A fitting for an aircraft bracing device including anchor points, wherein the fitting includes a face able to press against the aircraft and at least one guide hole for a connecting element able to collaborate with an anchor point, a slider able to move in a translational movement parallel to a first direction parallel to the face of the fitting and a connection between the slider and the connecting element which allows a movement in a second direction different from the first direction and parallel to the face of the fitting so as to align the connecting element with an anchor point.
Fitting for an aircraft bracing device
2017-03-07
Patent
Elektronische Ressource
Englisch