Airbus A318 vs. Grumman OV-1 Mohawk

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Airbus A318 versus Grumman OV-1 Mohawk
31.44 m 103 ft 2 in length 12.52 m 41 ft 1 in
12.56 m 41 ft 3 in height 3.89 m 12 ft 9 in
34.1 m 111 ft 11 in wingspan 14.63 m 48 ft
2x CFM56-5B or 2x PW6000 engines 2 x Lycoming T53 turboprop engines
23,300 lb thrust per engine Approximately 1,100 hp each
46,600 lb total thrust Approximately 2,200 hp total
59,000 kg 130,000 lb MTOW 14,950 lb 6,781 kg
5,750 km 3,106 nm range 1,690 km 913 nm
963km/h 598mph cruise speed 230 mph 370 km/h
107 to 132 passengers capacity Pilot and observer
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.