As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND CORROSION SPOTS ON FUSELAGE SKIN PANEL AT BUTT-STRAP C18 BETWEEN P26-27 LT. REPAIR WAS PERFORMED IAW TD942.047408/017/2006A (EA 6-5312-103399) AND APPROVED BY RAS/AS/165/2006 ISSUE:A. SEE ALSO DR 186 WHICH IS PERFORMED WITH MENTIONED RAS.