Airbus A321LR vs. Soko G-2 Galeb

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Airbus A321LR versus Soko G-2 Galeb
44.51 m 146 ft 0 in length 10.34 m 33 ft 11 in
11.76 m 38 ft 7 in height 3.28 m 10 ft 9 in
35.8 m 117 ft 5 in wingspan 11.62 m 38 ft 1 in
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines 1 x Armstrong Siddeley Viper II Mark 22/6 turbojet
Over 33,000 lbs (147 kN) thrust per engine 2,500 lb
66,000 lbs (294 kN) total thrust 2,500 lb
97,000 kg 213,800 lb MTOW 4,300 kg 9,480 lb
7,400 km 4,000 nm range 1,242 km 671 nm
832 km/h 517 mph cruise speed 730 km/h 454 mph
180-220 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.