Airbus A300-600 vs. Soko G-2 Galeb

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Airbus A300-600 versus Soko G-2 Galeb
54.10 m 177 ft 6 in length 10.34 m 33 ft 11 in
16.5 m 54 ft 2 in height 3.28 m 10 ft 9 in
44.84 m 147 ft 1 in wingspan 11.62 m 38 ft 1 in
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines 1 x Armstrong Siddeley Viper II Mark 22/6 turbojet
56,000lb to 61,500lb thrust per engine 2,500 lb
112,000–123,000 lb total thrust 2,500 lb
171,700 kg 378,600 lb MTOW 4,300 kg 9,480 lb
7,500 km 4,052 nm range 1,242 km 671 nm
897 km/h 557 mph cruise speed 730 km/h 454 mph
210-250 passengers capacity Fuel capacity: 1,120 ltr
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.