What was found
LOWER FUSELAGE FR 40, CENTER WING JOINT FOUND LT UPPER HOLE WITH CRACK. SIGNAL COMPLIED WITH FEDEX EA: 6-5710-T0356552 PT1, EA TITLE: WINGS-BASIC WING STRUCTURE-CRACK IN THE HOLES AT FR 40 LT AND RT CENTER WING JOINT. REPAIRED LOWER FUSELAGE FR 40, CENTER WING JOINT LT UPPER HOLE. THIS REPAIR CATEGORY B. SEE APPROVED DATA OF RDAS 80827737/006/2020 ISSUE A, WHICH PROVIDES STATIC STRENGTH APPROVAL. THE REPAIR HAS BEEN APPROVED BY AIRBUS TO BE STRUCTURALLY ACCEPTABLE AS INTERIM WITH A 6 MONTHS REPAIR LIFE LIMITATION FROM TIME OF REPAIR EMBODIMENT PENDING COMPLETION OF THE FATIGUE ANALYSIS. MAJOR REPAIR, IAW FEDEX GMM6-2-100.