What was found
THE REPAIR WAS C/W TO A SKIN DENT BETWEEN FRAME 24A-25 AND STRINGER 42-43 RT. REPAIRED UNDER USA 3000 EO 05-53-014, DATED APRIL 20,2005, WHICH INCORPORATES THE PERMANENT REPAIR DEFINITION PER AIRBUS SRM 53-00-11 PARAGRAPH 4K, FIGURE 221. REMOVED DAMAGED SKIN, FABRICATED INTERNAL DOUBLER FROM 2024T3, 0.056" ALUMINUM, FILLER FROM 2024T3, 0.050" ALUMINUM & ANOTHER FILLER FROM 2024T3, 0.020" ALUMINUM. REPAIRED STRINGER (43 RT), UTILIZING STRINGER MATERIAL ASNA2215 (SAME AS ORIGINAL), COUPLING MATERIAL TYPE DAN2001T79511 (A539-86219) & A FILLER FROM 2024T3, 0.056" ALUMINUM. APPLIED SEALANTS & PROTECTIVE TREATMENTS.