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 LOWER SIDE 8 INCHES FROM AFT EDGE AT BS 965 BETWEEN WL 215. REPLACED SUPPORT PAN ASSEMBLY OF AFT GALLEY DOOR INTERNAL STRUCTURE LOWER SIDE 8 INCHES FROM AFT EDGE AT BS 965 BETWEEN WL 215 IAW SRM 51-40-02.