Airbus A220-100 vs. North American Rockwell OV-10 Bronco

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Airbus A220-100 versus North American Rockwell OV-10 Bronco
35.0 m 114 ft 10 in length 12.7 m 41 ft 7 in
11.5 m 37 ft 9 in height 4.62 m 15 ft 2 in
35.1 m 115 ft 2 in wingspan 12.19 m 40 ft
2 Turbofans (wing mounted) engines 2 x Garrett T76-G-420/421 turboprop engines
21,000–23,000 lb thrust per engine Approximately 715 hp each
42,000–46,000 lb total thrust Approximately 1,430 hp total
63,100 kg 139,100 lb MTOW 14,444 lb 6,553 kg
6,390 km 3,451 nm range 1,931 km 1,043 nm
871 km/h 541 mph cruise speed 244 mph 393 km/h
Typical seating 2-class 100-120 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.