What was found
DURING C-2 CHECK, INSPECTION REPORTED FWD GALLEY DOOR INNER DOOR SKIN CRACKED AT ATTACH RIVET, FWD EDGE, CENTER SPAN. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-30-02, 51-10-02 AND 51-21-0.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-2 CHECK, INSPECTION REPORTED FWD GALLEY DOOR INNER DOOR SKIN CRACKED AT ATTACH RIVET, FWD EDGE, CENTER SPAN. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-30-02, 51-10-02 AND 51-21-0.