As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HFEC INSPECTION CARRIED OUT ON REAR SPAR CAP RT FORWARD FLANGE UPPER SECTION CRACKED. APPROXIMATE 0.50 INCH IN LENGTH AS MARKED AT STA Y=2164. CRACKED AREA REPAIRED PER EA NR 1-5530-T0326616 PT 1 TITLE: AD 98-25-15 - STABILIZERS - VERTICAL STABILIZER. REAR SPAR P/N: AJC7515-501. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.