Boeing 767-200ER vs. Lockheed Martin C-130J Super Hercules

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Boeing 767-200ER versus Lockheed Martin C-130J Super Hercules
48.5 m 159 ft 2 in length 34.37 m 112 ft 9 in
16.1 m 52 ft 10 in height 11.86 m 38 ft 11 in
47.8 m 156 ft 9 in wingspan 40.41 m 132 ft 7 in
2 x GE CF6-80C2B4F engines 4 x Rolls-Royce AE 2100D3 turboprop engines
62,020 lbs thrust per engine Approximately 4,700 hp per engine
124,040 lbs total thrust Approximately 18,800 hp total
164,200 kg 362,000 lb MTOW 76,610 kg 168,900 lb
12,200 km 6,587 nmi range 4,600 km 2,485 nm
850 km/hour 528 mph cruise speed 660 km/h 410 mph
249 capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.