What was found
LEFT WING LEADING EDGE SECTION 511AL .5 INCH CRACK NOTED IN OUTBOARD RIB UPPER FLANGE AT THE LAST FASTENER LOCATION. CRACK FOUND DURING C-CHECK. CRACK STOP DRILLED AND DOUBLER INSTALLED PER EA 7-57-49.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
LEFT WING LEADING EDGE SECTION 511AL .5 INCH CRACK NOTED IN OUTBOARD RIB UPPER FLANGE AT THE LAST FASTENER LOCATION. CRACK FOUND DURING C-CHECK. CRACK STOP DRILLED AND DOUBLER INSTALLED PER EA 7-57-49.