Airbus A330-200 vs. McDonnell-Douglas DC-9-30

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Airbus A330-200 versus McDonnell-Douglas DC-9-30
58.82 m 193 ft 0 in length 36.36 m 119 ft 3 in
17.39 m 57 ft 1 in height 8.5 m 27 ft 11 in
64 m 210 ft wingspan 28.44 m 93 ft 4 in
2 Turbofans engines 2x Pratt & Whitney JT8D
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 15,000 pound-force
Depends on the engine variant total thrust 30,000 pound-force (2 engines)
251,000 kg 553,400 lb MTOW 54,885 kg 121,000 lb
15,094 km 8,150 nm range 2,632 km 1,422 nm
531 mph 855 km/h cruise speed 898 km/h 558 mph
220-260 capacity Up to 139 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.