radials engines | ||
| Thrust | 2x 1,850 HP | 2x 1,380 kW | |
| Wingspan | 67.6 ft | 20.60 m | |
| Length | 52.9 ft | 16.13 m | |
| Height | 16.3 ft | 4.98 m | |
| Wingarea | 610 sq ft | 56.67 sq m | |
| Weight | empty | 21,120 lb | 9,580 kg |
| max. | 34,955 lb | 15,855 kg | |
| Speed | 275 mph | 443 km/h | |
| Initial climb rate | 1,109 ft/min | 338 m/min | |
| Ceiling | 24,200 ft | 7,375 m | |
| Range | 1,350 miles | 2,170 km | |
| Armament | 13x 12.7mm machine gun; 1,800 kg bombs | ||
| Crew | Six | ||
| First flight | January 1939 | ||
| Date deployed | 1943 | ||
| Cost | $96,000 (B-25B) | ||
| Number built | 11,433 | ||
Jirka Wagner
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