What was found
AGEING INSPECTION, EXISTING REPAIR ON RT INBD FLAP LE SKIN RIB 12A - 17 REQUIRES EVALUATION FOR CONFORMITY. THE REPAIR WAS EVALUATED & FOUND IN CONFORMITY WITH SRM 57-50-00 FIG 208. HOWEVER, DENTS & NICKS WERE FOUND ON EXISTING REPAIR INSERT. REPORTED TO ENGINEER. REMOVED THE DAMAGED REPAIR INSERT & REPAIRED AGAIN IAW SRM 57-50-00 FIG 208 & COMPLETED. EO 6-5100-7-5000 D EOCN D1 PART 1 WAS COMPLETED. THE REPAIR WAS CATEGORY B & WAS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 126. THE FIRST INSPECTION THRESHOLD WAS 51000 FLIGHT CYCLES AFTER REPAIR. THE REPETITIVE INSPECTION INTERVAL & METHOD WERE TBD.