Airbus A319neo vs. Airbus H225 Super Puma

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Airbus A319neo versus Airbus H225 Super Puma
33.84 m 111 ft 0 in length 14.06 m 46 ft 2 in
11.76 m 38 ft 7 in height 4.38 m 14 ft 4 in
35.8 m 117 ft 5 in wingspan
2 x PW 1100G or 2 x CFM LEAP-1A engines 2 x Turbomeca Makila 2A turboshaft engines
110kN (PW 1100G) or 109-156kN (CFM LEAP-1A) thrust per engine 2,778 hp
220kN (PW 1100G) or 218-312kN (CFM LEAP-1A) total thrust 5,556 hp
75,500 kg 166,400 lb MTOW 11,000 kg 24,251 lb
6,850 km 3,702 nm range 857 km 463 nm
530 mph 853 km/h cruise speed 242 km/h 150 mph
120-150 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.