What was found
AFT FUSELAGE MAIN CABIN LT UPPER SHEET PN 170-86101-001, BETWEEN FRAME 85 & 86, Y=-260.4 HAS CORROSION. ACCOMPLISHED PERMANENT REPAIR IAW EO NO E175-5300-123 REV IR WO 1958236 & 19451292B9.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
AFT FUSELAGE MAIN CABIN LT UPPER SHEET PN 170-86101-001, BETWEEN FRAME 85 & 86, Y=-260.4 HAS CORROSION. ACCOMPLISHED PERMANENT REPAIR IAW EO NO E175-5300-123 REV IR WO 1958236 & 19451292B9.