North American Rockwell OV-10 Bronco vs. Airbus H225 Super Puma

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North American Rockwell OV-10 Bronco versus Airbus H225 Super Puma
12.7 m 41 ft 7 in length 14.06 m 46 ft 2 in
4.62 m 15 ft 2 in height 4.38 m 14 ft 4 in
12.19 m 40 ft wingspan
2 x Garrett T76-G-420/421 turboprop engines engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 715 hp each thrust per engine 2,778 hp
Approximately 1,430 hp total total thrust 5,556 hp
14,444 lb 6,553 kg MTOW 11,000 kg 24,251 lb
1,931 km 1,043 nm range 857 km 463 nm
244 mph 393 km/h cruise speed 242 km/h 150 mph
Pilot and observer 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.