Airbus A220-100 vs. Short C-23 Sherpa

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Airbus A220-100 versus Short C-23 Sherpa
35.0 m 114 ft 10 in length 17.68 m 58 ft 0 in
11.5 m 37 ft 9 in height 6.55 m 21 ft 6 in
35.1 m 115 ft 2 in wingspan 22.76 m 74 ft 8 in
2 Turbofans (wing mounted) engines 2 x Pratt & Whitney Canada PT6A-45R turboprop engines
21,000–23,000 lb thrust per engine Approximately 1,200 hp per engine
42,000–46,000 lb total thrust Approximately 2,400 hp total
63,100 kg 139,100 lb MTOW 7,484 kg 16,500 lb
6,390 km 3,451 nm range 1,048 km 566 nm
871 km/h 541 mph cruise speed 425 km/h 264 mph
Typical seating 2-class 100-120 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.