Antonov An-124 Ruslan vs. AgustaWestland AW109

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Antonov An-124 Ruslan versus AgustaWestland AW109
69.10 m 226 ft 9 in length 13,04 m 42 ft 9 in
20.78 m 68 ft 2 in height 3,40 m 11 ft 2 in
73.3 m 240 ft 6 in wingspan
4 x Ivchenko Progress D-18T turbofan engines engines 2 × Pratt & Whitney Canada PW206C or 2 × Pratt & Whitney Canada PW207C
Approximately 51,590 lbf thrust per engine 638 shp (476 kW)
Approximately 206,360 lbf total thrust 1276 shp (952 kW)
405,000 kg 893,000 lb MTOW 3,175 kg 7,000 lb
3,700 km 1,998 nm range 932 km 503 nm
800 km/h 497 mph cruise speed 285 km/h 177 mph
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.