As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
STABILIZER REMOVABLE LE PANEL 341A INTERNAL FIBERGLASS WEB HAS A CRACK AT A FWD RIVET. REMOVED NUT PLATES; FOR FURTHER INSPECTION IAW SRM 51-40-02. REMOVED PAINT IN SUPPOSED DAMAGED AREA. NO DEFECTS NOTED TO PLY'S ON FWD AND AFT SIDE. CRACK ARE LINES IN THE MANUFACTURING PROCESS. IAW SRM 51-10-02-0G-0. REAPPLIED PROTECTIVE PROTECTIVE FINISHES IAW AMM 51-21-99.