As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON FUSELAGE EXTERNAL PLATING BETWEEN FUSELAGE STATIONS 30 AND 61 LONGERON 34 RIGHT. REPAIR ACCOMPLISHED BY REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND REPAIR DOUBLERS IN ACCORDANCE WITH FAA DER APPROVED DRAWING E27-R03 AND ENGINEERING ORDER 53-DC8-825.