What was found
CRACKED STRINGER AT AREA AFT OF FCB BS540 S-26L WL152. MARKED ; / [01] REMOVED DAMAGED S-26L SECTION AT BS 500D+10'-540 AND PERFORMED GVI NO ADDITIONAL DAMAGED FOUND IAW SRM 53-00-03-2R-1.; [02] VERIFIED DAMAGE REMOVAL AND PERFORMED GVI NO ADDITIONAL DAMAGED FOUND IAW SRM 53-00-03-2R-1.; [03] HFEC INSPECTED CUT END OF STRINGER PER NDTM PART 6; 51-00-00 PROCEDURE 23. NO CRACKS NOTED.<BR>CAL ID: ATS1465 S/N: 60004150296; [04] COMFORMED NEW S26L SECTION MAT. USED 7075 T6 CLAD 0.045' LOT#1439668-1 RO.827277-SWA. AND SPLICE MAT USED 7075 T6 CLAD 0.050' LOT#1442011-1 RO.827276-SWA. VERIFIED HEAT TREATMENT AND FABRICATION IAW BAC 5602;DWG 143A3241 AND SRM 53-00-03-2R-1; LOCATED AND DRILLED; APPLIED CHEMICAL CONVERSION COATING IAW SRM 53-00-03-2R-1.; [05] VERIFIED NEW S26L SECTION MAT. USED 7075 T6 CLAD 0.045' LOT#1439668-1 RO.827277-SWA. [06] APPLIED PRIMER ON REPAIR PARTS AND REPAIR AREA BS 500D+6' - 540 S26L IAW SRM 53-00-03-2R-1. OK TO INSTALL.; [07] VERIFIED PRIMER APPLICATION TO THE REPAIR PARTS AN AIRCRAFT STRUCTURE PER SRM 53-00-03-2R-1. OK TO INSTALL STR REPAIR AT BS500D + 6' TO BS540;