As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON LT FWD LOWER CORNER ON RING PAN OF WINDOW BETWEEN BS 617 AND 636. 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. CRACK RING PAN WAS REPAIRED IAW SRM 56-20-02 REP 1.