What was found
UPON REMOVAL OF GALLEY TIE ROD ATTACH PLATE THE L-ANGLE STRINGER WAS DAMAGED, FASTNER REMOVAL CAUSED END OF ANGLE TO CRACK OFF. REPAIRED IAW SRM 51-20-01 AND SRM 51-40-02.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
UPON REMOVAL OF GALLEY TIE ROD ATTACH PLATE THE L-ANGLE STRINGER WAS DAMAGED, FASTNER REMOVAL CAUSED END OF ANGLE TO CRACK OFF. REPAIRED IAW SRM 51-20-01 AND SRM 51-40-02.