As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
#8 SLAT; ACTUATOR ROD END ATTACH FITTING; FWD I/B MOST HOLE CRACKED (MARKED) VERIFIED BY HOLE PROBE PER NDT PART 6 51-00-00 PROCEDURE 16 / REMOVED AND REPLACED #8 SLAT PER MM 27-81-21. TAG NO: 442476 PN ON: 114A5010-4 SN ON: 000082 PN OFF: SN OFF: 001614