As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING CHECK-C MAINT, THE FWD CARGO DOOR INTERNAL DOOR SKIN HAD A 2 INCH CRACK IN THE RADIUS OUTBOARD SIDE OF AFT BOTTOM LATCH AND .5 INCH CRACK BETWEEN ADJACENT FASTENER HOLE. CRACK CONTAINED PER EDDY CURRENT PART L 51-00-03. INSTALLED DOUBLER PER SRM 52-05, FIG 26A.