As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LH WING I/B FLAP LOWER SURFACE HAS BULGING AREA AT FASTENER ROW JUST I/B OF O/B TRACK.(<P>REMOVED CORROSION LH WING I/B FLAP LOWER SURFACE. ORIG. MAT. WAS .125" REMAINING MAT. IS .034" IS FOUND TO BE OUT OF LIMITS IAW B767 SRM 57-53-01. REMOVED AND REPLACED LH WING I/B FLAP UPON CUSTOMER REQ. IAW B767 AMM 27-51-06, 27-51-07</P>)