Boeing 767-200ER vs. Airbus H225 Super Puma
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Boeing 767-200ER |
versus |
Airbus H225 Super Puma |
48.5 m |
159 ft 2 in |
length |
14.06 m |
46 ft 2 in |
16.1 m |
52 ft 10 in |
height |
4.38 m |
14 ft 4 in |
47.8 m |
156 ft 9 in |
wingspan |
|
|
2 x GE CF6-80C2B4F |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
62,020 lbs |
thrust per engine |
2,778 hp |
124,040 lbs |
total thrust |
5,556 hp |
164,200 kg |
362,000 lb |
MTOW |
11,000 kg |
24,251 lb |
12,200 km |
6,587 nmi |
range |
857 km |
463 nm |
850 km/hour |
528 mph |
cruise speed |
242 km/h |
150 mph |
249 |
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.