What was found
CUTOUT DAMAGED SKIN ARE AT BS 908 MAINTAINING A .50 INCH MINIMUM RADIUS AND 2D EDGE MARGIN. VERIFIED CRACK REMOVED USING HFEC METHOD. ENLARGED TRIMMED AREA BY .04 INCH AS AN INSURANCE CUT. FABRICATED TWO STRUCTURAL FILLERS, A REPAIR FILLER, DOUBLER, AND TRIPLER FROM 2024-T3 CLAD MATERIAL. FINISHED ALL BARE ALUMINUM WITH ALODINE AND TWO COATS BMS 10-11, TYPE 1 PRIMER. INSTALLED REPAIR PARTS WET WITH BMS 5-95 SEALANT BETWEEN THE FRAYING SURFACES. APPLIED A FILLET SEAL OF BMS 5-95 AROUND THE EDGES. REPAIR COMPLETED IAW SRM 53-30-3, FIGURE 48, SHEET 55. AIRCRAFT RETURNED TO SERVICE. (M)