Airbus A319neo vs. Short C-23 Sherpa

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Airbus A319neo versus Short C-23 Sherpa
33.84 m 111 ft 0 in length 17.68 m 58 ft 0 in
11.76 m 38 ft 7 in height 6.55 m 21 ft 6 in
35.8 m 117 ft 5 in wingspan 22.76 m 74 ft 8 in
2 x PW 1100G or 2 x CFM LEAP-1A engines 2 x Pratt & Whitney Canada PT6A-45R turboprop engines
110kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine Approximately 1,200 hp per engine
220kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust Approximately 2,400 hp total
75,500 kg 166,400 lb MTOW 7,484 kg 16,500 lb
6,850 km 3,702 nm range 1,048 km 566 nm
530 mph 853 km/h cruise speed 425 km/h 264 mph
120-150 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.