What was found
-AD- INSPECTION FOUND 01 EA CRACK AT THE SECOND FASTENER HOLE (COUNT FROM TOP TO BOTTOM) OF THE BS 1725 BULKHEAD OUTER CHORD STRAP. THE SKIN AND CHORD STRAP CRACK WAS REPAIRED AT STA 1725.5, S-7R PER B767-400 SRM 53-80-01-2R-5 REV 73.00 21AUG24. THIS IS A CATEGORY B REPAIR. INSPECTION THRESHOLD: 37500 FLIGHT CYCLES AFT AIRPLANE DELIVERY OR 6000 FLIGHT CYCLES AFTER REPAIR INSTALLATION WHICHEVER COMES LATER. THE REPEAT INSPECTIONS INTERVAL 6000 FLIGHT CYCLES, DO A DVI, LFEC, AND HFEC INSPECTION OF THE REPAIR AREA. SEE SRM 53-80-01-2R-5 TABLE III FOR DETAIL. (LP #0855552)