As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON INNER SKIN OF SERVICE DOOR JUST ABOVE HINGE AREA. BLENDED OUT MINOR CORROSION, REMOVING 0.002 OF MAT'L USING DEPTH GAUGE 1916 D/D 1-14-12 (ORIG THK 0.063) REMAINING THICKNESS WAS 0.061 BLENDED IAW SRM 51-21-06. MINOR REPAIR.