Airbus A310-300 vs. North American Rockwell OV-10 Bronco

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Airbus A310-300 versus North American Rockwell OV-10 Bronco
46.66 m 153 ft 1 in length 12.7 m 41 ft 7 in
15.8 m 51 ft 10 in height 4.62 m 15 ft 2 in
43.9 m 144 ft wingspan 12.19 m 40 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 x Garrett T76-G-420/421 turboprop engines
52,000 lb thrust per engine Approximately 715 hp each
104,000 lb total thrust Approximately 1,430 hp total
148,768 kg 328,000 lb MTOW 14,444 lb 6,553 kg
8,050 km 4,348 nm range 1,931 km 1,043 nm
482 knots 279 mph cruise speed 244 mph 393 km/h
190-230 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.