As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ROUTINE INSPECTION FOUND LT WING L/E FIXED FIBERGLASS PANEL UPPER SURFACE AT WS 577/586 CRACKED LONGITUDINAL AND AT WS 752 PREVIOUS REPAIR DELAMINATED. PERMANENT REPAIRS ACCOMPLISHED IAW 51-40-09 AND 51-40-12, DOCUMENTED ON EO 4757A406.