Bombardier CRJ1000 vs. Airbus H225 Super Puma

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Bombardier CRJ1000 versus Airbus H225 Super Puma
39.1 m 128 ft 5 in length 14.06 m 46 ft 2 in
7.5 m 24 ft 7 in height 4.38 m 14 ft 4 in
26.2 m 86 ft wingspan
2 GE CF34-8C5A1 turbofans engines 2 x Turbomeca Makila 2A turboshaft engines
13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve thrust per engine 2,778 hp
27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve total thrust 5,556 hp
41,640 kg 91,800 lb MTOW 11,000 kg 24,251 lb
3,004 km 1,623 nm range 857 km 463 nm
515 mph 829 km/h cruise speed 242 km/h 150 mph
100 (common) 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.