What was found
LH STR 32L BETWEEN FR63 AND FR62 HAS SEVERAL SPOTS OF CORROSION GROUNDED - YES. EVALUATED CORROSION ON S32L AT FR 62-FR 63, ORIGINAL MATERIAL 0.071", REMOVED 0.045", REMAINING MATERIAL 0.026" FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS GIVEN IN A320 SRM MAJOR REPAIR ACCOMPLISHED - FUSELAGE STRINGER S-32L, BETWEEN FR62 AND FR63, CORROSION DAMAGE REPAIR PERFORMED IN ACCORDANCE WITH AIRBUS DOSSIER 81312718 WITH APPROVAL PER AIRBUS RDAF 81312718/003/2023 #B DATED 19-DEC-2023 PER EA A320-53EA-02-022 REV 00 DATED 12/19/2023 THIS IS A CATEGORY "A" REPAIR