Brake actuator assembly with line replaceable motor features

An aircraft brake system electromechanical actuator (104) is provided. The actuator is configured with features that allow the electric motor (206) to be a line replaceable unit. One such feature is a foreign-object-damage shield (708) that inhibits dust, debris, and/or other particulate contaminants from entering the electromechanical actuator during electric motor removal and replacement.