As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ACFT SKIN SPLICE PLATE HAS .50 INCH LONG CRACK APPROXIMATELY 13 INCHES RT OF LONGERON 1. THE OTBD END OF THE CRACK WAS LOCATED WITH HFEC, THE INBD END EXTENDS UNDER VERTICAL STAB RT ATTACH ANGLE MOUNT DOUBLER. REPAIRED IAW PRI 554287-14 REV 0 AND COMPLIED WITH ER/A 554287-14 REV A.