What was found
LEFT WING LEADING EDGE UPPER SPLICE PLATE IS CORRODED AT LWS 500. REMOVED SECTION OF UPPER WING SPLICE FROM LWS 412.2 TO 512.3. INSTALLED SPLICE SECTION IAW AMES ENGINEERING DOCUMENT REA 47224REA15.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING LEADING EDGE UPPER SPLICE PLATE IS CORRODED AT LWS 500. REMOVED SECTION OF UPPER WING SPLICE FROM LWS 412.2 TO 512.3. INSTALLED SPLICE SECTION IAW AMES ENGINEERING DOCUMENT REA 47224REA15.