As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK OF 1.250" LENGTH WAS FOUND ON RT HORIZONTAL STABILIZER UPPER AFT SKIN PANEL STA XH=-8.500. UPPER AFT SKIN WAS REPAIRED PER DWG SR09550028 REV D AND SRM 51-30-2 AND 51-30-5(ET). HFEC INSPECTION WAS ACCOMPLISHED ON RT HORIZONTAL STABILIZER UPPER AFT SKIN PANEL STA XH=-8.500 AND NO CRACKS WERE FOUND AFTER TRIM OUT PER NDT SPM 06-10-01.001.