Airbus A340-200 vs. Commonwealth CA-25 Winjeel
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Airbus A340-200 |
versus |
Commonwealth CA-25 Winjeel |
59.4 m |
194 ft 11 in |
length |
7.77 m |
25 ft 6 in |
16.8 m |
55 ft 1 in |
height |
2.84 m |
9 ft 4 in |
60.3 m |
197 ft 9 in |
wingspan |
10.82 m |
35 ft 6 in |
4 x CFM International CFM56-5C4 |
engines |
1 x Pratt & Whitney R-985-AN-2 radial engine |
34,000 lbf |
thrust per engine |
Approximately 450 hp |
136,000 lbf |
total thrust |
Approximately 450 hp |
275,000 kg |
606,300 lb |
MTOW |
5,650 lb |
2,563 kg |
12,400 km |
6,699 nm |
range |
1,287 km |
695 nm |
880 km/h |
547 mph |
cruise speed |
150 mph |
241 km/h |
Typical seating 3-class 210-250 |
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.