Airbus A320neo vs. Short C-23 Sherpa

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Airbus A320neo versus Short C-23 Sherpa
37.57 m 123 ft 3 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
120kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine Approximately 1,200 hp per engine
240kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust Approximately 2,400 hp total
79,000 kg 174,200 lb MTOW 7,484 kg 16,500 lb
6,300 km 3,403 nm range 1,048 km 566 nm
M0.82 101,3 km/h cruise speed 425 km/h 264 mph
150-180 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.