What was found
FOUND CRACK ON THE FRAME AT BS 480 ABOVE STRINGER 17R. CUT OUT AND REMOVED DAMAGED PORTION OF FORMED SECTION. VERIFIED CUTOUT WITH HFEC. DETERMINED FROM TABLES III, IV, AND V, THE NUMBER OF FASTENERS AND FASTENER ROWS REQUIRED. FABRICATED REPAIR PARTS FROM MATERIALS SPECIFIED IN TABLE 1. APPLIED ALODINE AND BMS10-11 TYPE 1 PRIMER TO ALL BARE ALUMINUM. INSTALLED REPAIR PARTS MAKING A FRAYING SURFACE SEAL AND FASTENERS WET WITH BMS 5-95 SEALANT. REPAIR COMPLETED IAW WITH SRM. AIRCRAFT RETURNED TO SERVICE.