METHOD AND SYSTEM FOR THRUST REVERSER OPERATION

A method for operating a thrust reverser (202) of an aircraft engine (100), the thrust reverser (202) having a deployed state and a stowed state comprises placing the thrust reverser (202) in the stowed state when the thrust reverser (202) is in the deployed state, a thrust lever (302) associated with the engine (100) is in a forward position (F), and the engine (100) is rotating at a speed below an idle speed, wherein hydraulic pressure for stowing the thrust reverser (202) is provided by a pump (304) driven by the engine (100) rotating at the speed below the idle speed.