As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER TRAILING EDGE PANEL ATTACH CHORD AT WS.434 22 INCHES AFT OF REAR SPAR HAS CORROSION AROUND NUTPLATE. BLENDED CORROSION ON UPPER CORD ON AILERON RIB AT WS 434 TO A DEPTH OF 0.17", MAX DEPTH ALLOWED .008" IAW B767 SRM 57-51-02-1A-1 DETAIL 19. OUT OF LIMITS. MECHANICALLY MEASURED TAG# 2932. INSTALLED NEW UPPER CHORD ON AILERON RIB AT WS 434 IAW B767SRM 51-40-02 PAR 4 AND 7 BOEING DWG 113T1510