What was found
INSPECTION FOUND A 2 INCH CRACK IN TAIL CONE FRAME UNDER ACTUATOR LINK AREA. THE CRACKED AREA WAS TRIMMED OUT. THE AREA WAS REINFORCED WITH FRAME AND SPLICE IAW SRM 53-30-00, FIGURE 3, 51-31-01 AND 51-21-01.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 2 INCH CRACK IN TAIL CONE FRAME UNDER ACTUATOR LINK AREA. THE CRACKED AREA WAS TRIMMED OUT. THE AREA WAS REINFORCED WITH FRAME AND SPLICE IAW SRM 53-30-00, FIGURE 3, 51-31-01 AND 51-21-01.