Airbus H225 Super Puma vs. Bell 412
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Airbus H225 Super Puma |
versus |
Bell 412 |
14.06 m |
46 ft 2 in |
length |
17,10 m |
56 ft 1 in |
4.38 m |
14 ft 4 in |
height |
3,48 m |
11 ft 5 in |
|
|
wingspan |
|
|
2 x Turbomeca Makila 2A turboshaft engines |
engines |
2 x Pratt & Whitney Canada PT6T-3D turboshaft engines |
2,778 hp |
thrust per engine |
1,800 hp |
5,556 hp |
total thrust |
3,600 hp |
11,000 kg |
24,251 lb |
MTOW |
5,400 kg |
11,905 lb |
857 km |
463 nm |
range |
659 km |
356 nm |
242 km/h |
150 mph |
cruise speed |
259 km/h |
161 mph |
24-28 |
capacity |
13 |
16.2 m |
53 ft 2 in |
rotor diameter |
14.0 m |
45 ft 11 in |
10.7 m/s |
2,106 ft/min |
rate of climb |
9.5 m/s |
1,870 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.