What was found
NDT INSPECTION, CRACK WAS FOUND AT THE RH FLANGE OF GANTRY 4.RH FR52.A. REPAIRED THE CRACK OF THE GANTRY RH #4 AT FR52A PER AIRBUS DWG: R53810581 ISSUE: C. DETAIL REPAIR STEPS: DRILLED CRACK STOP HOLES DIA 4 TO 4.012MM AT EACH END OF CRACK AND INSTALLED THE CRACK STOP HOLE PLUGS PER AIRBUS DWG: R53810581 ISSUE: C. WET INSTALLED THE REPAIR ANGLE AND STRAP OF MOD MATERIAL KIT PER A300-600 SRM 51-40-21 & AIRBUS DWG: R53810581 ISSUE: C. MANUFACTURED AND INSTALLED A NEW BRACKET TO BE ADAPTED THE REPAIR CRACK AREA PER A300-600 SRM 51-40-21. MAJOR REPAIR IAW FEDEX GMM 6-2-100. THIS IS A CAT A REPAIR