As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
R-1 DOOR FRAME HAS A CRACK IN INNER CLOSE OUT PANEL; EMITTING FROM UPPER FWD CAM PLATE ATTACHMENT. SEE ATTACHED PICTURE. CRACK IS 2 IN LENGTH AND ENDS AT DOOR OPENING CUTOUT. VERIFIED CRACK WITH HFEC PROC 23<[01] OK TO INSTALL INNER CLOSE OUT PANEL PER 51-40-02;[02] REMOVED AND REPLACED FORWARD GALLEY ENTRY DOORWAY FRAME ASSEMBLY P/N 141A8370U13; AT FWD UPPER CORNER OF DOORWAY PER SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02.