As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INITIAL INSPECTION : CRACKED LH RING PAN STA Y= 927 AND 946 AT UPPER FWD CORNER PAX CABIN. DAMAGE AREA WAS REPAIRED PER DC9/MD80 SRM 53-05 FIG. 122. HFEC INSPECTION WAS ACCOMPLISHED ON LH RING PAN STA. Y= 927 AND Y=946 AT UPPER FWD CORNER, NO CRACKS WERE FOUND AFTER TRIM OUT. (LP0336335)