What was found
RT OTBD FLAP L/E UPPER PLATING WORN AT XF 226.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DWG W51-R05 FAA FORM 8110-3 DATED 09-28-04. REMOVED DAMAGED SKIN SEGMENT IAW SRM 51-1-21, SRM 51-3-0. FABRICATED NEW SKIN SEGMENT (2024-T3AL 0.071) INTERNAL SPLICE DOUBLER (2024-T3AL 0.080) IAW DWG W51-R05. CLEANED, TREATED AND PRIMED REPAIRED AREA, NEW SKIN SEGMENT INTERIOR, INTERNAL SPLICE IAW SRM 51-1-8B. APPLIED SEALANT IAW SRM 51-1-11. INSTALLED NEW SKIN SEGMENT AND INTERNAL SPLICE DOUBLER IAW SRM 51-1-21 PG 1, SRM 51-3-0 PG 1, DWG W51-R05.