As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRINGER 24S CLIP IS CORRODED AT BS 547. STRINGER CLIP 24S AT STA 547 FOUND TO BE OUT OF LIMITS IAW SRM 53-30-03-00-01, REV 12. REMOVED STRINGER CLIP AT STA 547 STR 24S IAW SRM 51-42-05-02-01, REV 12. NEW CLIP MATCH DRILLED TO ACFT IAW SRM REV 12 51-40-07-02-01. INSTALLED STR CLIP IAW SRM 51-42-05-02-01, REV 12. APPLIED PRIMER AND TOPCOAT IAW SRM 51-25-10-02-01 AND 51-25-15-02-01, REV 12. APPLIED CPC IAW AMM 51-25-01-390-801 REV 40.