Airbus A330-200 vs. North American T-6 Texan

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Airbus A330-200 versus North American T-6 Texan
58.82 m 193 ft 0 in length 9.0 m 29 ft 6 in
17.39 m 57 ft 1 in height 3.56 m 11 ft 8 in
64 m 210 ft wingspan 12.8 m 42 ft
2 Turbofans engines 1 x Pratt & Whitney R-1340-AN-1 radial engine
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf thrust per engine Approximately 600 hp
Depends on the engine variant total thrust Approximately 600 hp
251,000 kg 553,400 lb MTOW 5,617 lb 2,548 kg
15,094 km 8,150 nm range 1,175 km 634 nm
531 mph 855 km/h cruise speed 145 mph 233 km/h
220-260 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.