Airbus A310-300 vs. Temco TT Pinto

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Airbus A310-300 versus Temco TT Pinto
46.66 m 153 ft 1 in length 9.33 m 30 ft 7 in
15.8 m 51 ft 10 in height 3.3 m 10 ft 10 in
43.9 m 144 ft wingspan 9.09 m 29 ft 1
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 1 × Continental YJ69-T-9
52,000 lb thrust per engine 920 lb f (4.1 kN)
104,000 lb total thrust 920 lb f (4.1 kN)
148,768 kg 328,000 lb MTOW 4,453 lb 2,020 kg
8,050 km 4,348 nm range 300 km 162 nm
482 knots 279 mph cruise speed 345 mph 555 km/h
190-230 passengers capacity Fuel capacity: 119 US gal (99 imp gal; 450 L) normal; 165 US gal (137 imp gal; 620 L) max
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.