What was found
DURING C-CHECK AT ILN, MAINTENANCE FOUND A CRACK INDICATION DURING AFTER MODIFICATION INSPECTION OF THE RIGHT FORWARD OUTER CHORD AND TENSION FITTING PER A/B 767-53A0078, AS MANDATED BY AD 2005-11-02. THREE DISCREPANT FASTENER HOLE LOCATIONS WERE OVERSIZED TO REMOVE DISCREPANCIES AND THE LOWER TENSION FITTING WAS REPLACED AS THE ANOMALY WAS TOO LARGE TO REMOVE BY HOLE ENLARGEMENT. RESULTING IN 3 HOLE LOCATIONS WITH HOLES LARGER THAN ALLOWED IN THE BULLETIN. BOEING INSTRUCTED ABX TO INSTALL OVERSIZED FASTENERS IN THE 3 LOCATIONS THROUGH THE ENTIRE STACK UP, TO INCLUDE THE CHORD, FITTINGS AND FUSELAGE SKIN. REPAIRED IAW REA B657-58095-MR.