As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACKED FWD UPPER ANGLE ON WINDOW RING PAN STA Y= 598 BELOW LONG 12 RT AT INTERNAL STRUCTURE. DAMAGE WAS REMOVED IAW SRM 53-05 FIG 122. REPAIR PARTS WERE FABRICATED IAW DC9/MD80 SRM 53-05 FIG 122. REPAIR PARTS WERE TREATED AND PAINTED IAW SRM 51-10-3 P21 AND 14. REPAIR PARTS WERE INSTALLED IAW SRM 51-30-2 AND 51-30-5.