What was found
WHILE IN HEAVY MAINTENANCE PERFORMING REPAIR MAPPING IT WAS NOTED THAT THE EXISTING REPAIR LOCATED ON THE EXTERNAL FUSELAGE SKIN B.S. 300 BETWEEN STRINGER 24R - 26R IS NON-COMPLAINT WITH SRM. REMOVED EXISTING REPAIR, CUT OUT DAMAGE DIM 18" X 15", PERFORMED HFEC INSPECTION WITH NO DEFECTS. FABRICATED REPAIR PARTS 1 EA FILLER FROM 2024 T3 .063" DIM. 5.8" X 28.5", 1 EA FILLER FROM 2024 T3 DIM. 1.1 X 8.5", 1 EA FILLER FROM 2024 T3 .071" DIM. 11.25" X 18" AND DOUBLER FROM 2024 T3 .071" DIM. 20" X 28.9". INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED AIRCRAFT WAS RETURNED TO SERVICE.