Cessna 172 vs. Airbus H225 Super Puma
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Cessna 172 |
versus |
Airbus H225 Super Puma |
8.28 m |
27 ft 2 in |
length |
14.06 m |
46 ft 2 in |
2.72 m |
8 ft 11 in |
height |
4.38 m |
14 ft 4 in |
11 m |
36 ft 1 in |
wingspan |
|
|
1 x Lycoming IO-360-L2A flat-4 piston engine |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
180 to 200 horsepower (134 to 149 kW) |
thrust per engine |
2,778 hp |
180 to 200 horsepower (134 to 149 kW) |
total thrust |
5,556 hp |
1,040 kg |
2,293 lb |
MTOW |
11,000 kg |
24,251 lb |
1,056 km |
570 nm |
range |
857 km |
463 nm |
226 km/h |
140 mph |
cruise speed |
242 km/h |
150 mph |
4 |
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.