Beechcraft T-6 Texan II vs. Airbus H225 Super Puma

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Beechcraft T-6 Texan II versus Airbus H225 Super Puma
10.18 m 33 ft 4 in length 14.06 m 46 ft 2 in
3.29 m 10 ft 10 in height 4.38 m 14 ft 4 in
10.21 m 33 ft 6 in wingspan
1 x Pratt & Whitney Canada PT6A-68 engines 2 x Turbomeca Makila 2A turboshaft engines
1100 lbs thrust per engine 2,778 hp
1100 lbs total thrust 5,556 hp
6,250 lb 2,835 kg MTOW 11,000 kg 24,251 lb
900 nm 1,667 km range 857 km 463 nm
320 kts 199 mph cruise speed 242 km/h 150 mph
2 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.