Airbus A321LR vs. Grumman OV-1 Mohawk

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Airbus A321LR 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
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 2 x Lycoming T53 turboprop engines
Over 33,000 lbs (147 kN) thrust per engine Approximately 1,100 hp each
66,000 lbs (294 kN) total thrust Approximately 2,200 hp total
97,000 kg 213,800 lb MTOW 14,950 lb 6,781 kg
7,400 km 4,000 nm range 1,690 km 913 nm
832 km/h 517 mph cruise speed 230 mph 370 km/h
180-220 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.