As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DAMAGES ON SKIN PANEL AT FRAME 33 BETWEEN STRG 38-39 RT. REPAIR PERFORMED BY REWORK DAMAGES TO A SMOOTH CONTOUR. MINIMUM THICKNESS FOLLOWING REWORK IS 1.37MM, NDT INSPECTION FOR CRACK FREE CONDITION AND ENLARGE THE INNER STRAP TO ACT AS A REPAIR DOUBLER IAW DD-0378007 ISSUE A, APPROVED BY EA 6-5314-92144 AND RAS/DABRE/7005386/2005 ISSUE A.