What was found
INSPECTION TYPE:C, WING CTR SECTION FRONT SPAR VERTICAL STIFFENER FOUND CRACKED JUST AT STA 785.9, RBL10.94, WING CTR SECTION FRONT SPAR VERT STIFFENER AT STA 785.9, RBL10.94. REPAIRED IAW R57-10-36925 & B767-5710-41478, CRACK LENGTH 2.25" CUTOFF LENGTH 19.5". THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH BAC1518-749-2024T3511 AS REPLACEMENT SECTION. TOTAL REPAIR LENGTH 28.5".