Airbus A310-300 vs. Short C-23 Sherpa

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Airbus A310-300 versus Short C-23 Sherpa
46.66 m 153 ft 1 in length 17.68 m 58 ft 0 in
15.8 m 51 ft 10 in height 6.55 m 21 ft 6 in
43.9 m 144 ft wingspan 22.76 m 74 ft 8 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 x Pratt & Whitney Canada PT6A-45R turboprop engines
52,000 lb thrust per engine Approximately 1,200 hp per engine
104,000 lb total thrust Approximately 2,400 hp total
148,768 kg 328,000 lb MTOW 7,484 kg 16,500 lb
8,050 km 4,348 nm range 1,048 km 566 nm
482 knots 279 mph cruise speed 425 km/h 264 mph
190-230 passengers capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.