As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C1 AFT PIT STA 1020 L36 2 NUT PLATES WITH CORROSION ON FRAME UNDER NUT PLATES. REMOVED CORROSION MAT ID 7075-T6 0.625 PO 334056. FAB IAW DWG DC8-53 A-011. HEAT TREATED, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. NEW FRAME CAP P/N 57643434507. LOCATED AND DRILLED HOLES IAW DC8 SRM 51-1-24. INSTALLED IAW DC8 SRM 51-2-20D.