Airbus A320-200 vs. North American Rockwell OV-10 Bronco

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Airbus A320-200 versus North American Rockwell OV-10 Bronco
38.7 m 127 ft 0 in length 12.7 m 41 ft 7 in
17.4 m 57 ft 1 in height 4.62 m 15 ft 2 in
35.8 m 117 ft 5 in wingspan 12.19 m 40 ft
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 2 x Garrett T76-G-420/421 turboprop engines
Between 21,000 - 33,000 lbf thrust per engine Approximately 715 hp each
Between 42,000 - 66,000 lbf total thrust Approximately 1,430 hp total
77,000 kg 169,800 lb MTOW 14,444 lb 6,553 kg
5,700 km 3,078 nm range 1,931 km 1,043 nm
530 mph 853 km/h cruise speed 244 mph 393 km/h
Typically between 140-180 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.