As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT UPPER WING, REMOVED CORROSION AT 57\ O/B OF BBL 70.5 AND 8\ FWD OF REAR SPAR. REMOVED APPROX .010\ MAT AND TREATED AREA WITH ALODINE. CORR DID NOT GO INTO FASTENER AND FASTENER OKAY REF AVO ENC120524-5325-1. INSPECTED AREA WBL 139.0 USING 757 NDT PART 4 51 00 00 AND MEASURED .007 INCH, REMOVED FOR CORROSION, ORIG THICKNESS .330 INCH NO LAMINAR CORROSION FOUND, USING AVO ENC120524-5325-1 ITEMS 4 & 5.