As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
1C/30 ACCESS FROM COCKPIT-UPPER FACE OF PRESSURE PANEL BELOW RUDDER PEDAL STA 110 JUNCTURE AT FUSELAGE FRAME HAS CORROSION AT RT END OF ANGLE 4 INCHES BY 3 INCHES CPCP TASK 45-53302. FABRICATED AND INSTALLED NEW ANGLE IAW DOUGLAS DRAWING NR 3911397 AND DC-9 SRM 51-30-5.