Airbus A220-300 vs. North American Rockwell OV-10 Bronco

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Airbus A220-300 versus North American Rockwell OV-10 Bronco
38.7 m 127 ft 0 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 x Pratt & Whitney PurePower PW1500G 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
70,900 kg 156,300 lb MTOW 14,444 lb 6,553 kg
6,297 km 3,402 nm range 1,931 km 1,043 nm
Mach 0.82 101,3 km/h cruise speed 244 mph 393 km/h
Typical seating 2-class 120-150 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.