Airbus A310-300 vs. Grumman OV-1 Mohawk

versus
... or view the full comparison list here.
Airbus A310-300 versus Grumman OV-1 Mohawk
46.66 m 153 ft 1 in length 12.52 m 41 ft 1 in
15.8 m 51 ft 10 in height 3.89 m 12 ft 9 in
43.9 m 144 ft wingspan 14.63 m 48 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 x Lycoming T53 turboprop engines
52,000 lb thrust per engine Approximately 1,100 hp each
104,000 lb total thrust Approximately 2,200 hp total
148,768 kg 328,000 lb MTOW 14,950 lb 6,781 kg
8,050 km 4,348 nm range 1,690 km 913 nm
482 knots 279 mph cruise speed 230 mph 370 km/h
190-230 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.