As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TOOLING DAMAGE TO LEFT WING LOWER SKIN FASTENER HOLE AFT INBOARD HOLE COMMON TO AFT PITCH LOAD FITTING, DAMAGED OCCURRED DURING THE ACCOMPLISHMENT OF SIP MOD. DISCREPANT HOLE WAS OVERSIZED AND STRAIGHT SHANK REPAIR BUSHING INSTALLED AND RE-INSTALLATION COMPLIED WITH SIP MOD PER SB 767-54-0081 (DL76G102856).