Airbus A310-300 vs. Dornier 228

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Airbus A310-300 versus Dornier 228
46.66 m 153 ft 1 in length 16.56 m 54 ft 4 in
15.8 m 51 ft 10 in height 4.86 m 15 ft 11 in
43.9 m 144 ft wingspan 16.97 m 55 ft 8 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 x Garrett TPE331 turboprop engines
52,000 lb thrust per engine Approximately 776 kW per engine
104,000 lb total thrust Approximately 1,552 kW total
148,768 kg 328,000 lb MTOW 5,650 kg 12,456 lb
8,050 km 4,348 nm range 1,465 km 791 nm
482 knots 279 mph cruise speed 350 km/h 217 mph
190-230 passengers capacity Up to 19 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.