Praetor 600 vs. Airbus H225 Super Puma

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Praetor 600 versus Airbus H225 Super Puma
17.02 m 55 ft 10 in length 14.06 m 46 ft 2 in
6.2 m 20 ft 4 in height 4.38 m 14 ft 4 in
20.97 m 68 ft 9 in wingspan
2 Honeywell HTF7500E engines 2 x Turbomeca Makila 2A turboshaft engines
7,036 lbf thrust per engine 2,778 hp
14,072 lbf total thrust 5,556 hp
31,750 lb 14,397 kg MTOW 11,000 kg 24,251 lb
4,018 nm 7,435 km range 857 km 463 nm
466 kts 290 mph cruise speed 242 km/h 150 mph
12 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.