As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-CHECK, UPPER RUDDER L/E LEFT/RIDE SIDE WORE OUT / CHAFING AREAS. DAMAGED AREA FOUND TO BE OUT OF LIMITS IAW B-727 SRM 55-40-1 FIG 1. FABRICATED REPAIR DOUBLER IAW B-727 SRM 55-40-3 FIG 1. METAL TREATED AND PRIMED IAW B-727 SRM 51-10-2. INSTALLED DOUBLER IAW B-727 SRM 51-30-2.