As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFTER REMOVAL OF EXISTING REPAIR DOUBLER AT LEFT HAND WING SLAT NR 2, FOUND FASTENER HOLES ELONGATED ON INNER SURFACE SKIN OUTBOARD CORNER. ACCOMPLISHED REPAIR AS PER SRM 51-10-00 FIGURE 29 VOLUME I REVISION 96. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.