Airbus A350-900ULR vs. Commonwealth CA-25 Winjeel
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Airbus A350-900ULR |
versus |
Commonwealth CA-25 Winjeel |
66.80 m |
219 ft 2 in |
length |
7.77 m |
25 ft 6 in |
17.05 m |
55 ft 11 in |
height |
2.84 m |
9 ft 4 in |
64.75 m |
212 ft 5 in |
wingspan |
10.82 m |
35 ft 6 in |
2 Rolls-Royce Trent XWB |
engines |
1 x Pratt & Whitney R-985-AN-2 radial engine |
84,000 lbs |
thrust per engine |
Approximately 450 hp |
168,000 lbs |
total thrust |
Approximately 450 hp |
280,000 kg |
617,300 lb |
MTOW |
5,650 lb |
2,563 kg |
17,964 km |
9,700 nm |
range |
1,287 km |
695 nm |
552 mph |
888 km/h |
cruise speed |
150 mph |
241 km/h |
300-350 passengers in three classes |
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.