As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION AROUND SCREW HOLE ON INNER SKIN OF SERVICE DOOR JUST ABOVE HINGE POINT. BLENDED CORROSION AROUND SCREW HOLE ON INNER SKIN OF SERVICE DOOR JUST ABOVE HINGE POINT, ORIGINAL MAT .063. REMOVED .001 OF MATERIAL REMAINING MATERIAL IS .062 IS WITHIN SERVICEABLE LIMITS IAW SRM 51-12-00. MAJOR REPAIR.