Airbus A330-200 vs. Soko G-2 Galeb

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Airbus A330-200 versus Soko G-2 Galeb
58.82 m 193 ft 0 in length 10.34 m 33 ft 11 in
17.39 m 57 ft 1 in height 3.28 m 10 ft 9 in
64 m 210 ft wingspan 11.62 m 38 ft 1 in
2 Turbofans engines 1 x Armstrong Siddeley Viper II Mark 22/6 turbojet
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf thrust per engine 2,500 lb
Depends on the engine variant total thrust 2,500 lb
251,000 kg 553,400 lb MTOW 4,300 kg 9,480 lb
15,094 km 8,150 nm range 1,242 km 671 nm
531 mph 855 km/h cruise speed 730 km/h 454 mph
220-260 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.