As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSTALLATION OF NEW NR 1 AND NR 2 PYLON WING ATTACH TENSION CLIPS WOULD HAVE REQUIRED SPOTFACE GREATER THAN THE 0.005" ALLOWABLE PER EO 6-070332-03 WHICH PERTAINED TO S/B 757-54-0034 REV 1 FOR THE SIP MODIFICATION. TAPERED RADIUS FILLERS WERE FABRICATED AND INSTALLED FOR EACH HOLE.