What was found
INSPECTION FOUND VERTICAL STABILIZER LEADING EDGE LOWER PANEL UPPER ATTACH BULKHEAD CRACKED AT ATTACH HOLES. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND VERTICAL STABILIZER LEADING EDGE LOWER PANEL UPPER ATTACH BULKHEAD CRACKED AT ATTACH HOLES. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 55-30-3.