As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING D-CHECK, HEAVY CORROSION RIGHT O/B END OF BS 1176.9 CHORD. REMOVED CHORD ANGLE PER SRM 51-30-2. REMOVED CORROSION PER SRM 51-10-6 MAT LOSS .002 INCH. REPLACED CHORD ANGLE PER SRM 51-10-1 PAR 4 AND INSTALLED PER SRM 51-30-2. TOTAL CYCLES 29235.