As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON FUSELAGE LOWER SKIN BS 1088 RBL 5 TO LBL5 JUST FORWARD WL 210 OF APU DOOR. REMOVED CORROSION IN TWO AREA'S 4'X7' AND 0.50'X7 MAX BLEND OF .005' IN BOTH AREA'S ORIGINAL THICKNESS 0.080'. AS PER EA 20-153-01244 REV IR AND ATS ER. 20-02917 REV IR THE DAMAGE IS ALLOWABLE FOR CONTINUED SERVICE WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTION REQUIREMENTS.