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 FOUND ON FUSELAGE FRAME AT FUSELAGE STATION 70 BETWEEN LONGERONS 32 AND 33 RIGHT. REPAIR WAS ACCOMPLISHED BY CORROSION REMOVAL, FABRICATION AND INSTALLATION OF A NESTED ANGLE REPAIR DOUBLER IN ACCORDANCE WITH FAA DER APPROVED DRAWING E27-R04 AND ENGINEERING ORDER 53-DC8-820.