North American B-25 Mitchell (1941)
| Specifications | |
|---|---|
| Crew | 5 (pilot, navigator/bombardier, turret gunner/engineer, radio operator/waist gunner, tail gunner) |
| Engine | 2 × Wright R-2600-92 Twin Cyclone |
| Length | 16.13 m / 53 ft 11 in |
| Wingspan | 20.6 m / 68 ft 7 in |
| Height | 4.98 m / 16 ft 4 in |
| Wing Area | 56.67 m² / 609.99 sq ft |
| Empty Weight | 8836 kg / 19480 lb |
| Take-off Weight | 15876 kg / 35001 lb |
| Maximum Speed | 438 km/h / 272 mph |
| Range | 2173 km / 1350 mi |
| Ceiling | 7375 m / 24200 ft |
| Armament | 12 × 12.7 mm (0.50 in) M2 Browning machine guns, 1361 kg (3000 lb) of bombs |