Airbus A340-200 vs. Short C-23 Sherpa

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Airbus A340-200 versus Short C-23 Sherpa
59.4 m 194 ft 11 in length 17.68 m 58 ft 0 in
16.8 m 55 ft 1 in height 6.55 m 21 ft 6 in
60.3 m 197 ft 9 in wingspan 22.76 m 74 ft 8 in
4 x CFM International CFM56-5C4 engines 2 x Pratt & Whitney Canada PT6A-45R turboprop engines
34,000 lbf thrust per engine Approximately 1,200 hp per engine
136,000 lbf total thrust Approximately 2,400 hp total
275,000 kg 606,300 lb MTOW 7,484 kg 16,500 lb
12,400 km 6,699 nm range 1,048 km 566 nm
880 km/h 547 mph cruise speed 425 km/h 264 mph
Typical seating 3-class 210-250 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.