What was found
INSPECTION FOUND A 1 INCH CRACK IN RIB AT LT INNER CAVITY OF TAIL CONE. THE RIB WAS TRIMMED OUT AND THE AREA WAS REINFORCED WITH AN ANGLE REPAIR IAW SRM 53-00-00, FIGURE 1 AND 51-31-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1 INCH CRACK IN RIB AT LT INNER CAVITY OF TAIL CONE. THE RIB WAS TRIMMED OUT AND THE AREA WAS REINFORCED WITH AN ANGLE REPAIR IAW SRM 53-00-00, FIGURE 1 AND 51-31-01.