What was found
IT WAS FOUND CRACK IN OPEN HOLE, AT AFT LOWER CORNER FUSELAGE SKIN, FWD SERVICE DOOR,DURING INSPECTION ROTARY SCANNER PER 767 NDT MANUAL PART 6, 51-00-16. IT WAS PERFORMED PERMANENT REPAIR AS PER SRM 53-10-01-2R-1, DETAIL III, FIGURE 201. THIS IS A CATEGORY B REPAIR; IT IS NECESSARY TO PERFORM THE INSPECTION REQUIREMENTS AS PER SRM 53-10-01-2R-1 PARAGRAPH 5.A TABLE INSPECTION THRESHOLD - 37,500 FLIGHT CYCLES AFTER AIRPLANE DELIVERY OR 6,000 MAXIMUM FLIGHT CYCLES FROM THE REPAIR INSTALL ATION, WHICHEVER OCCURS LATER. REPEAT INSPECTION EVERY 3,000 FLI GHT CYCLES. THIS REPAIR WAS ACCOMPLISHED AT THE #1RH FWD SERVICE DOOR CUTOUT, AFT LOWER CORNER. APPROVED.