As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON FUSELAGE INTERNAL SIDE OF THE SKIN PANEL JUST BEFOR E FR 20 AT STRINGER 28R. ACCOMPLISHED REPAIR AT FUSELAGE INTERNAL SIDE OF THE SKIN PANEL JUST BEFORE FR 20 AT STRG 28R IAW ECRA 5311-02682. ALL WORK ACCO MPLISHED ON HAECO NR 9296298.