Bombardier CRJ1000 vs. Short C-23 Sherpa

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Bombardier CRJ1000 versus Short C-23 Sherpa
39.1 m 128 ft 5 in length 17.68 m 58 ft 0 in
7.5 m 24 ft 7 in height 6.55 m 21 ft 6 in
26.2 m 86 ft wingspan 22.76 m 74 ft 8 in
2 GE CF34-8C5A1 turbofans engines 2 x Pratt & Whitney Canada PT6A-45R turboprop engines
13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve thrust per engine Approximately 1,200 hp per engine
27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve total thrust Approximately 2,400 hp total
41,640 kg 91,800 lb MTOW 7,484 kg 16,500 lb
3,004 km 1,623 nm range 1,048 km 566 nm
515 mph 829 km/h cruise speed 425 km/h 264 mph
100 (common) 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.