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 STA 489.5. REMOVED STRINGER CLIP 24S AT STA 489.5 IAW Q400 SRM 51-42-05-02-01 REV 12. FOUND STRINGER CLIP 24S AT STA 489.5 TO BE OUT OF LIMITS PRIOR TO REMOVAL IAW SRM 53-30-03-00-01, REV 12. MATCH DRILLED TO ACFT IAW SRM REV 12 51-40-07-02-01. INSTALLED STRINGER CLIP SRM 51-42-05-02-01, REV 12. APPLIED PRIMER, TOPCOAT AND CPC IAW SRM 51-25-10-02-01, 51-25-15-02-01 REV 12 AND AMM 51-25-01-390-801 REV 40.