As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A SCHEDULED STRUCTURAL CHECK MX DISCOVERED A CRACK ON THE LT FUSELAGE SKIN JUST INBD OF THE LT WING BOTTOM WING PANEL AT F.S. 303.25. CRACK APPROXIMATELY 2.250 INCHES IN LENGTH. MX REPAIRED THE CRACK ON THE LT FUSELAGE SKIN JUST INBD OF THE LT WING BOTTOM WING PANEL AT F.S. 303.25 IAW GLA EO-09-1900-53-004.