Airbus A220-100 vs. Grumman OV-1 Mohawk

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Airbus A220-100 versus Grumman OV-1 Mohawk
35.0 m 114 ft 10 in length 12.52 m 41 ft 1 in
11.5 m 37 ft 9 in height 3.89 m 12 ft 9 in
35.1 m 115 ft 2 in wingspan 14.63 m 48 ft
2 Turbofans (wing mounted) engines 2 x Lycoming T53 turboprop engines
21,000–23,000 lb thrust per engine Approximately 1,100 hp each
42,000–46,000 lb total thrust Approximately 2,200 hp total
63,100 kg 139,100 lb MTOW 14,950 lb 6,781 kg
6,390 km 3,451 nm range 1,690 km 913 nm
871 km/h 541 mph cruise speed 230 mph 370 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.