Airbus A340-200 vs. Airbus H225 Super Puma
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Airbus A340-200 |
versus |
Airbus H225 Super Puma |
59.4 m |
194 ft 11 in |
length |
14.06 m |
46 ft 2 in |
16.8 m |
55 ft 1 in |
height |
4.38 m |
14 ft 4 in |
60.3 m |
197 ft 9 in |
wingspan |
|
|
4 x CFM International CFM56-5C4 |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
34,000 lbf |
thrust per engine |
2,778 hp |
136,000 lbf |
total thrust |
5,556 hp |
275,000 kg |
606,300 lb |
MTOW |
11,000 kg |
24,251 lb |
12,400 km |
6,699 nm |
range |
857 km |
463 nm |
880 km/h |
547 mph |
cruise speed |
242 km/h |
150 mph |
Typical seating 3-class 210-250 |
capacity |
24-28 |
|
|
rotor diameter |
16.2 m |
53 ft 2 in |
|
|
rate of climb |
10.7 m/s |
2,106 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.