What was found
TEAR STRAP FASTENER HOLE CRACK AT BS 777, S-20L. REMOVED FASTENER AND VERIFIED CRACK UTILIZING HFEC ROTARY HOLE PROBE METHOD IAW WITH NDT, REMOVED DAMAGED AREA AND HFEC INSPECTION COMPLETED NO DEFECTS NOTED. FABRICATED AND INSTALLED .032 IN 2024-T3 CLAD REPAIR FILLERS AND DOUBLERS WITH APPROVED FASTENERS, APPLIED ALODINE AND BMS 10-79 TYPE II PRIMER TO ALL REPAIR PARTS AND BARE SURFACES. APPLIED BMS 5-95 SEALANT TO ALL FAYING SURFACES. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE.