Airbus A321LR vs. Short C-23 Sherpa

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Airbus A321LR 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
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 2 x Pratt & Whitney Canada PT6A-45R turboprop engines
Over 33,000 lbs (147 kN) thrust per engine Approximately 1,200 hp per engine
66,000 lbs (294 kN) total thrust Approximately 2,400 hp total
97,000 kg 213,800 lb MTOW 7,484 kg 16,500 lb
7,400 km 4,000 nm range 1,048 km 566 nm
832 km/h 517 mph cruise speed 425 km/h 264 mph
180-220 passengers 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.