As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C2 AFT PIT AT FS 1220 L33R FITTING IS CORRODED ***CPCP*** REMOVED CORROSION IAW DC8 SRM 51-1-8 ORIGINAL THICKNESS 0.125 MINIMUM REMAINING THICKNESS IS 0.063 & FOUND TO BE OUT OF LIMITS RMVD CORROSION LOCATED & DRILL NEW FITTING IAW DC8 SRM 51-1-21 AND INSTALLED FIT TING IAW DC8 SRM 51-1-20D