As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
WHILE ACCOMPLISHING INSPECTIONS MANDATED BY DAL SI 4-59271-12AD, MTC FOUND A .031 GAP BETWEEN THE NR 1 SLAT ACTUATOR AND THE SUPPORT FITTINGS. THE GAP WAS SHIMMED PER THE REQUIREMENTS OF BAC S/B 727-57-0130 AND DOCUMENTED IN ER/A 363526-14AD.