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 AFT SPAR UPPER CLEVIS FWD AND AFT LUG HAVE EVIDENCE OF CORROSION. SPOTFACED FWD AND AFT FACES OF THE LUGS TO REMOVE CORROSION TO THE FINAL DIMENSION OF 1.110" ON THE FWD LUG AND 1.126 INCH ON THE AFT LUG. REAMED FWD LUG TO THE FINAL DIMENSION OF 1.5312 INCH. ALL WITHIN LIMITS. REPAIRS ACP'D REF SRM 55-10-10.