What was found
INSPECTION FOUND AFT FUSELAGE TO VERTICAL STABILIZER ANGLE ON RT SIDE CRACKED. THE OLD SPLICE WAS REMOVED AND A REPAIR ANGLE AND SPLICE WERE INSTALLED IAW SRM 51-30-2 AND 53-05, FIGURE 23A AND 23B.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND AFT FUSELAGE TO VERTICAL STABILIZER ANGLE ON RT SIDE CRACKED. THE OLD SPLICE WAS REMOVED AND A REPAIR ANGLE AND SPLICE WERE INSTALLED IAW SRM 51-30-2 AND 53-05, FIGURE 23A AND 23B.