N. American T-28 Trojan vs. Airbus H225 Super Puma

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N. American T-28 Trojan versus Airbus H225 Super Puma
10.06 m 33 ft 0 in length 14.06 m 46 ft 2 in
3.86 m 12 ft 8 in height 4.38 m 14 ft 4 in
12.22 m 40 ft 1 in wingspan
1 x Wright R-1820-86 Cyclone radial engine engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 1,425 hp thrust per engine 2,778 hp
Approximately 1,425 hp total thrust 5,556 hp
8,500 lb 3,856 kg MTOW 11,000 kg 24,251 lb
1,705 km 921 nm range 857 km 463 nm
210 mph 338 km/h cruise speed 242 km/h 150 mph
Pilot and one passenger 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.