Airbus A220-100 vs. Short C-23 Sherpa
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Airbus A220-100 |
versus |
Short C-23 Sherpa |
35.0 m |
114 ft 10 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 Turbofans (wing mounted) |
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 |
63,100 kg |
139,100 lb |
MTOW |
7,484 kg |
16,500 lb |
6,390 km |
3,451 nm |
range |
1,048 km |
566 nm |
871 km/h |
541 mph |
cruise speed |
425 km/h |
264 mph |
Typical seating 2-class 100-120 |
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.