As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FASTENER HOLE CRACKED ON PANEL 561CB<[01] REMOVED DAMAGE AND APPLIED REPAIR PER SRM 51-70-04-2R-9;[02] C/W INSPECTION.;[03] RESIN SWEEPED AND SANDED TO AERODYNAMIC SMOOTHNESS PER SRM 51-70-08;[04] C/W INSPECTION.;[05] PRIMED PER AMM 51-21-72 APPLIED TOPCOAT PER AMM 51-21-73;[06] C/W INSPECTION.