Douglas DC-6 vs. Airbus H225 Super Puma

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Douglas DC-6 versus Airbus H225 Super Puma
32.18 m 105 ft 7 in length 14.06 m 46 ft 2 in
8.94 m 29 ft 4 in height 4.38 m 14 ft 4 in
35.81 m 117 ft 6 in wingspan
4 x Pratt & Whitney R-2800-CB17 radial engines engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 2,500 hp per engine thrust per engine 2,778 hp
Approximately 10,000 hp total total thrust 5,556 hp
52,200 kg 115,100 lb MTOW 11,000 kg 24,251 lb
5,800 km 3,133 nm range 857 km 463 nm
507 km/h 315 mph cruise speed 242 km/h 150 mph
Up to 102 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.