Airbus A310-300 vs. Nanchang CJ-6

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Airbus A310-300 versus Nanchang CJ-6
46.66 m 153 ft 1 in length 8.48 m 27 ft 10 in
15.8 m 51 ft 10 in height 2.67 m 8 ft 9 in
43.9 m 144 ft wingspan 10.49 m 34 ft 5 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 x Ivchenko AI-14RA radial engine
52,000 lb thrust per engine Approximately 260 hp
104,000 lb total thrust Approximately 260 hp
148,768 kg 328,000 lb MTOW 3,858 lb 1,751 kg
8,050 km 4,348 nm range 800 km 432 nm
482 knots 279 mph cruise speed 155 mph 249 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.