Airbus A321-200 vs. North American T-6 Texan

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Airbus A321-200 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
2 GE CFM56-5B3 engines 1 x Pratt & Whitney R-1340-AN-1 radial engine
31,600 lbs thrust per engine Approximately 600 hp
63,200 lbs total thrust Approximately 600 hp
89,000 kg 196,200 lb MTOW 5,617 lb 2,548 kg
4,000 nmi 7,408 km range 1,175 km 634 nm
871 km/h 541 mph cruise speed 145 mph 233 km/h
185 to 220 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.