As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
HORIZONTAL STABILIZER CENTER SECTION REAR SPAR LT UPPER CLEVIS HAS CORROSION ON AFT SIDE OF THE AFT CLEVIS AND FWD SIDE OF THE FWD CLEVIS AROUND THE BUSHING. *S/D* REAMED THE BORES AND SPOTFACED BOTH SIDES OF THE FWD AND AFT CLEVIS TO REMOVE CORROSION. ALL WITHIN LIMITS OF SRM 55-10-10 ALLOWABLE DAMAGE 5. ACP'D HFEC WITH NO DEFECTS NOTED. INSTALLED OVERSIZED BUSHING REF SRM 55-10-10 ALLOWABLE DAMAGE 5.