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 FRAME FLANGE AT FUSELAGE STATION 1380, LONGERON 35 LEFT. REPAIR ACCOMPLISH CORROSION REMOVAL, FABRICATION AND INSTALLATION A REPAIR ANGLE IN ACCORDANCE WITH DACO STRUCTURAL REPAIR MANUAL AND ENGINEERING ORDER 51-DC8-1782.