What was found
DURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACK ON THE RT FWD SPAR CAP ANGLE ON THE VERTICAL STAB COMING DOWN TO THE FIRST FASTENER, .375" IN LENGTH. REPAIRED IAW FR-CO-02532 REV 1, 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 CRACK ON THE RT FWD SPAR CAP ANGLE ON THE VERTICAL STAB COMING DOWN TO THE FIRST FASTENER, .375" IN LENGTH. REPAIRED IAW FR-CO-02532 REV 1, STEP 1. MAJOR REPAIR.