Airbus A320-200 vs. North American T-6 Texan

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Airbus A320-200 versus North American T-6 Texan
38.7 m 127 ft 0 in length 9.0 m 29 ft 6 in
17.4 m 57 ft 1 in height 3.56 m 11 ft 8 in
35.8 m 117 ft 5 in wingspan 12.8 m 42 ft
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 1 x Pratt & Whitney R-1340-AN-1 radial engine
Between 21,000 - 33,000 lbf thrust per engine Approximately 600 hp
Between 42,000 - 66,000 lbf total thrust Approximately 600 hp
77,000 kg 169,800 lb MTOW 5,617 lb 2,548 kg
5,700 km 3,078 nm range 1,175 km 634 nm
530 mph 853 km/h cruise speed 145 mph 233 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.