What was found
RT BS 1129 AND BS 1138 FUSELAGE SKIN CRACKS LOCATED AT S5R AND S12R. TRIMMED OUT CRACKS MAINTAINING A MINIMUM TRIM OUT CORNER RADIUS .050 INCHES AT A SURFACE FINISH OF 63 RMS OR SMOOTHER. PERFORMED HFEC INSPECTION AROUND TRIMOUT AREA, NO DEFECTS NOTED. FABRICATED AND INSTALLED .063 INCHES 2024T3 REPAIR DOUBLER, TWO .056 INCHES 2024T3 FILLERS AND A 2024T3 CLAD ALUMINUM TAPER SHIM WITH APPROVED FASTENERS WET WITH CORROSION INHIBITOR TO A REPAIR PARTS. APPLIED BMS 5-95 SEALANT TO ALL FAYING SURFACES IAW ECO. RECEIVED 8110-3 APPROVAL. AIRCRAFT RETURNED TO SERVICE.