Airbus A220-100 vs. Soko G-2 Galeb

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Airbus A220-100 versus Soko G-2 Galeb
35.0 m 114 ft 10 in length 10.34 m 33 ft 11 in
11.5 m 37 ft 9 in height 3.28 m 10 ft 9 in
35.1 m 115 ft 2 in wingspan 11.62 m 38 ft 1 in
2 Turbofans (wing mounted) engines 1 x Armstrong Siddeley Viper II Mark 22/6 turbojet
21,000–23,000 lb thrust per engine 2,500 lb
42,000–46,000 lb total thrust 2,500 lb
63,100 kg 139,100 lb MTOW 4,300 kg 9,480 lb
6,390 km 3,451 nm range 1,242 km 671 nm
871 km/h 541 mph cruise speed 730 km/h 454 mph
Typical seating 2-class 100-120 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.