Commonwealth CA-25 Winjeel vs. Airbus H225 Super Puma

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Commonwealth CA-25 Winjeel versus Airbus H225 Super Puma
7.77 m 25 ft 6 in length 14.06 m 46 ft 2 in
2.84 m 9 ft 4 in height 4.38 m 14 ft 4 in
10.82 m 35 ft 6 in wingspan
1 x Pratt & Whitney R-985-AN-2 radial engine engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 450 hp thrust per engine 2,778 hp
Approximately 450 hp total thrust 5,556 hp
5,650 lb 2,563 kg MTOW 11,000 kg 24,251 lb
1,287 km 695 nm range 857 km 463 nm
150 mph 241 km/h cruise speed 242 km/h 150 mph
Instructor pilot and one student 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.