As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION - SUPPORT, FWD CGO ENGWALL CURTAIN SUPPORT STRUCTURE RH SIDE STANCHION NUTPLATE AREA.REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.91.PERFORMED THE HEAT TREATMENT FROM 7075-O TO T62 CONDITION. I.A.W. EGAT WORK SHEET NO.50165 STEP 3. AND SPWPS-HT-008 REV.33 AND SPDS-HT-005 REV.3.INSTALLED FABRICATE PART I.A.W SRM 51-40-02-0G REV.91 AND BOEING DWG NO: 453T1146 SH 11 REV. E.