As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT HORIZONTAL STABILIZER CENTER SECTION FWD SPAR UPPER CLEVIS FWD AND AFT LUG HAVE EVIDENCE OF CORROSION. SPOTFACE FWD AND AFT FACES ON BOTH LUGS TO REMOVED CORROSION WITH FINAL DIMENSION OF .596 INCH ON THE FWD AND .577 INCH ON THE AFT LUG. REAMED THE BORES TO FINAL DIMENSION OF 1.1395 INCH ON THE FWD AND 1.1398 INCH ON THE AFT LUG. ALL WITHIN LIMITS. REPAIRS ACP'D REF SRM 55-10-10.