What was found
CORROSION ON FUSELAGE SKIN AREA BELOW FILLET PANEL RUBSTRIP UPPER SECTION BTW STA Y= 760 TO Y= 800. CORROSION ON FUSELAGE SKIN WAS ATTENDED PER SRM 51-10-04 (1378771)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON FUSELAGE SKIN AREA BELOW FILLET PANEL RUBSTRIP UPPER SECTION BTW STA Y= 760 TO Y= 800. CORROSION ON FUSELAGE SKIN WAS ATTENDED PER SRM 51-10-04 (1378771)