What was found
TRIMMED OUT THE SKIN CRACK. VERIFIED HFEC CUTOUT AND ROTARY PROBE INSPECTION OF LAP SPLICE FASTENER HOLES. FABRICATED AND INSTALLED STRUCTURAL FILLERS, A DOUBLER, AND TEARSTRAP PER FIGURE 48. ALODINED AND PRIMED ALL REPAIR PARTS AND BARE SURFACES. APPLIED CORROSION INHIBITING COMPOUND. ASSEMBLED REPAIR PARTS WITH BMS 5-59 SEALANT ON ALL MATING SURFACES PRIOR TO FASTENER INSTALLATION. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 48, DETAIL XII. AIRCRAFT RETURNED TO SERVICE. (M)