What was found
DURING INSPECTION, FOUND CRACK IN RUDDER SKIN APPROX .875 INCH IN LENGTH FROM RIVET TO RIVET TOP CLOSE OUT RIB MID POINT OF RUDDER. INSTALLED FLUSH REPAIR IAW SRM 55-03 FIG 8A.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING INSPECTION, FOUND CRACK IN RUDDER SKIN APPROX .875 INCH IN LENGTH FROM RIVET TO RIVET TOP CLOSE OUT RIB MID POINT OF RUDDER. INSTALLED FLUSH REPAIR IAW SRM 55-03 FIG 8A.