Airbus A321XLR vs. Grumman OV-1 Mohawk

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Airbus A321XLR 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 LEAP-1A and P&W PW1100G engines 2 x Lycoming T53 turboprop engines
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
101,000 kg 222,700 lb MTOW 14,950 lb 6,781 kg
4,700 nmi 8,704 km range 1,690 km 913 nm
963km/h 598mph cruise speed 230 mph 370 km/h
180-220 seats (typical 2-class seating) 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.