Dornier 228 vs. Airbus H225 Super Puma

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Dornier 228 versus Airbus H225 Super Puma
16.56 m 54 ft 4 in length 14.06 m 46 ft 2 in
4.86 m 15 ft 11 in height 4.38 m 14 ft 4 in
16.97 m 55 ft 8 in wingspan
2 x Garrett TPE331 turboprop engines engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 776 kW per engine thrust per engine 2,778 hp
Approximately 1,552 kW total total thrust 5,556 hp
5,650 kg 12,456 lb MTOW 11,000 kg 24,251 lb
1,465 km 791 nm range 857 km 463 nm
350 km/h 217 mph cruise speed 242 km/h 150 mph
Up to 19 passengers 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.