Airbus A310-300 vs. Bell 412

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Airbus A310-300 versus Bell 412
46.66 m 153 ft 1 in length 17,10 m 56 ft 1 in
15.8 m 51 ft 10 in height 3,48 m 11 ft 5 in
43.9 m 144 ft wingspan
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 x Pratt & Whitney Canada PT6T-3D turboshaft engines
52,000 lb thrust per engine 1,800 hp
104,000 lb total thrust 3,600 hp
148,768 kg 328,000 lb MTOW 5,400 kg 11,905 lb
8,050 km 4,348 nm range 659 km 356 nm
482 knots 279 mph cruise speed 259 km/h 161 mph
190-230 passengers capacity 13
rotor diameter 14.0 m 45 ft 11 in
rate of climb 9.5 m/s 1,870 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.