What was found
OUTWARD DING IN FUSELAGE SKIN REMOVED SKIN DAMAGE BY DRILLING A 0.1935" HOLE INSTALLED A BACR15BB6 RIVET IAW ASA EA 5330 02205 REV NEW AND AAR EA 112004 REV IR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
OUTWARD DING IN FUSELAGE SKIN REMOVED SKIN DAMAGE BY DRILLING A 0.1935" HOLE INSTALLED A BACR15BB6 RIVET IAW ASA EA 5330 02205 REV NEW AND AAR EA 112004 REV IR.