As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SAL - C21 - MAJOR REPAIR - CRACK ON SUPPORT PAN ASSEMBLY OF AFT GALLEY DOOR INTERNAL STRUCTURE FORWARD EDGE AT BS 955 BETWEEN WL 218.34 TO WL 266.93. REPLACED SUPPORT PAN ASSEMBLY OF AFT GALLEY DOOR INTERNAL STRUCTURE FORWARD EDGE AT BS 955 BETWEEN WL 218.34 TO WL 266.93 IAW SRM 51-40-02.