North American T-6 Texan vs. Airbus H225 Super Puma

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North American T-6 Texan versus Airbus H225 Super Puma
9.0 m 29 ft 6 in length 14.06 m 46 ft 2 in
3.56 m 11 ft 8 in height 4.38 m 14 ft 4 in
12.8 m 42 ft wingspan
1 x Pratt & Whitney R-1340-AN-1 radial engine engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 600 hp thrust per engine 2,778 hp
Approximately 600 hp total thrust 5,556 hp
5,617 lb 2,548 kg MTOW 11,000 kg 24,251 lb
1,175 km 634 nm range 857 km 463 nm
145 mph 233 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.