Airbus A310-300 vs. N. American T-28 Trojan

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Airbus A310-300 versus N. American T-28 Trojan
46.66 m 153 ft 1 in length 10.06 m 33 ft 0 in
15.8 m 51 ft 10 in height 3.86 m 12 ft 8 in
43.9 m 144 ft wingspan 12.22 m 40 ft 1 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 x Wright R-1820-86 Cyclone radial engine
52,000 lb thrust per engine Approximately 1,425 hp
104,000 lb total thrust Approximately 1,425 hp
148,768 kg 328,000 lb MTOW 8,500 lb 3,856 kg
8,050 km 4,348 nm range 1,705 km 921 nm
482 knots 279 mph cruise speed 210 mph 338 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.