CASA 2.111 vs. Airbus H225 Super Puma

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CASA 2.111 versus Airbus H225 Super Puma
16.4 m 53 ft 10 in length 14.06 m 46 ft 2 in
3.9 m 12 ft 10 in height 4.38 m 14 ft 4 in
22.5 m 73 ft 1 wingspan
2 × Rolls-Royce Merlin 500-29 V-12 liquid-cooled piston engines engines 2 x Turbomeca Makila 2A turboshaft engines
1,176 kW (1,577 hp) thrust per engine 2,778 hp
2,352 kW (3,154 hp) total thrust 5,556 hp
14,000 kg 30,900 lb MTOW 11,000 kg 24,251 lb
1,950 km 1,053 nm range 857 km 463 nm
315 km/h 196 mph cruise speed 242 km/h 150 mph
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.