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.(<P>BLENDED CORROSION ON UPPER CHORD ON AILERON RIB AT WS 434 TO DEPTH OF .017", MAX DEPTH ALLOWED.008" IAW B767 SRM 57-51-02-1A-1 DETAIL 19. OUT OF LIMITS. INSTALLED NEW AILERON UPPER CHORD RIB IAW B767 SRM 51-40-02 AND BOEING DWG 113T1510.</P>)