What was found
DURING A SCHEDULED ROUTINE INSPECTION, FOUND THREE CRACKS ON THE VERTICAL STAB RT SPAR CAP ANGLE AT THE 20 PERCENT CHORD TOP FASTENER AT VSS 84.10, .5" 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 THREE CRACKS ON THE VERTICAL STAB RT SPAR CAP ANGLE AT THE 20 PERCENT CHORD TOP FASTENER AT VSS 84.10, .5" IN LENGTH. REPAIRED IAW FR-CO-02520R1, STEP 1. MAJOR REPAIR