Airbus A330-200 vs. Douglas DC-8-61

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Airbus A330-200 versus Douglas DC-8-61
58.82 m 193 ft 0 in length 57.0 m 187 ft 0 in
17.39 m 57 ft 1 in height 13.1 m 43 ft
64 m 210 ft wingspan 45.24 m 148 ft 5 in
2 Turbofans engines 4x P&W JT3D-3B 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 18,000 pound-force
Depends on the engine variant total thrust 72,000 pound-force
251,000 kg 553,400 lb MTOW 147,400 kg 325,000 lb
15,094 km 8,150 nm range 3,200 nm 5,926 km
531 mph 855 km/h cruise speed 483 knots 282 mph
220-260 capacity 180 to 220 passengers in a mixed-class seating
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.