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.