As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CREW DOOR, AFT FRAME (FR16.1) MECHANISM LOCK FITTING HAS GOUGE. DOT 103-62 (ATTACHED PHOTO) REMOVED MINOR GOUGE AT LOCK FITTING IAW SRM A300-600 51-73-11 MATERIAL THIKNESS IS 1.100" AND MATERIAL LOSS 0.003 AND REMAINING THIKNESS IS 1.197" THERE IS WHTIN IN LIMITS IAW SRM 51-73-11 T98826 C18-C02 AND RESTORE SURFACE PROTECTION.