FIELD: aircraft engines. SUBSTANCE: control system for thrust reverser incorporating movable parts has at least one unit of electromechanical drive elements connected to electronic control unit. Electromechanical drive unit mainly has linear power-operated hoist used for setting in motion one movable part of thrust reverser and at least one power-operated lock referred to as primary lock and used to hold mentioned movable part in position. Electromechanical drive elements and electronic control unit are supplied with power from aircraft power system through power conductors. EFFECT: improved reliability of thrust reversal, reduced mass and cost of control system. 15 cl, 1 dwg
