As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORRODED FUSELAGE SKIN AT F/STA 150 STRINGER 33L. CORROSION WAS FOUND 2 INCHES FORWARD OF AN EXISTING REPAIR MADE PER OVERHAUL MANUAL FIGURE 12-22. REMOVE EXISTING REPAIR AND CUT-OUT CORRODED AREA. EXTEND REPAIR PER OVERHAUL MANUAL FIGURE 12-22 TO COVER NEW DAMAGED AREA.