Cessna O-2 Skymaster vs. Airbus H225 Super Puma
... or view the full comparison list
here.
| Cessna O-2 Skymaster |
versus |
Airbus H225 Super Puma |
| 8.9 m |
29 ft 2 in |
length |
14.06 m |
46 ft 2 in |
| 2.87 m |
9 ft 5 in |
height |
4.38 m |
14 ft 4 in |
| 11.58 m |
38 ft |
wingspan |
|
|
| Two 210-hp Continental IO-360s |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
| 210 hp |
thrust per engine |
2,778 hp |
| 420 hp |
total thrust |
5,556 hp |
| 5,400 lb |
2,449 kg |
MTOW |
11,000 kg |
24,251 lb |
| 1,705 km |
921 nm |
range |
857 km |
463 nm |
| 144 mph |
232 km/h |
cruise speed |
242 km/h |
150 mph |
| 2 |
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.
