As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
C5 CHECK - SKIN IS BENT ON THE AFT LT SIDE OF THE FORE RUDDER NEAR THE UPPER HINGE POINT. REMOVED DAMAGE BY BLENDING IAW SRM 51-14-00-02-01. REMOVED .058 METAL FROM EDGE. HFEC INSPECTED BLEND AREA FOR CRACKS IAW NDTM PART 6, 51-00-01, NO CRACKS NOTED. MAPPED FOR ENGINEERING. BLENDED AREA FOUND TO BE WITHIN LIMITS IAW RD 8/4-55-0504. PRIMED AND PAINTED BARE AREAS IAW RD 8/4-55-05-4.