Grumman OV-1 Mohawk vs. Airbus H225 Super Puma

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Grumman OV-1 Mohawk versus Airbus H225 Super Puma
12.52 m 41 ft 1 in length 14.06 m 46 ft 2 in
3.89 m 12 ft 9 in height 4.38 m 14 ft 4 in
14.63 m 48 ft wingspan
2 x Lycoming T53 turboprop engines engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 1,100 hp each thrust per engine 2,778 hp
Approximately 2,200 hp total total thrust 5,556 hp
14,950 lb 6,781 kg MTOW 11,000 kg 24,251 lb
1,690 km 913 nm range 857 km 463 nm
230 mph 370 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.