Airbus A330-200 vs. McDonnell-Douglas DC-10-30

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Airbus A330-200 versus McDonnell-Douglas DC-10-30
58.82 m 193 ft 0 in length 55.35 m 181 ft 8 in
17.39 m 57 ft 1 in height 17.8 m 58 ft 5 in
64 m 210 ft wingspan 50.39 m 165 ft 4 in
2 Turbofans engines 3x GE CF6-50C Turbofan
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 54,000 lbf
Depends on the engine variant total thrust 162,000 lbf
251,000 kg 553,400 lb MTOW 251,744 kg 555,000 lb
15,094 km 8,150 nm range 9,630 km 5,200 nm
531 mph 855 km/h cruise speed 507 knots 939 km/h
220-260 capacity Up to 380 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.