As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TWO CORROSION SPOTS OUT OF SRM LIMITS ON INTERNAL SKIN BETWEEN FRAME 19-20, STRG 51-52 LHS. REPAIR PERFORMED BY CORROSION REMOVAL, FLAP PEENING, NDT INSPECTION FOR CRACK FREE CONDITION AND INSTALLATION OF ENLARGED FILLER AND FINGER STRAP IAW EA 6-5313-82909 AND RAS/DABRE/7005417/2006 ISSUE A.