What was found
RT WING UPPER SKIN CORRODED AROUND HILOCK AT XRS554, ABOVE S54. NDT VERIFIED MATERIAL THICKNESS AT CORROSION REMOVAL SITE RANGED FROM .090-0.125. CUT OUT CORROSION SITE REF SRM 57-2-1 FIG28. FABRICATED DOUBLER AND FILLER FROM SHT7075T6-.190, MACHINED FILLER TO MATCH THICKNESS, INSTALLED AND SEALED CONICAL WASHERS AND REPAIR PARTS REF SRM 57-2-1 FIG 28, 51-1-20D, 51-1-8, 51-1-20B, 51-1-15.