As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE CPCP INSPECTION, FOUND CORROSION ON FRAME TO SPAR FITTING CENTER WING UPPER SKIN UNDER CUSP RIGHT SIDE STA680 X=-64. REMOVED CORROSION IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. REMOVED FITTING AND REPLACED WITH NEW FITTING IAW DC8 SRM 51-1-20D. CORROSION TASK CARD NUMBER 2000-0551. NON-ROUTINE NR 02199 TASK NR X0021.