As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 RUDDER HINGE ARM FORWARD ATTACH AREA FORWARD OF BEARINGS EXFOLIATED. REMOVED CORROSION AND POLISHED REWORK AREA PER SRM 51-76-10, APPLIED ALODINE TO THE REWORK AREA PER SRM 51-21-10. PERFORM HFEC TO REWORK AREA FOR CRACK, NO CRACK FOUND PER NTM 51-10-09/801 AND REPAIRED PER EA 6-5530-117380. MAJOR REPAIR PER GMM 6-2-100.