Airbus A300-600F vs. Piper PA-34 Seneca

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Airbus A300-600F versus Piper PA-34 Seneca
54.08 m 177 ft 5 in length 8.71 m 28 ft 7 in
17.05 m 55 ft 11 in height 2.99 m 9 ft 10 in
44.84 m 147 ft 1 in wingspan 11.64 m 38 ft 2 in
2 x General Electric CF6-80C2A5 turbofan engines engines 2 x Continental IO-360
Approximately 59,000 lbf per engine thrust per engine 220 lbs
Approximately 118,000 lbf total total thrust 440 lbs
170,000 kg 374,786 lb MTOW 4,750 lb 2,155 kg
4,830 km 2,608 nm range 980 nm 1,815 km
860 km/h 534 mph cruise speed 165 kts 103 mph
capacity 5
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.