What was found
DURING C-CHECK, FOUND FWD ENTRANCE DOOR HAS CRACK .5 INCH ON EDGE OF DOOR SKIN, LOWER FWD CORNER. INSTALLED REPAIR IAW SRM 52-05, FIG 32.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING C-CHECK, FOUND FWD ENTRANCE DOOR HAS CRACK .5 INCH ON EDGE OF DOOR SKIN, LOWER FWD CORNER. INSTALLED REPAIR IAW SRM 52-05, FIG 32.