As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON R1 DOOR INNER PAN "THE FWD GALLEY DOOR STUB FRAME HFEC INSP" CRACK WAS INDICATED APPROX .5 INCH, LOCATION MARKED. (THIS IS IN REF TO SUB STEP 5A). REMOVED AND REPLACED R-1 DOOR FWD UPPER INNER PAN FRAME SRM 51-40-02-0G-0 AND DWG141A8370 ESFR NO. 852.