What was found
LEFT WING LEADING EDGE LBL 92.0 WEB CRACKED 1.5 INCHES DOWN FROM TOP AFT VERTICAL STIFFENER. ACCESS 6302. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER SUGGESTED WING FLEX OR STRESS LOADS POSSIBLE CAUSE.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING LEADING EDGE LBL 92.0 WEB CRACKED 1.5 INCHES DOWN FROM TOP AFT VERTICAL STIFFENER. ACCESS 6302. FOUND DURING SCHEDULED C-MAINTENANCE CHECK. SUBMITTER SUGGESTED WING FLEX OR STRESS LOADS POSSIBLE CAUSE.