Airbus A320-200 vs. N. American T-28 Trojan

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Airbus A320-200 versus N. American T-28 Trojan
38.7 m 127 ft 0 in length 10.06 m 33 ft 0 in
17.4 m 57 ft 1 in height 3.86 m 12 ft 8 in
35.8 m 117 ft 5 in wingspan 12.22 m 40 ft 1 in
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 1 x Wright R-1820-86 Cyclone radial engine
Between 21,000 - 33,000 lbf thrust per engine Approximately 1,425 hp
Between 42,000 - 66,000 lbf total thrust Approximately 1,425 hp
77,000 kg 169,800 lb MTOW 8,500 lb 3,856 kg
5,700 km 3,078 nm range 1,705 km 921 nm
530 mph 853 km/h cruise speed 210 mph 338 km/h
Typically between 140-180 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.