As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THREE CORROSION SPOTS ON INNER SKIN PANEL BETWEEN FRAME 18-19 AND BETWEEN STRG 49-51 LHS. REPAIR PERFORMED BY LOCAL CUT OUT AF SKIN PANEL BETWEEN STRG 49-50 AND SMOOTH REWORK OF REMAINING CORRODED AREAS, HFEC-, ROTOTEST INSPECTION AND INSTALLING EXTERNAL SKIN DOUBLER IAW EA 6-5312-92140 AND RAS/AS/135/2005 ISSUE A.