Airbus A321XLR vs. Nanchang CJ-6

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Airbus A321XLR versus Nanchang CJ-6
44.51 m 146 ft 0 in length 8.48 m 27 ft 10 in
11.76 m 38 ft 7 in height 2.67 m 8 ft 9 in
35.8 m 117 ft 5 in wingspan 10.49 m 34 ft 5 in
CFM LEAP-1A and P&W PW1100G engines 1 x Ivchenko AI-14RA radial engine
33,000 lbs (147 kN) thrust per engine Approximately 260 hp
66,000 lbs (294 kN) total thrust Approximately 260 hp
101,000 kg 222,700 lb MTOW 3,858 lb 1,751 kg
4,700 nmi 8,704 km range 800 km 432 nm
963km/h 598mph cruise speed 155 mph 249 km/h
180-220 seats (typical 2-class seating) capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.