As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
SEVERAL CORROSION POINTS ON FUSELAGE SKIN BTW STA Y=794 TO Y=851 BTW LONG 26L TO 26R AT FILLET PANELS AREA IN REF 5315-2001. (FUS). NRC 00420: CORROSION LEVEL 2, AREA WAS REPAIRED PER ER/A 579396-14 REV ORIGINAL SECTION I AND SECTION II. ASSOCIATED ER/A 00-579396 ADDED FOR AC 9508. (LP #1168257)