Airbus A310-300 vs. Short 360

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Airbus A310-300 versus Short 360
46.66 m 153 ft 1 in length 17.74 m 58 ft 2 in
15.8 m 51 ft 10 in height 6.8 m 22 ft 4 in
43.9 m 144 ft wingspan 22.72 m 74 ft 6 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 x Pratt & Whitney Canada PT6A-65R
52,000 lb thrust per engine 2,430 lbs
104,000 lb total thrust 4,860 lbs
148,768 kg 328,000 lb MTOW 28,400 lb 12,882 kg
8,050 km 4,348 nm range 820 nm 1,519 km
482 knots 279 mph cruise speed 220 kts 137 mph
190-230 passengers capacity 36
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.