What was found
LEVEL 2 CORROSION, LOWER AFT FUSELAGE SKIN HAS INTERNAL CORROSION WITH BULGING SKIN AND CRACKED RIVET HEADS AT ST1536 FROM STR 33 TO STR 35L. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-31-00.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEVEL 2 CORROSION, LOWER AFT FUSELAGE SKIN HAS INTERNAL CORROSION WITH BULGING SKIN AND CRACKED RIVET HEADS AT ST1536 FROM STR 33 TO STR 35L. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 53-31-00.