Airbus A350-900ULR vs. Airbus H225 Super Puma
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Airbus A350-900ULR |
versus |
Airbus H225 Super Puma |
66.80 m |
219 ft 2 in |
length |
14.06 m |
46 ft 2 in |
17.05 m |
55 ft 11 in |
height |
4.38 m |
14 ft 4 in |
64.75 m |
212 ft 5 in |
wingspan |
|
|
2 Rolls-Royce Trent XWB |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
84,000 lbs |
thrust per engine |
2,778 hp |
168,000 lbs |
total thrust |
5,556 hp |
280,000 kg |
617,300 lb |
MTOW |
11,000 kg |
24,251 lb |
17,964 km |
9,700 nm |
range |
857 km |
463 nm |
552 mph |
888 km/h |
cruise speed |
242 km/h |
150 mph |
300-350 passengers in three classes |
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.