Method for repairing composite laminate material component

A method for repairing a composite laminate component, the method comprising:

• removing a damaged portion of the composite laminate component, the composite laminate component extends between and to a first component side and a second component side, the composite laminate component includes a first plurality of layers having a first sequential arrangement from the first component side to the second component side, the composite laminate component forms a plurality of mounting holes extending through the first plurality of layers, and the damaged portion includes the first plurality of layers and at least one of the plurality of mounting holes;
• preparing a repair portion for the composite laminate component, the repair portion extends between and to a first portion side and a second portion side, the repair portion includes a second plurality of layers having a second sequential arrangement from the first portion side to the second portion side, and the second sequential arrangement is different than the first sequential arrangement;
• positioning the repair portion on the composite laminate component with the second plurality of layers at the first plurality of layers;
• and
• forming the at least one of the plurality of mounting holes in the repair portion;
• wherein each of the first sequential arrangement and the second sequential arrangement includes opposing outer layers and intermediate layers extending between and to the opposing outer layers, and the intermediate layers of the first sequential arrangement are different than the intermediate layers of the second sequential arrangement;
• and
• wherein the intermediate layers of the first sequential arrangement include one or more carbon fiber layers and one or more aramid fiber layers and each of the intermediate layers of the second sequential arrangement is an aramid fiber layer.

A method for repairing a composite laminate component, the method comprising:

• removing a first portion of the composite laminate component, the composite laminate component extends between and to a first component side and a second component side, the composite laminate component includes a first plurality of layers including one or more carbon fiber ply layers and one or more aramid fiber ply layers, the first plurality of layers has a first sequential arrangement from the first component side to the second component side, and the first portion includes the first plurality of layers;
• preparing a second portion for the composite laminate component, the second portion extends between and to a first portion side and a second portion side, the second portion includes a second plurality of layers with each layer of the second plurality of layers comprising an aramid fiber ply layer, the second plurality of layers has a second sequential arrangement from the first portion side to the second portion side, and the second sequential arrangement is different than the first sequential arrangement;
• positioning the second portion on the composite laminate component with the one or more carbon fiber ply layers disposed at a respective one or more of the plurality of aramid fiber ply layers;
• and
• curing the second portion with the second portion positioned on the composite laminate component.