Lockheed Martin C-130J Super Hercules vs. AgustaWestland AW109

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Lockheed Martin C-130J Super Hercules versus AgustaWestland AW109
34.37 m 112 ft 9 in length 13,04 m 42 ft 9 in
11.86 m 38 ft 11 in height 3,40 m 11 ft 2 in
40.41 m 132 ft 7 in wingspan
4 x Rolls-Royce AE 2100D3 turboprop engines engines 2 × Pratt & Whitney Canada PW206C or 2 × Pratt & Whitney Canada PW207C
Approximately 4,700 hp per engine thrust per engine 638 shp (476 kW)
Approximately 18,800 hp total total thrust 1276 shp (952 kW)
76,610 kg 168,900 lb MTOW 3,175 kg 7,000 lb
4,600 km 2,485 nm range 932 km 503 nm
660 km/h 410 mph cruise speed 285 km/h 177 mph
based on configuration capacity 1 or 2 pilots + up to 7 passengers
rotor diameter 11.00 m 36 ft 1 in
rate of climb 651 m/min 2,136 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.