As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT FUSELAGE APPROX STA 192 AT LAP JOINT LWR ROW HAS DAMAGED SKIN AT FASTENER FROM STATIC DISCHARGE. REMOVED DAMAGE BY OPENING HOLE TO 1 - 4 INCH AND SPOT FACING DAMAGE REMOVED .030 MATERIAL FROM OVERLAPPING SKIN. ACP REPAIR PER UA-EVA-72343 AND SRM 53-00-01 REPAIR 8.