Airbus A321LR vs. N. American T-28 Trojan

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Airbus A321LR 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
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 1 x Wright R-1820-86 Cyclone radial engine
Over 33,000 lbs (147 kN) thrust per engine Approximately 1,425 hp
66,000 lbs (294 kN) total thrust Approximately 1,425 hp
97,000 kg 213,800 lb MTOW 8,500 lb 3,856 kg
7,400 km 4,000 nm range 1,705 km 921 nm
832 km/h 517 mph cruise speed 210 mph 338 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.