What was found
INSPECTION FOUND A .5 INCH CRACK AT AFT END OF RT VERTICAL STABILIZER ATTACH ANGLE, STA 1485. THE CRACKED AREA WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 23 AND 23A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A .5 INCH CRACK AT AFT END OF RT VERTICAL STABILIZER ATTACH ANGLE, STA 1485. THE CRACKED AREA WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-05, FIGURE 23 AND 23A.