Airbus A321-200 vs. North American Rockwell OV-10 Bronco

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Airbus A321-200 versus North American Rockwell OV-10 Bronco
44.51 m 146 ft 0 in length 12.7 m 41 ft 7 in
11.76 m 38 ft 7 in height 4.62 m 15 ft 2 in
35.8 m 117 ft 5 in wingspan 12.19 m 40 ft
2 GE CFM56-5B3 engines 2 x Garrett T76-G-420/421 turboprop engines
31,600 lbs thrust per engine Approximately 715 hp each
63,200 lbs total thrust Approximately 1,430 hp total
89,000 kg 196,200 lb MTOW 14,444 lb 6,553 kg
4,000 nmi 7,408 km range 1,931 km 1,043 nm
871 km/h 541 mph cruise speed 244 mph 393 km/h
185 to 220 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.