Airbus A320-200 vs. Grumman OV-1 Mohawk

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Airbus A320-200 versus Grumman OV-1 Mohawk
38.7 m 127 ft 0 in length 12.52 m 41 ft 1 in
17.4 m 57 ft 1 in height 3.89 m 12 ft 9 in
35.8 m 117 ft 5 in wingspan 14.63 m 48 ft
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines 2 x Lycoming T53 turboprop engines
Between 21,000 - 33,000 lbf thrust per engine Approximately 1,100 hp each
Between 42,000 - 66,000 lbf total thrust Approximately 2,200 hp total
77,000 kg 169,800 lb MTOW 14,950 lb 6,781 kg
5,700 km 3,078 nm range 1,690 km 913 nm
530 mph 853 km/h cruise speed 230 mph 370 km/h
Typically between 140-180 passengers 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.