Antonov An-124 Ruslan vs. Beechcraft T-6 Texan II

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Antonov An-124 Ruslan versus Beechcraft T-6 Texan II
69.10 m 226 ft 9 in length 10.18 m 33 ft 4 in
20.78 m 68 ft 2 in height 3.29 m 10 ft 10 in
73.3 m 240 ft 6 in wingspan 10.21 m 33 ft 6 in
4 x Ivchenko Progress D-18T turbofan engines engines 1 x Pratt & Whitney Canada PT6A-68
Approximately 51,590 lbf thrust per engine 1100 lbs
Approximately 206,360 lbf total thrust 1100 lbs
405,000 kg 893,000 lb MTOW 6,250 lb 2,835 kg
3,700 km 1,998 nm range 900 nm 1,667 km
800 km/h 497 mph cruise speed 320 kts 199 mph
capacity 2
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.