Airbus A310-300 vs. McDonnell-Douglas DC-9-30

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Airbus A310-300 versus McDonnell-Douglas DC-9-30
46.66 m 153 ft 1 in length 36.36 m 119 ft 3 in
15.8 m 51 ft 10 in height 8.5 m 27 ft 11 in
43.9 m 144 ft wingspan 28.44 m 93 ft 4 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2x Pratt & Whitney JT8D
52,000 lb thrust per engine 15,000 pound-force
104,000 lb total thrust 30,000 pound-force (2 engines)
148,768 kg 328,000 lb MTOW 54,885 kg 121,000 lb
8,050 km 4,348 nm range 2,632 km 1,422 nm
482 knots 279 mph cruise speed 898 km/h 558 mph
190-230 passengers 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.