lockheed C-130 hercules vs. Bell 206

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lockheed C-130 hercules versus Bell 206
29.79 m 97 ft 9 in length 12.11 m 39 ft 9 in
11.66 m 38 ft 3 in height 2.88 m 9 ft 5 in
40.41 m 132 ft 7 in wingspan
4 x Allison T56-A-15 turboprop engines engines 1 × Allison 250-C20B
Approximately 4,590 hp per engine thrust per engine 420 shp (313 kW)
Approximately 18,360 hp total total thrust 420 shp (313 kW)
70,307 kg 155,000 lb MTOW 1,451 kg 3,199 lb
3,760 km 2,031 nm range 374 km 202 nm
540 km/h 335 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.