Boeing 777-200LR Worldliner vs. Airbus H225 Super Puma
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Boeing 777-200LR Worldliner |
versus |
Airbus H225 Super Puma |
63.7 m |
209 ft 1 in |
length |
14.06 m |
46 ft 2 in |
18.6 m |
61 ft |
height |
4.38 m |
14 ft 4 in |
64.8 m |
212 ft 7 in |
wingspan |
|
|
2 x GE90-115B |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
115,300 lbf |
thrust per engine |
2,778 hp |
230,600 lbf |
total thrust |
5,556 hp |
347,500 kg |
766,100 lb |
MTOW |
11,000 kg |
24,251 lb |
15,843 km |
8,555 nmi |
range |
857 km |
463 nm |
950 km/h |
590 mph |
cruise speed |
242 km/h |
150 mph |
317 (2-class) |
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.