What was found
THE CRACKS WERE FOUND IN THE SUBJECT STRUT CAP SKIN ASSEMBLY AND ADJACENT BULKHEAD STRAP AT STA-286 BULKHEAD INSTALLATION CROWN AREA AT B-L. 0-0. THE AFT EDGE OF CAP SKIN ASSEMBLY. THE BULKHEAD STRAP IN AREA COMMON TO CAP SKIN. INTERIM REPAIR OF THE 65B94053-27 CAP SKIN ASSEMBLY AND THE ADJACENT 65B89049-38. UPPER BULKHEAD ASSEMBLY, AT NAC STA 286 IN THE 65B94051-1 STRUT STRUCTURE ASSEMBLY FOR NR 2 PYLON ACCOMPLISHED AS PER BOEING MESSAGE 1-176887932 AND FAA FORM 8100-9.