What was found
CENTER WING BOX MID SPAR VERTICAL STIFFENER GOT CRACK AT FR44,Y1456~Y1959 POSITION. FABRICATED AND INSTALLED NEW STIFFENER AT CENTER WING BOX FR44, Y1456~Y1959 I.A.W AIRBUS DRAWING A57110436 & GMM 7-0-1001 & EA NO:T6-5710-T0380275 P1, SEQ NO:760, TITLE:WINGS-BASIC WING STRUCTURE- CENTER WING BOX-FR44 BEAM STIFFENER FABRICATION- ALERNATE HEAT TREATMENT. THE REPAIR CLASSIFIED AS CAT.A MAJOR PER GMM 6-2-100.