Airbus A321LR vs. North American T-6 Texan

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Airbus A321LR 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 International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 1 x Pratt & Whitney R-1340-AN-1 radial engine
Over 33,000 lbs (147 kN) thrust per engine Approximately 600 hp
66,000 lbs (294 kN) total thrust Approximately 600 hp
97,000 kg 213,800 lb MTOW 5,617 lb 2,548 kg
7,400 km 4,000 nm range 1,175 km 634 nm
832 km/h 517 mph cruise speed 145 mph 233 km/h
180-220 passengers 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.