Airbus A220-300 vs. Short C-23 Sherpa

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Airbus A220-300 versus Short C-23 Sherpa
38.7 m 127 ft 0 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 x Pratt & Whitney PurePower PW1500G 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
70,900 kg 156,300 lb MTOW 7,484 kg 16,500 lb
6,297 km 3,402 nm range 1,048 km 566 nm
Mach 0.82 101,3 km/h cruise speed 425 km/h 264 mph
Typical seating 2-class 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.