Airbus A321-200 vs. Short C-23 Sherpa

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Airbus A321-200 versus Short C-23 Sherpa
44.51 m 146 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 GE CFM56-5B3 engines 2 x Pratt & Whitney Canada PT6A-45R turboprop engines
31,600 lbs thrust per engine Approximately 1,200 hp per engine
63,200 lbs total thrust Approximately 2,400 hp total
89,000 kg 196,200 lb MTOW 7,484 kg 16,500 lb
4,000 nmi 7,408 km range 1,048 km 566 nm
871 km/h 541 mph cruise speed 425 km/h 264 mph
185 to 220 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.