As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACKED RING PAN ON AFT UPPER CORNER BETWEEN BS 889 AND 908. DAMAGE WAS REMOVED IAW SRM 56-20-02 REP 1. HFEC INSPECTION WAS ACCOMPLISHED ALONG THE TRIM LINE, NO CRACKS WERE FOUND 06-10-01.001. THE RING PAN WAS REPAIRED IAW SRM 56-20-02 REP 1.