Lockheed Martin C-130J Super Hercules vs. Bell 206

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Lockheed Martin C-130J Super Hercules versus Bell 206
34.37 m 112 ft 9 in length 12.11 m 39 ft 9 in
11.86 m 38 ft 11 in height 2.88 m 9 ft 5 in
40.41 m 132 ft 7 in wingspan
4 x Rolls-Royce AE 2100D3 turboprop engines engines 1 × Allison 250-C20B
Approximately 4,700 hp per engine thrust per engine 420 shp (313 kW)
Approximately 18,800 hp total total thrust 420 shp (313 kW)
76,610 kg 168,900 lb MTOW 1,451 kg 3,199 lb
4,600 km 2,485 nm range 374 km 202 nm
660 km/h 410 mph cruise speed 222 km/h 138 mph
based on configuration 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.