Airbus H225 Super Puma vs. Bell 206
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Airbus H225 Super Puma |
versus |
Bell 206 |
14.06 m |
46 ft 2 in |
length |
12.11 m |
39 ft 9 in |
4.38 m |
14 ft 4 in |
height |
2.88 m |
9 ft 5 in |
|
|
wingspan |
|
|
2 x Turbomeca Makila 2A turboshaft engines |
engines |
1 × Allison 250-C20B |
2,778 hp |
thrust per engine |
420 shp (313 kW) |
5,556 hp |
total thrust |
420 shp (313 kW) |
11,000 kg |
24,251 lb |
MTOW |
1,451 kg |
3,199 lb |
857 km |
463 nm |
range |
374 km |
202 nm |
242 km/h |
150 mph |
cruise speed |
222 km/h |
138 mph |
24-28 |
capacity |
1 pilot + 4 passengers |
16.2 m |
53 ft 2 in |
rotor diameter |
11.00 m |
36 ft 1 in |
10.7 m/s |
2,106 ft/min |
rate of climb |
425 m/min |
1,395 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.