Douglas DC-8-61 vs. Airbus H225 Super Puma

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Douglas DC-8-61 versus Airbus H225 Super Puma
57.0 m 187 ft 0 in length 14.06 m 46 ft 2 in
13.1 m 43 ft height 4.38 m 14 ft 4 in
45.24 m 148 ft 5 in wingspan
4x P&W JT3D-3B Turbofan engines 2 x Turbomeca Makila 2A turboshaft engines
18,000 pound-force thrust per engine 2,778 hp
72,000 pound-force total thrust 5,556 hp
147,400 kg 325,000 lb MTOW 11,000 kg 24,251 lb
3,200 nm 5,926 km range 857 km 463 nm
483 knots 282 mph cruise speed 242 km/h 150 mph
180 to 220 passengers in a mixed-class seating 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.