As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON CUSP WEB BS 663 BTW LBL 54 TO 60. HFEC WAS ACCOMPLISHED AND A CRACK WAS CONFIRMED OF 1.900" LENGTH IAW NDT SPM 06-10-01 .001: THE CRACK WAS STOPPED DRILL IAW SRM 51-00-07 PAR 5. HFEC WAS ACCOMPLISHED IAW NDT SPM 06-10-01 .001 AND NO CRACKS WERE FOUND AFTER STOP DRILL. THE CUSP WEB WAS REPAIRED IAW SRM 53-00-55 REPAIR 4.