Airbus A310-300 vs. McDonnell-Douglas DC-10-30

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Airbus A310-300 versus McDonnell-Douglas DC-10-30
46.66 m 153 ft 1 in length 55.35 m 181 ft 8 in
15.8 m 51 ft 10 in height 17.8 m 58 ft 5 in
43.9 m 144 ft wingspan 50.39 m 165 ft 4 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 3x GE CF6-50C Turbofan
52,000 lb thrust per engine 54,000 lbf
104,000 lb total thrust 162,000 lbf
148,768 kg 328,000 lb MTOW 251,744 kg 555,000 lb
8,050 km 4,348 nm range 9,630 km 5,200 nm
482 knots 279 mph cruise speed 507 knots 939 km/h
190-230 passengers 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.