As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE C-CHECK AND CPCP INSPECTION. CORROSION WAS FOUND ON FUSELAGE FRAME UPPER CAP AT FUSELAGE STATION 1080 BETWEEN LONGERONS 30 LEFT AND 36. REPAIR ACCOMPLISHED BY REMOVING THE CORRODED AREA, FABRICATION AND INSTALLION OF A REPAIR FILLER AND REPAIR DOUBLER IN ACCORDANCE WITH ENGINEERING ORDER 53-DC8-436 AND FAA DER APPROVED DRAWING 853-06-97.