Airbus A321XLR vs. Antonov An-124 Ruslan

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Airbus A321XLR versus Antonov An-124 Ruslan
44.51 m 146 ft 0 in length 69.10 m 226 ft 9 in
11.76 m 38 ft 7 in height 20.78 m 68 ft 2 in
35.8 m 117 ft 5 in wingspan 73.3 m 240 ft 6 in
CFM LEAP-1A and P&W PW1100G engines 4 x Ivchenko Progress D-18T turbofan engines
33,000 lbs (147 kN) thrust per engine Approximately 51,590 lbf
66,000 lbs (294 kN) total thrust Approximately 206,360 lbf
101,000 kg 222,700 lb MTOW 405,000 kg 893,000 lb
4,700 nmi 8,704 km range 3,700 km 1,998 nm
963km/h 598mph cruise speed 800 km/h 497 mph
180-220 seats (typical 2-class seating) capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.