Airbus A321-200 vs. N. American T-28 Trojan

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Airbus A321-200 versus N. American T-28 Trojan
44.51 m 146 ft 0 in length 10.06 m 33 ft 0 in
11.76 m 38 ft 7 in height 3.86 m 12 ft 8 in
35.8 m 117 ft 5 in wingspan 12.22 m 40 ft 1 in
2 GE CFM56-5B3 engines 1 x Wright R-1820-86 Cyclone radial engine
31,600 lbs thrust per engine Approximately 1,425 hp
63,200 lbs total thrust Approximately 1,425 hp
89,000 kg 196,200 lb MTOW 8,500 lb 3,856 kg
4,000 nmi 7,408 km range 1,705 km 921 nm
871 km/h 541 mph cruise speed 210 mph 338 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.