What was found
INSPECTION FOUND TWO 3 CRACKS IN VERTICAL STABILIZER SADDLE PANEL. THE SADDLE PANEL WAS REMOVED, REPAIRED IAW SRM 55-30-7, FIGURE3, AND REINSTALLED IAW MM 55-30-1, PAGE 201.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND TWO 3 CRACKS IN VERTICAL STABILIZER SADDLE PANEL. THE SADDLE PANEL WAS REMOVED, REPAIRED IAW SRM 55-30-7, FIGURE3, AND REINSTALLED IAW MM 55-30-1, PAGE 201.