As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK AROUND THE FASTENER AT RIGHT WING NO.8 SLAT LOWER SURFACE NOSE SKIN AT ACTUATOR RIBS. / REMOVED; INSTALLED SERVICEABLE; ADJUSTED AND FUNCTIONAL TESTED #8 SLAT IAW MM 27-81-21-000-801 AND MM 27-81-21-000-801 AND MM 27-81-21-400-801 FUNCTIONAL CHECK GOOD VERIFIED ALL TORQUES SAFETYS AND CLEARANCES (POS: #8; TAG NO.: 702418; P/N OFF/ON: 144A5010-4; S/N OFF: 000796; S/N ON: 001646)