Short C-23 Sherpa vs. Airbus H225 Super Puma

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Short C-23 Sherpa versus Airbus H225 Super Puma
17.68 m 58 ft 0 in length 14.06 m 46 ft 2 in
6.55 m 21 ft 6 in height 4.38 m 14 ft 4 in
22.76 m 74 ft 8 in wingspan
2 x Pratt & Whitney Canada PT6A-45R turboprop engines engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 1,200 hp per engine thrust per engine 2,778 hp
Approximately 2,400 hp total total thrust 5,556 hp
7,484 kg 16,500 lb MTOW 11,000 kg 24,251 lb
1,048 km 566 nm range 857 km 463 nm
425 km/h 264 mph cruise speed 242 km/h 150 mph
based on configuration 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.