As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
OLD REPAIR ON FRAME 13, STRG 14 LT, FUSELAGE NOSE SECTION. THE REINFORCEMENT REPAIR ANGLE AT FRAME SEGMENT WAS CHAFED AND AFTER REWORK OUT OF LIMIT. REPAIR PERFORMED BY INSTALLING NEW REPAIR ANGLE AT OLD REPAIR AS PER PRINCIPLE IN SRM 53-10-13.