Airbus A321XLR vs. North American T-6 Texan

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Airbus A321XLR versus North American T-6 Texan
44.51 m 146 ft 0 in length 9.0 m 29 ft 6 in
11.76 m 38 ft 7 in height 3.56 m 11 ft 8 in
35.8 m 117 ft 5 in wingspan 12.8 m 42 ft
CFM LEAP-1A and P&W PW1100G engines 1 x Pratt & Whitney R-1340-AN-1 radial engine
33,000 lbs (147 kN) thrust per engine Approximately 600 hp
66,000 lbs (294 kN) total thrust Approximately 600 hp
101,000 kg 222,700 lb MTOW 5,617 lb 2,548 kg
4,700 nmi 8,704 km range 1,175 km 634 nm
963km/h 598mph cruise speed 145 mph 233 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.