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 LT FORWARD FLANGE UPPER SECTION FOUND CRACKED. CRACK APPROXIMATE 2.0 INCHES IN LENGTH AS MARKED AT STA Y =2164. CRACKED AREA REPAIRED PER EA NR 1-5530-T0326617 PT 1 TITLE: AD 98-25-15 - STABILIZERS - VERTICAL STABILIZER. REAR SPAR P/N: AJC7515-501 FORWARD FLANGE RADIUS. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.