North American B-25 Mitchell vs. Bell 412

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North American B-25 Mitchell versus Bell 412
16.15 m 53 ft 0 in length 17,10 m 56 ft 1 in
5 m 16 ft 4 in height 3,48 m 11 ft 5 in
20.58 m 67 ft 6 in wingspan
2 x Wright R-2600-92 Twin Cyclone engines 2 x Pratt & Whitney Canada PT6T-3D turboshaft engines
1,700 horsepower thrust per engine 1,800 hp
3,400 horsepower total thrust 3,600 hp
7,484 kg 16,500 lb MTOW 5,400 kg 11,905 lb
1,350 mi 1,175 nm range 659 km 356 nm
233 MPH 375 km/h cruise speed 259 km/h 161 mph
capacity 13
rotor diameter 14.0 m 45 ft 11 in
rate of climb 9.5 m/s 1,870 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.