As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE ATTACH FITTINGS: VERTICAL STABILIZER CLEVIS LUGS - CORROSION. THE NR 11 CLEVIS LUG FWD FACE WAS FOUND GOUGED. THE DAMAGE WAS CLEANED UP USING A SPOTFACE, WITH A MIN REMAINING LUG THICKNESS OF 0.940 INCH IAW DAL ER/A 412535-14, INITIAL RELEASE.