As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STANCHION AT FR 236 IS CORRODED BY STR 31P. BLENDED AWAY CORROSION IAW SRM 51-21-00-00-01. MINIMUM REMAINING THICKNESS IS .014", MATERIAL LOSS OUT OF LIMITS. REMOVED STANCHION IAW SRM 51-42-05-02-01. RECEIVED NEW PART AND MATCH DRILLED IAW SRM 51-42-05-02-01. INSTALLED STANCHION IAW SRM 51-42-05-02-01 AND 51-42-15-02-01.