Airbus A300-600 vs. Piper PA-34 Seneca

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Airbus A300-600 versus Piper PA-34 Seneca
54.10 m 177 ft 6 in length 8.71 m 28 ft 7 in
16.5 m 54 ft 2 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 turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 2 x Continental IO-360
56,000lb to 61,500lb thrust per engine 220 lbs
112,000–123,000 lb total thrust 440 lbs
171,700 kg 378,600 lb MTOW 4,750 lb 2,155 kg
7,500 km 4,052 nm range 980 nm 1,815 km
897 km/h 557 mph cruise speed 165 kts 103 mph
210-250 passengers 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.