What was found
DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK ON THE VERTICAL STAB LT SPAR CAP ANGLE AT THE 20 PERCENT CHORD TOP FASTENER AT VSS 84.18, .125" IN LENGTH. REPAIRED IAW FR-CO-02520R1 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 ON THE VERTICAL STAB LT SPAR CAP ANGLE AT THE 20 PERCENT CHORD TOP FASTENER AT VSS 84.18, .125" IN LENGTH. REPAIRED IAW FR-CO-02520R1 STEP 1. MAJOR REPAIR