What was found
GSO - INSPECTION FOUND AFT EDGE OF C-2 DOOR SKIN BUCKLED AND CRACKED IN TWO PLACES. THE CRACKS WERE .75 INCH LONG. THE DAMAGED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 52-00-03. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
GSO - INSPECTION FOUND AFT EDGE OF C-2 DOOR SKIN BUCKLED AND CRACKED IN TWO PLACES. THE CRACKS WERE .75 INCH LONG. THE DAMAGED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 52-00-03. (X)