As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON REMOVAL OF STRINGER SPLICE 9L, HFEC FOUND CRACK APPROX 0.1" LENGTH AT CABIN STA 5-0 ON LONGERON 9L FWD SECTION. REPAIRED AS PER SRM 53-00-05 FIG 202 REPAIR 1 REVISION 46. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 112. REPAIR LONGERON SEGMENT FABRICATED AS PER EA 1-5310-143570.