As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK INDICATION ON LT STAB L/E AT UPPER FWD TANG. CRACK EXTENDS ITSELF ACROSS FASTENER HOLE APPROX 1.25 INCH IN LENGTH. CRACK LOCATION IS 5 INCHES I/B OF CLOSURE RIB AREA. REPAIRED CRACK IN REF TO SRM 55-20-00 FIG 9 AND 10. ALSO, PER EA 8-5510-21035A.