What was found
EXPOSED COMPOSITE MATERIAL ON BOTH FACE OF RUDDER CONTROL TAB. BOTH FACES OF RUDDER CONTROL TAB WERE REPAIRED IAW SRM 51-70-1, AD PAR 23.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
EXPOSED COMPOSITE MATERIAL ON BOTH FACE OF RUDDER CONTROL TAB. BOTH FACES OF RUDDER CONTROL TAB WERE REPAIRED IAW SRM 51-70-1, AD PAR 23.