Airbus A340-500 vs. Commonwealth CA-25 Winjeel
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Airbus A340-500 |
versus |
Commonwealth CA-25 Winjeel |
67.93 m |
222 ft 10 in |
length |
7.77 m |
25 ft 6 in |
17.53 m |
57 ft 6 in |
height |
2.84 m |
9 ft 4 in |
63.45 m |
208 ft 2 in |
wingspan |
10.82 m |
35 ft 6 in |
4 Rolls-Royce Trent 500 |
engines |
1 x Pratt & Whitney R-985-AN-2 radial engine |
54,000 lbf (240 kN) |
thrust per engine |
Approximately 450 hp |
216,000 lbf (960 kN) |
total thrust |
Approximately 450 hp |
380,000 kg |
837,800 lb |
MTOW |
5,650 lb |
2,563 kg |
16,670 km |
9,000 nm |
range |
1,287 km |
695 nm |
475 knots |
880 km/h |
cruise speed |
150 mph |
241 km/h |
Typical seating 3-class 270-310 |
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.