de Havilland Canada DHC-2 Beaver vs. Airbus H225 Super Puma

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de Havilland Canada DHC-2 Beaver versus Airbus H225 Super Puma
13.56 m 44 ft 6 in length 14.06 m 46 ft 2 in
5 m 16 ft 5 in height 4.38 m 14 ft 4 in
16.56 m 54 ft 4 in wingspan
2 x Armstrong Siddeley Double Mamba turboprop engines engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 3,100 hp (2,312 kW) each thrust per engine 2,778 hp
Approximately 6,200 hp (4,624 kW) total total thrust 5,556 hp
24,200 lb 10,977 kg MTOW 11,000 kg 24,251 lb
2,535 km 1,369 nm range 857 km 463 nm
228 mph 367 km/h cruise speed 242 km/h 150 mph
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling 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.