Airbus A310-300 vs. North American T-6 Texan

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Airbus A310-300 versus North American T-6 Texan
46.66 m 153 ft 1 in length 9.0 m 29 ft 6 in
15.8 m 51 ft 10 in height 3.56 m 11 ft 8 in
43.9 m 144 ft wingspan 12.8 m 42 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 x Pratt & Whitney R-1340-AN-1 radial engine
52,000 lb thrust per engine Approximately 600 hp
104,000 lb total thrust Approximately 600 hp
148,768 kg 328,000 lb MTOW 5,617 lb 2,548 kg
8,050 km 4,348 nm range 1,175 km 634 nm
482 knots 279 mph cruise speed 145 mph 233 km/h
190-230 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.