What was found
B767-53-3-7064 - LOWER HALF FUSELAGE STA 1438 BETWEEN S38R-S39R HAS CRACK REF NRC 9130394, SKIN DAMAGED AREA TRIMMED OFF PER SRM 53-00-01- 2R-29 REAPIR FIG 201. SKIN THICKNESS IS 0.056". HFEC CARRIED OUT PER B767 NTM PART6 51-00-19 REV 125, NO CRACK FOUND. REPAIR DOUB LER INSTALLED PER SRM 53-00-01-2R-29 REPAIR 29 FIG 201 DETAIL 1 CREATED DIP FOR CATEGORY B REPAIR INSPECTION REQUIREMENT PER SRM 53-00-01 REPAIR 29 FIG 201 TABLE V. PER SRM 53-00-01-R2-29 REPAIR 29 TABLE V(5) ACP INITIAL 1 TIME INSPECTION AT 6000 FLIGHT CYCLES AFTER REPAIR INSTALLATION (REPAIR ACP AT 17460 CYCLES) AND ALTERNATIVE 1 INSPECTIONS AT 12000 FLIGHT CYCLES THEREAFTER PER NDT PART 6, 51-00-01. THIS REPAIR IS A: ZONE A-CATEGORY B REPAIR. TOMC-APPROVAL FROM SC1ELBYC COMMENT RECORDS UPDATE............VD TOMC APPROVED : QC REVIEWED. TOMC APPROVED : QC REVIEWED. RECORDS UPDATE............VD INIT: 6000 FC (INIT WILL ITO TO RIR -0607) RIR: 12000 FC...............VD/U353583