North American B-25 Mitchell vs. Bell 206

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North American B-25 Mitchell versus Bell 206
16.15 m 53 ft 0 in length 12.11 m 39 ft 9 in
5 m 16 ft 4 in height 2.88 m 9 ft 5 in
20.58 m 67 ft 6 in wingspan
2 x Wright R-2600-92 Twin Cyclone engines 1 × Allison 250-C20B
1,700 horsepower thrust per engine 420 shp (313 kW)
3,400 horsepower total thrust 420 shp (313 kW)
7,484 kg 16,500 lb MTOW 1,451 kg 3,199 lb
1,350 mi 1,175 nm range 374 km 202 nm
233 MPH 375 km/h cruise speed 222 km/h 138 mph
capacity 1 pilot + 4 passengers
rotor diameter 11.00 m 36 ft 1 in
rate of climb 425 m/min 1,395 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.