As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION COMMON TO PRESSURE FLOOR ANGLE AT FUSELAGE STATION 559.00 LBL 40 . TO LBL 42. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION AT FS 559.00 LBL 40 TO LBL 42, 1.1 INCH WIDE X 1.2 INCH LONG PERFORMED HFEC NO DEFECTS NOTED, PERFORMED UT THICHNESS CHECK, MINIMUM REMAINING THICKNESS .076 INCHES. FOUND TO BE WITHIN LIMITS. RESTORED PROTECTIVE FINISH REF REO 601R-53-41-666 REV C 2012-11-06.