Device to handle and lock a cover of an aircraft nacelle

The object of the invention is an aircraft nacelle that comprises, on the inside, an inside pipe that empties out toward the front at an air intake, and, on the outside, an aerodynamic wall that extends from the air intake up to the rear end of the nacelle, and a hood that comprises said air intake as well as a cylindrical wall that forms at least one portion of the aerodynamic surface of the outside of the nacelle, whereby said hood can move translationally relative to a stationary part of the nacelle toward the front along slides, each slide comprising a guide element that is connected to the hood (or to the stationary part of the nacelle), whereby said guide element can slide into a pipe that is connected to the stationary part of the nacelle (or to a hood) and has a section that is above the section of the guide element so as to allow the hood to rotate in order to immobilize it in the closed position.