Airbus A330-200 vs. Airbus H225 Super Puma
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here.
Airbus A330-200 |
versus |
Airbus H225 Super Puma |
58.82 m |
193 ft 0 in |
length |
14.06 m |
46 ft 2 in |
17.39 m |
57 ft 1 in |
height |
4.38 m |
14 ft 4 in |
64 m |
210 ft |
wingspan |
|
|
2 Turbofans |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf |
thrust per engine |
2,778 hp |
Depends on the engine variant |
total thrust |
5,556 hp |
251,000 kg |
553,400 lb |
MTOW |
11,000 kg |
24,251 lb |
15,094 km |
8,150 nm |
range |
857 km |
463 nm |
531 mph |
855 km/h |
cruise speed |
242 km/h |
150 mph |
220-260 |
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.