What was found
DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB LT SPAR CAP ANGLE AT 20 PERCENT CHORD AT VSS 84.10, .75" IN LENGTH. REPAIRED IAW FR-CO002516R1, STEP 1. MAJOR REPAIR.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE VERTICAL STAB LT SPAR CAP ANGLE AT 20 PERCENT CHORD AT VSS 84.10, .75" IN LENGTH. REPAIRED IAW FR-CO002516R1, STEP 1. MAJOR REPAIR.