As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT LOWER FORWARD WING ATTACH FITTING CRACKED. CRACK WAS FOUND DURING SIRM WING ATTACH FITTING INSPECTION. EDDY CURRENT WAS THE INSPECTION METHOD. MFG SUPPORT WAS CONTACTED IAW SIRM INSTRUCTIONS. THE FITTING WAS REPLACED BY MFG SERVICES TECH USING WING FITTING KIT PN 90-4111-1S, SN 163 IWA DWG 90-4111.