As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING SCHEDULED INSPECTION, MAINTENANCE FOUND A CRACK ON THE LT THRUST REVERSER LT INNER UPPER LONGERON TAB. THE CRACK STARTED IN FASTENER HOLE AND PROPAGATED TO THE EDGE OF THE TAB. THE CRACK WAS REPAIRED BY FABRICATING AND INSTALLING REPAIR DOUBLER IAW NORDAM STANDARD REPAIR PROCEDURE. MAJOR MOD/REPAIR REPORT FILED WITH T.C.