Canadair CL-415 vs. Airbus H225 Super Puma

versus
... or view the full comparison list here.
Canadair CL-415 versus Airbus H225 Super Puma
19.82 m 65 ft 0 in length 14.06 m 46 ft 2 in
8.66 m 28 ft 5 in height 4.38 m 14 ft 4 in
28.6 m 93 ft 1 wingspan
2 x Pratt & Whitney Canada PW123AF turboprop engines engines 2 x Turbomeca Makila 2A turboshaft engines
2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW) thrust per engine 2,778 hp
4,300 to 4,760 shaft horsepower total thrust 5,556 hp
19,733 kg 43,525 lb MTOW 11,000 kg 24,251 lb
1,600 km 864 nm range 857 km 463 nm
290 km/h 180 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.