Airbus A220-300 vs. Grumman OV-1 Mohawk

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Airbus A220-300 versus Grumman OV-1 Mohawk
38.7 m 127 ft 0 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 x Pratt & Whitney PurePower PW1500G 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
70,900 kg 156,300 lb MTOW 14,950 lb 6,781 kg
6,297 km 3,402 nm range 1,690 km 913 nm
Mach 0.82 101,3 km/h cruise speed 230 mph 370 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.