Airbus A321-200 vs. Grumman OV-1 Mohawk

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Airbus A321-200 versus Grumman OV-1 Mohawk
44.51 m 146 ft 0 in length 12.52 m 41 ft 1 in
11.76 m 38 ft 7 in height 3.89 m 12 ft 9 in
35.8 m 117 ft 5 in wingspan 14.63 m 48 ft
2 GE CFM56-5B3 engines 2 x Lycoming T53 turboprop engines
31,600 lbs thrust per engine Approximately 1,100 hp each
63,200 lbs total thrust Approximately 2,200 hp total
89,000 kg 196,200 lb MTOW 14,950 lb 6,781 kg
4,000 nmi 7,408 km range 1,690 km 913 nm
871 km/h 541 mph cruise speed 230 mph 370 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.