Engine RU19A-300

Technical specifications:

            Static thrust at rated power  7 845 N (800 kp)

            Weight                                  320 kg

            Maximum height for starting 6500m in flight

                                                                  4000m on the ground (mountains)

            Start                                    to -30 ° on the ground without preheating

                                                         to -20 ° in the air (from -20 ° preheating is connected)

The RU-19 is located in the rear part of the right engine nacelle.