As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK ON RT CUSP WEB BS 218 X=45 AT CABIN PAX RH. CRACK WAS STOP DRILL IAW SRM 53-00-55 REPAIR 4, HFEC INSPECTION WAS ACCOMPLISHED IAW NDT SPM 06-10-01.001, NO CRACKS WERE FOUND AFTER STOP DRILL. REPAIR DOUBLER WAS FABRICATED IAW SRM 53-00-55. AREA DRILLED WAS TREATED AND PAINTED IAW SRM 51-10-04 PAR 21 AND 15. REPAIR INSTALLED IAW SRM 53-00-55 REPAIR 4. C