Airbus A320-200 vs. Short C-23 Sherpa

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Airbus A320-200 versus Short C-23 Sherpa
38.7 m 127 ft 0 in length 17.68 m 58 ft 0 in
17.4 m 57 ft 1 in height 6.55 m 21 ft 6 in
35.8 m 117 ft 5 in wingspan 22.76 m 74 ft 8 in
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 2 x Pratt & Whitney Canada PT6A-45R turboprop engines
Between 21,000 - 33,000 lbf thrust per engine Approximately 1,200 hp per engine
Between 42,000 - 66,000 lbf total thrust Approximately 2,400 hp total
77,000 kg 169,800 lb MTOW 7,484 kg 16,500 lb
5,700 km 3,078 nm range 1,048 km 566 nm
530 mph 853 km/h cruise speed 425 km/h 264 mph
Typically between 140-180 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.