As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON FRAME BS 1148 BETWEEN STR 25-26 LT. BLENDED CORROSION FROM FRMAE BS 1148 BETWEEN STR 25-26 LT. REMOVED .040 FROM ORIGINAL THICKNESS OF .065. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGE MATERIAL 1 X 2.5 INCH. FABRICATED AND INSTALLED REPAIR IAW SRM 51-40-3 USING LOT 518135 AND ER NO. 03-4723 AND FED EX EA 7-5310-55168.