Airbus A330-200 vs. Short C-23 Sherpa

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Airbus A330-200 versus Short C-23 Sherpa
58.82 m 193 ft 0 in length 17.68 m 58 ft 0 in
17.39 m 57 ft 1 in height 6.55 m 21 ft 6 in
64 m 210 ft wingspan 22.76 m 74 ft 8 in
2 Turbofans engines 2 x Pratt & Whitney Canada PT6A-45R turboprop engines
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 Approximately 1,200 hp per engine
Depends on the engine variant total thrust Approximately 2,400 hp total
251,000 kg 553,400 lb MTOW 7,484 kg 16,500 lb
15,094 km 8,150 nm range 1,048 km 566 nm
531 mph 855 km/h cruise speed 425 km/h 264 mph
220-260 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.