What was found
SPLICE HOLE ELONGATION AT FR54 STGR 44RH SIDE. REPLACED THE DAMAGED SPLICE WITH NEW FABRICATED SPLICE AT LOWER FUSELAGE FR54, S- 44R. I.A.W A300-600 SRM 51-72-10-001, PAGE.2& AIRBUS DWG NO:A53812405, REV.C00& FEDEX GMM 07-0-1001. THIS REPAIR IS CLASSIFIED AS CAT.A MAJOR PER GMM 06-2-100. (THE SPLICE REMOVED AND INSTALLED STEP, PLEASE REFERENCE FEDEX EA NO:T6-5330-T0369235 A P2, STEP.2& 7)