What was found
DURING THE INSPECTION STRUCTURE INSPECTION PER RDAS 80150308/002/2016 ISSUE A ROTO TEST INSPECTIONS, THERE WERE FOUND TWO HOLES WITH CRACK INDICATION AT FRAME 66, AT STOP FITTING #5 AREA, DUE TO THIS FACT DETAILS WERE SENT TO AIRBUS ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL. AFTER AIRBUS EVALUATION, REPAIR INSTRUCTIONS WERE PROVIDED UNDER DOSSIER 80150308. THE REPAIR WAS HANDLED UNDER COO JOB A1M100 ITEM 2-41.