Airbus A310-300 vs. Boeing CH-47 Chinook

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Airbus A310-300 versus Boeing CH-47 Chinook
46.66 m 153 ft 1 in length 15.88 m 51 feet 2 inches
15.8 m 51 ft 10 in height 5.68 m 18 feet 7.8 inches
43.9 m 144 ft wingspan
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 x Honeywell T55-GA-714A turboshaft engines
52,000 lb thrust per engine 4,868 hp
104,000 lb total thrust 9,736 hp
148,768 kg 328,000 lb MTOW 22,680 kg 50,000 lb
8,050 km 4,348 nm range 370 km 200 nm
482 knots 279 mph cruise speed 259 km/h 161 mph
190-230 passengers capacity 33-55
rotor diameter 18.3 m 60 ft
rate of climb 10.2 m/s 2,008 ft/min
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.