Airbus A321-200 vs. Commonwealth CA-25 Winjeel
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Airbus A321-200 |
versus |
Commonwealth CA-25 Winjeel |
44.51 m |
146 ft 0 in |
length |
7.77 m |
25 ft 6 in |
11.76 m |
38 ft 7 in |
height |
2.84 m |
9 ft 4 in |
35.8 m |
117 ft 5 in |
wingspan |
10.82 m |
35 ft 6 in |
2 GE CFM56-5B3 |
engines |
1 x Pratt & Whitney R-985-AN-2 radial engine |
31,600 lbs |
thrust per engine |
Approximately 450 hp |
63,200 lbs |
total thrust |
Approximately 450 hp |
89,000 kg |
196,200 lb |
MTOW |
5,650 lb |
2,563 kg |
4,000 nmi |
7,408 km |
range |
1,287 km |
695 nm |
871 km/h |
541 mph |
cruise speed |
150 mph |
241 km/h |
185 to 220 |
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.