Boeing 767-300ER vs. Lockheed Martin C-130J Super Hercules

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Boeing 767-300ER versus Lockheed Martin C-130J Super Hercules
54.9 m 180 ft 3 in length 34.37 m 112 ft 9 in
15.85 m 52 ft height 11.86 m 38 ft 11 in
47.57 m 156 ft 1 in wingspan 40.41 m 132 ft 7 in
Two Pratt & Whitney PW4060 turbofan engines engines 4 x Rolls-Royce AE 2100D3 turboprop engines
Up to 63,300 pounds of thrust each thrust per engine Approximately 4,700 hp per engine
Up to 126,600 pounds of thrust total thrust Approximately 18,800 hp total
186,880 kg 412,000 lb MTOW 76,610 kg 168,900 lb
11,070 km 5,980 nm range 4,600 km 2,485 nm
528 MPH 850 km/h cruise speed 660 km/h 410 mph
Typically 218 (3-class) 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.