Airbus A300-600 vs. Grumman OV-1 Mohawk

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Airbus A300-600 versus Grumman OV-1 Mohawk
54.10 m 177 ft 6 in length 12.52 m 41 ft 1 in
16.5 m 54 ft 2 in height 3.89 m 12 ft 9 in
44.84 m 147 ft 1 in wingspan 14.63 m 48 ft
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 2 x Lycoming T53 turboprop engines
56,000lb to 61,500lb thrust per engine Approximately 1,100 hp each
112,000–123,000 lb total thrust Approximately 2,200 hp total
171,700 kg 378,600 lb MTOW 14,950 lb 6,781 kg
7,500 km 4,052 nm range 1,690 km 913 nm
897 km/h 557 mph cruise speed 230 mph 370 km/h
210-250 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.