As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACKED RING PAN ON FWD UPPER CORNER BETWEEN BS 756 AND 775. DAMAGE WAS REMOVED IAW SRM 56-20-02 REP 1. HFEC INSPECTION WAS ACCOMPLISHED ALONG THE TRIM LINE, NO CRACKS WERE FOUND IAW 06-10-01.001. RING PAN WAS REPAIRED IAW SRM 56-20-02 REP 1.