As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/H WING REAR SPAR UPPER CAP UPPER SURFACE FROM I/B OF O/B OF FLAP TO O/B OF O/B AILERON SHOW NUMEROUS OF SURFACE CORROSION (MARKED) REMOVED CORROSION PER E.A1-5710-T034511 PART 1 FROM XORS=486.600 - XORS=827.000. REMOVED CORROSION PER E.A.1-5710-T034511PART 2 FROM XORS=843.000-XORS=1070.000