As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STRINGER 25P IS CORROSDED AT FR 19.4. REMOVED CORROSION IAW SRM 51-21-00-000-02, REV12. VERIFIED BLENDS ARE CRACK FREE IAW NTM 51-00-06-910-801 PART1 REV 8. CORROSION DAMAGE ON STRINGER FOUND TO BE OUT OF LIMITS IAW SRM REV 12 53-20-17-00-01.