As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE C-CHECK INSP FOUND CHORD CRACKED AT STA 287 RT BOTTOM LINE 25. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCIES NOTED. FABRICATED DOUBLERS. HEAT TREATED REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 51-70-12, 51-40-02, AND NDT 51-00-19, PART6,