What was found
INSPECTION FOUND A 1.3 INCH CRACK IN VERTICAL STABILIZER FRAME (VERT STAB T/E HINGE RIB) WHERE RUDDER RIG PIN R-5 GOES THROUGH FEEL AND CENTERING FRAME. A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5530-01445, PART 3.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
INSPECTION FOUND A 1.3 INCH CRACK IN VERTICAL STABILIZER FRAME (VERT STAB T/E HINGE RIB) WHERE RUDDER RIG PIN R-5 GOES THROUGH FEEL AND CENTERING FRAME. A PERMANENT REPAIR WAS INSTALLED IAW ECRA 5530-01445, PART 3.