Airbus A300-600 vs. N. American T-28 Trojan

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Airbus A300-600 versus N. American T-28 Trojan
54.10 m 177 ft 6 in length 10.06 m 33 ft 0 in
16.5 m 54 ft 2 in height 3.86 m 12 ft 8 in
44.84 m 147 ft 1 in wingspan 12.22 m 40 ft 1 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 1 x Wright R-1820-86 Cyclone radial engine
56,000lb to 61,500lb thrust per engine Approximately 1,425 hp
112,000–123,000 lb total thrust Approximately 1,425 hp
171,700 kg 378,600 lb MTOW 8,500 lb 3,856 kg
7,500 km 4,052 nm range 1,705 km 921 nm
897 km/h 557 mph cruise speed 210 mph 338 km/h
210-250 passengers capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.