What was found
CRACK LOCATED AT BS 807, S-14L. CUT AND REMOVED DAMAGED AREA, VERIFIED CRACK REMOVAL UTILIZING HFEC METHOD NO DEFECTS NOTED, FABRICATED AND INSTALLED REPAIR ANGLES AND FILLER FROM .063 IN 2075-T6 IAW APPROVED FASTENERS WENT WITH BMS 5-95 SEALANT PER TABLE I AND TABLE V IAW SRM. APPLIED ALODINE COATING AND ONE COAT OF BMS 10-11, TYPE 1 PRIMER TO ALL REPAIR PARTS AND BARE SURFACES AND BMS 5-95 SEALANT APPLIED TO ALL FAYING SURFACES. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE.