What was found
FORWARD CARGO DOOR PAN IS CORRODED ON VERTICAL & HORIZONTAL FLANGES AT STRINGER 26R BETWEEN FUSELAGE STATINS 370 & 427. SPLICED IN NEW SECTION OF PAN IAW SRM 53-05-00 & EA 253062.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
FORWARD CARGO DOOR PAN IS CORRODED ON VERTICAL & HORIZONTAL FLANGES AT STRINGER 26R BETWEEN FUSELAGE STATINS 370 & 427. SPLICED IN NEW SECTION OF PAN IAW SRM 53-05-00 & EA 253062.