Airbus A330-200 vs. Nanchang CJ-6

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Airbus A330-200 versus Nanchang CJ-6
58.82 m 193 ft 0 in length 8.48 m 27 ft 10 in
17.39 m 57 ft 1 in height 2.67 m 8 ft 9 in
64 m 210 ft wingspan 10.49 m 34 ft 5 in
2 Turbofans engines 1 x Ivchenko AI-14RA 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 260 hp
Depends on the engine variant total thrust Approximately 260 hp
251,000 kg 553,400 lb MTOW 3,858 lb 1,751 kg
15,094 km 8,150 nm range 800 km 432 nm
531 mph 855 km/h cruise speed 155 mph 249 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.