Airbus A320neo vs. North American T-6 Texan

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Airbus A320neo versus North American T-6 Texan
37.57 m 123 ft 3 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 x PW 1100G or 2 x CFM LEAP-1A engines 1 x Pratt & Whitney R-1340-AN-1 radial engine
120kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine Approximately 600 hp
240kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust Approximately 600 hp
79,000 kg 174,200 lb MTOW 5,617 lb 2,548 kg
6,300 km 3,403 nm range 1,175 km 634 nm
M0.82 101,3 km/h cruise speed 145 mph 233 km/h
150-180 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.