Airbus A330-300 vs. Airbus H225 Super Puma
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Airbus A330-300 |
versus |
Airbus H225 Super Puma |
63.66 m |
208 ft 9 in |
length |
14.06 m |
46 ft 2 in |
16.79 m |
55 ft 1 in |
height |
4.38 m |
14 ft 4 in |
60.3 m |
197 ft 9 in |
wingspan |
|
|
General Electric CF6-80E, Pratt & Whitney PW4000 series, Rolls-Royce Trent 700 |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
311.4 kN (Pratt & Whitney PW4170), 304.7 kN (General Electric CF6-80E1A3), 316.3 kN (Rolls-Royce Trent 772C-60) |
thrust per engine |
2,778 hp |
Depends on the engine type |
total thrust |
5,556 hp |
242,000 kg |
533,600 lb |
MTOW |
11,000 kg |
24,251 lb |
11,750 km |
6,346 nm |
range |
857 km |
463 nm |
900 km/h |
559 mph |
cruise speed |
242 km/h |
150 mph |
250-290 |
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.