Airbus A350-900ULR vs. North American T-6 Texan

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Airbus A350-900ULR versus North American T-6 Texan
66.80 m 219 ft 2 in length 9.0 m 29 ft 6 in
17.05 m 55 ft 11 in height 3.56 m 11 ft 8 in
64.75 m 212 ft 5 in wingspan 12.8 m 42 ft
2 Rolls-Royce Trent XWB engines 1 x Pratt & Whitney R-1340-AN-1 radial engine
84,000 lbs thrust per engine Approximately 600 hp
168,000 lbs total thrust Approximately 600 hp
280,000 kg 617,300 lb MTOW 5,617 lb 2,548 kg
17,964 km 9,700 nm range 1,175 km 634 nm
552 mph 888 km/h cruise speed 145 mph 233 km/h
300-350 passengers in three classes 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.