Airbus A220-100 vs. Commonwealth CA-25 Winjeel
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Airbus A220-100 |
versus |
Commonwealth CA-25 Winjeel |
35.0 m |
114 ft 10 in |
length |
7.77 m |
25 ft 6 in |
11.5 m |
37 ft 9 in |
height |
2.84 m |
9 ft 4 in |
35.1 m |
115 ft 2 in |
wingspan |
10.82 m |
35 ft 6 in |
2 Turbofans (wing mounted) |
engines |
1 x Pratt & Whitney R-985-AN-2 radial engine |
21,000–23,000 lb |
thrust per engine |
Approximately 450 hp |
42,000–46,000 lb |
total thrust |
Approximately 450 hp |
63,100 kg |
139,100 lb |
MTOW |
5,650 lb |
2,563 kg |
6,390 km |
3,451 nm |
range |
1,287 km |
695 nm |
871 km/h |
541 mph |
cruise speed |
150 mph |
241 km/h |
Typical seating 2-class 100-120 |
capacity |
Instructor pilot and one student |
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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.