As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING CHECK-C MAINT FOUND CORROSION AT ATTACH HOLES FOR FUSELAGE FILLET AREA, BENEATH RUB STRIP AT STA 1104 TO 1136, LOWER LT SIDE. REMOVED CORROSION FROM ATTACH HOLES PER SPM 6-10-01. REPAIR MATERIAL LOSS PER PART 1-51-04-00 MARKED ON SKIN.