As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C WING CTR SECTION FRONT SPAR VERTICAL STIFFENER FOUND CRACKED JUST AT STA785.9 RBL10.94. WING CTR SECT FRONT SPAR AT STA785.9 RBL10.94 VERT STIFFENER REPAIRED IAW RS R57-00-36677 ORG MATL IS BAC1518-749-2024T3511 CRK LENGTH IS 3" CUT OFF LENGTH IS 19.5" THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MATL BAC1518-749-2024T3511 AS REPLACEMENT SECTION TOTAL REPAIR LENGTH IS 29.6250" REF EO B767-5710-37263-A.