As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION (C53-224-01) IN STR AND STR CLIP AT BS 660 STR 3R. REMOVED CORROSION AT STR 3 BS 660 RT. ORIGINAL THICKNESS .045, REMOVED .002, 5 INCH BY 1 INCH AREA WITHIN LIMITS PER FEDEX SRM 53-10-1, ALODINED AND PRIMED AREA. REMOVED STR CLIP AT BS 660 RT DUE TO CRACK. REPLACED STR CLIP PER FEDEX SRM 53-10-1.