As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INITIAL INSPECTION : CRACKED RH RING PAN STA Y= 984 AND 1041 AT LOWER FWD CORNER PAX CABIN. DAMAGE AREA WAS REPAIRED PER DC9/MD80 SRM 53-05 FIG. 122. (ET)(HFEC) WAS ACCOMPLISHED ON RH RING PAN STA Y=984 AND 1041 AT LOWER FWD CORNER PAX CABIN AND NO CRACK INDICATIONS WERE FOUND AFTER TRIMMED. (LP0334901)