As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PANEL 561CB HAS SEVERAL PULLED FASTENER HOLES. FABRICATED REPAIR PLIES. INSTALLED THE REPAIR PLIES. VACUUM BAGGED AND SET FOR CURE IAW SRM 51-70-04-2R-9 PARA 4. ACCOMPLISHED UT INSPECTION IAW NDTM D6-37239 PART 4; 51-00-02. NO DISBONDS FOUND.