As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CAPTAIN REPORTED THAT THE AIRPLANE AILERON COMPENSATOR TWIST ONLY TWO UNITS TO THE RIGHT. AIRCRAFT WAS SENT TO THE HANGAR, AND THE AFT TAB PUSHROD FAIRING BOLT WAS DETECTED INVERTED PROMOTING FRICTION BETWEEN THE ANCHOR NUT AND THE FAIRING. THE ANCHOR NUT WAS REPLACED AND THE AILERON TRIM TAB WAS ADJUSTED AND TESTED IAW MM 27-10-05, ALL CORRECT.