Airbus A321-200 vs. Short C-23 Sherpa
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Airbus A321-200 |
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 |
2 GE CFM56-5B3 |
engines |
2 x Pratt & Whitney Canada PT6A-45R turboprop engines |
31,600 lbs |
thrust per engine |
Approximately 1,200 hp per engine |
63,200 lbs |
total thrust |
Approximately 2,400 hp total |
89,000 kg |
196,200 lb |
MTOW |
7,484 kg |
16,500 lb |
4,000 nmi |
7,408 km |
range |
1,048 km |
566 nm |
871 km/h |
541 mph |
cruise speed |
425 km/h |
264 mph |
185 to 220 |
capacity |
based on configuration |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.