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, A GOUGED WAS DETECTED AT FUSELAGE STATION 1703, LONGERON 22 LEFT FUSELAGE FRAME CAP. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED CAP, FABRICATION AND INSTALLATION IN ACCORDANCE WITH DACO DRAWING 5612146 AND ENGINEERING ORDER 53-DC8-1783.