As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING INSPECTION CORROSION WAS FOUND ON THE SERVICE DOOR AFT SURROUND STRUCTURE. THE THICKNESS MEASUREMENT DONE BY UT IAW NDI MANUAL P.22 (F) ON REWORKED AREA FOUND THE MINIMUM MATERIAL THICKNESS REMAINING AT 0.022 INCHES. HFEC DONE ON THE AREA FOUND NO CRACKS. THE SERVICE DOOR AFT SURROUND STRUCTURE WAS REPAIRED IAW ETD2011-145-02494.